G12132 CONSOLE WIRING DIAGRAMS REVISION U

EAGLE COPTERS USA INC.

190 S Danebo Ave, Eugene, OR 97402 | Phone: 800-564-6469

www.eaglecopters.com

G12132 CONSOLE WIRING DIAGRAMS

REVISION U

MDL GA107 Rev R STC SH4747NM

Canada STC# SH93-83 ANAC-Brazil CHST# 2007S06-08, -09

http://www.eaglecopters.com/

ELECTRICAL INSTALLATION INSTRUCTIONS AND NOTES FOR P132 AND P122 CONSOLES

THIS DOCUMENT INCLUDES INFORMATION PROPRIETARY TO GENEVA AVIATION AND SHALL NOT BE

USED OR DUPLICATED BY ANYONE WITHOUT THE WRITTEN PERMISSION OF GENEVA AVIATION, INC.

www.genevaaviation.com

G12132-1 Revision U DATE: 10/20/2017 Page 1 of 16

1 OVERVIEW

1.1 It is essential, and required, for the installer to read all instructions and notes contained on all documents PRIOR to starting the installation of the console.

1.2 This G12132 document applies to the P132 and P122 Consoles. This document provides the electrical definition of the console, which is the same for the P132 and P122 with the exception of the model-specific wiring for the switch overlay lighting. P132 and P122 consoles are mechanically different; see documents G10251 (Rev. H or later) and G12310 (Rev. B or later) for the mechanical details of the P132 and P122 console assemblies, respectively.

1.3 G12132 Page Summary (base versions):

-1: Electrical Installation Instructions and Notes -2: BAT-EXT PWR, MASTER CUTOFF (DIRECT BATTERY also on some versions) -3: GENERATOR, CRANK, HYDRAULICS (or ACCU) TEST, WARNING HORN, WARN / FIRE TEST -4: Lighting circuits. -5: FUEL PUMP, PITOT HEAT, WIPER, SAND FILTER, (SERVO TEST also on some versions) and optional

switches. -6: Circuit Breakers EFN-36 thru EFN-43 -7: Circuit Breakers EFN-45 thru EFN-58 -8: Circuit Breakers EFN-59 thru EFN-66 -9: Circuit Breakers EFN-67 thru EFN-87 -10: Circuit Breakers EFN-91 thru EFN-N/A-2 (-4 on some versions) -11: Bus Bar supply circuits -12: Optional circuit breakers for the middle and top left breaker rails -13: Console right side layout -14: Console left side layout -15: Console top view switch layout -16: Sample AVIONICS control circuits -17: Sample CARGO HOOK circuit -18: Sample HOIST circuit -21: Float Electrical circuit for use with new installation of Aerazur float system -23: Overlay Dimmer circuit -26: Wiring modifications for combined HOIST and CARGO HOOK switch -27: Wiring modification for active-OFF avionics relay circuit -28: Breaker / switch wiring modifications for use with Precise Flight 3060S Pulse Light module -29: Instrument Lights 2 switch wiring modification for PP15 bus mounted outside the console -30: Sand Filter switch wiring modification for use with FDC/aerofilter filter system P/N 1350IN1-7 -31: Float Switch circuit for interfacing to pre-installed float systems -32: Wiring modifications for Dual Hydraulics system on AS350B3 -33: Wiring modifications for Twist Grip per SB 67.00.37 -34: Wiring modifications to Instrument Lights circuits for 217L dimmer power supply -35: Wiring modifications to Emergency bus circuit for mod 350A07-3476 -36: Wiring modifications to Cargo Hook circuit per SB 25.01.09 -37: Console Backlight Power for mod 350-A073476

1.4 Due to the changes in the AS350 product line as it has evolved, the wiring in a console for any particular aircraft will be based on one of eight overall templates:

1.4.1 The base version of the wiring diagrams is generally applicable to AS350D, D1, B, BA, B1, or B2 aircraft that predate mod 350A07-3273. The wiring diagrams belonging to this set have no suffix on the ends of the drawing numbers. Where differences exist between aircraft versions, a table lists the different breaker ratings, breaker labels and/or aircraft wire numbers, as applicable. The drawing numbers for the layout pages (-13 through -15) generally end with the aircraft version, for example G12132-13-B2.

1.4.2 The version for AS350B2 aircraft embodying mods 350A07-3273 and -3274 ends in -073273, for example G12132-3-073273. AS350B2 aircraft at this mod level are not compatible with any other versions of the wiring






diagrams, and earlier aircraft or those embodying mod 350A07-3368 are not compatible with the -073273 drawing set.

1.4.3 The version for AS350B2 aircraft embodying mod 350A07-3368 ends in -073368, for example G12132-3-073368. AS350B2 aircraft at this mod level are not compatible with any other versions of the wiring diagrams, and earlier aircraft are not compatible with the -073368 drawing set.

1.4.4 The version for AS350B3 aircraft that predate mod 350A07-3274 covers the original release, Service Bulletin 80.00.05 / mod 350A07-3087, and mod 350A07-3257. The wiring diagrams specific to this set end in -073087, for example G12132-2-073087. Although the console wiring is the same for mods 350A07-3087 and 350A07-3257, there are some differences in breaker labels on the right hand side of the console, requiring separate right-side views G12132-13-073087 and G12132-13-073257. AS350B3 aircraft that predate mod 350A07-3087, and in which Service Bulletin 80.00.05 has not been implemented, should use the -073087 labeling and wiring, leaving the FADEC breaker circuitry shown on G12132-2-073087 unconnected.

1.4.5 The version for AS350B3 aircraft embodying mods 350A07-3273, -3274 and OP.3346 ends in -073274, for example G12132-5-073274. AS350B3 aircraft at this mod level are not compatible with the earlier B3 versions of the wiring diagrams, and earlier aircraft are not compatible with the -073274 drawing set. The -073274 drawing set must be modified per G12132-34 in accordance with sections 3, 7, 8 and 9 of this document for compatibility with AS350B3 aircraft embodying mod 350A07-3368.

1.4.6 The version for AS350B3e aircraft with the Arriel 2D engine embodying mod 350A07-3476 but before mod -4280 ends in -073476, for example G12132-3-073476. AS350B3e aircraft at this mod level not compatible with earlier B3 versions of the wiring diagrams, and earlier aircraft are not compatible with the -073476 drawing set.

1.4.7 The version for AS350B3 aircraft embodying mod 350A07-4280 ends in -074280, for example G12132-4-074280. AS350B3 aircraft at this mod level are not compatible with any other versions of the wiring diagrams, and earlier aircraft are not compatible with the -074280 drawing set. Although the internal wiring is the same, for aircraft embodying mod 350A07-4629 and mod 350A07-4677 there are aircraft wire connection changes, and for mod 350A07-4629 a circuit breaker name and rating change. Where these differences exist, a table lists the different breaker ratings, breaker labels and/or aircraft wire numbers, as applicable. The different breaker label name requires separate left-side views G12132-14-074280 and G12132-14-074629.

1.4.8 The version for AS350B2 aircraft embodying mod 350A07-4280 ends in -074280B2, for example G12132-4-074280B2. AS350B2 aircraft at this mod level are not compatible with any other versions of the wiring diagrams, and earlier aircraft are not compatible with the -074280B2 drawing set.

1.5 The information contained in one of these eight drawing sets applies to most AS350 helicopters of the specified version and mod level. However, a particular helicopter may not exactly fit the data as shown. The installer must determine whether the information is suitable for the specific AS350 helicopter that this installation is being applied to.

1.5.1 For instance, a particular helicopter may have been upgraded from an earlier version. In such a case, a wire on the aircraft may have a different label than the one shown in the drawing that applies to the aircraft’s current version level. The installer will need to trace out the wire to determine how it is connected, and then compare that information to the Eurocopter Wiring Diagram Manual (WDM).

1.5.2 Also, some aircraft might require a 7.5A breaker for the same function for which other aircraft require a 2.5A breaker. The installer must determine the rating of the existing fuse or circuit breaker installed for each circuit, and make sure the proper breaker rating is used in the replacement circuit on the console, prior to starting this installation.

1.6 Drawings containing Sample Optional circuitry such as the HOIST and CARGO HOOK show primarily the circuitry related to the console. This includes items that were part of the original console but are not installed in the P132 or P122 console, such as status lights. The installer must ensure that the complete circuitry for these functions is installed in accordance with the Eurocopter Wiring Diagrams Manual, including any items listed as being outside






the console. For instance, with the CARGO HOOK function, the installer would need to provide and install a HOOK ARMED status light in clear view of the pilot and provide suitable labeling.

1.7 In all cases, it is up to the installer to insure that this installation is correct for the particular helicopter. If there is any doubt, or any questions, contact Geneva Aviation for assistance before proceeding.

2 ORIENTATION

2.1 All references in this document to “forward”, “aft”, “left”, “right”, “up”, “down”, “top” or “bottom” are given with respect to the airframe in which the console is or will be installed. “Forward” is toward the nose of the aircraft, etc. The top surface of the console sits at an angle, with the forward edge higher than the aft edge, so “up” in reference to a switch on the console refers to its forward position, and “down” refers to its aft position.

3 CONFIGURATIONS AND CONFIGURATION-SPECIFIC DRAWING IDENTIFICATION

3.1 For quicker reference in relation to a specific aircraft, a subset of the G12132 document set may be compiled, containing only the pages relevant to that particular aircraft, provided that the entire document is also available for reference. For example, in the case of generic console for an AS350B2 that embodies mod 350A07-3273, the subset might include all pages of G12132-1; the -073273 versions of G12132-2 through G12132-18; and the version of G12132-23 relevant to the console type (P122 or P132).

3.2 A drawing subset may be assigned a configuration number, consisting of the console type and a suffix that refers to the generic aircraft version, the specific aircraft serial number, or a 5-digit index number for a customer-specific configuration. In addition, individual drawings in a configuration set that deviate from the standard drawings are identified with suffixes that identify either the aircraft or the customer for which the configuration is developed. To prevent unintentional re-use of a configuration number or customer-specific drawing set suffix, Geneva Aviation maintains a log of factory-assigned configuration numbers and the associated suffixes for P132 and P122 consoles.

3.3 Examples of configuration numbers include P132-00001, which consists of the diagrams relevant to a P132 console built for use with an AS350B2 predating mod 350A07-3273, and P132-00042, which consists of the diagrams relevant to a P132 console built for use with a B3 embodying mod 350A07-3257. The hypothetical configuration number P122-2817 would refer to a P122 configuration specifically defined to interface to the equipment installed in aircraft serial number 2817, while P122-D would refer to the diagram subset for a basic P122 console wired for, and bearing the switch and breaker labels relevant to, the AS350D version.

3.4 While many of the circuits shown in the standard wiring diagrams are required for the operation of the aircraft, some others are not. Switches, circuit breakers, diodes, wires, and connector pins that are not required for a particular installation, may be reassigned for another purpose at the installer's discretion, provided that they are labeled appropriately and that the current ratings of all parts in the circuit are adequate for the application. Unused switches, circuit breakers, diodes, connector positions, etc. may be used for additional needs at the installer's discretion, with the same provisions. Unneeded items may be left out of the final assembly at the installer's discretion. Unneeded items that are installed should be labeled "SPARE" to indicate that they are not being used and are available for future use.

3.5 Any such modifications to the console wiring or labeling, the circuit breaker ratings or switch types, or to the aircraft wires connecting to the console, must be documented. To this end, a page in a wiring diagram subset may be derived from the original and changed to show those modifications, provided that the page is assigned a unique drawing number based on both the original drawing number and the specific installation or customer-defined configuration of which the drawing is a part.

3.6 For example, if a console were built specifically to be installed on aircraft serial number 1111, and if the label for switch number OP-3 on that console were to be changed from the original shown in the base version of the drawings, then all diagrams in the subset that contain switch OP-3 (specifically G12132-5, -14, -15 and -18) would need to show the new switch label, and would need to be renumbered. The resulting pages in this case might be numbered G12132-5-1111 etc.






3.7 In some cases, a drawing will not contain any changes to the circuits contained on the drawing, but will contain references to other diagrams that do contain changes. In the example above, drawings G12132-6, G12132-8, G12132-9 and G12132-10 all contain references to G12132-5. In the example of the previous paragraph, all references to G12132-5 on these diagrams would need to be updated to G12132-5-1111, and the resulting diagrams would need to be named G12132-6-1111 etc. Since the outer views G12132-13 and -14 contain references to some or all of these drawings, those references would also need to be changed and the resulting drawings would be identified as G12132-13-1111 and G12132-14-1111.

3.8 Only those drawings in the set that actually contain modifications, either to the circuitry or to the references, need to be assigned new, unique drawing numbers, so at the installer’s discretion the unmodified drawings in the drawing set for a particular aircraft or configuration may, but need not, be assigned drawing numbers with a suffix matching the rest of the drawing set. For instance, G12132-2 contains only switch circuitry that should not be changed, and no references to other drawings, so a derived version of G12132-2 is unlikely to be needed, but the drawing included in a set for aircraft serial number 1111 could be assigned the number G12132-2-1111 if desired.

3.9 If a single modification or set of modifications is intended to be applied to consoles on several aircraft that use the same base wiring template (for example, several AS350B2 aircraft that predate mod 350A07-3273), the resulting drawing set may be assigned a configuration number as outlined in paragraph 3.2, but would use a suffix based on the specific application or customer rather than referring to a single aircraft’s serial number. One example of an actual customer configuration drawing is G12132-5-LAPD, from configuration P132-00004.

3.10 Modifications contained in any customer-specific configuration must follow the rules specified in this G12132-1 document, so that a console may be built to the configuration-specific wiring diagrams at assembly time, rather than being built to one of the basic templates and needing to be modified during installation.

4 WIRE AND WIRE LABELS

4.1 The following wire types are approved for internal console wires: M22759/16-“gauge”-9, M22759/32-“gauge”-9 or M22759/41-“gauge”-9. The wire type and gauge is printed directly on the insulation, and therefore does not need to be included in the wire number.

4.2 All wires within the console are AN20 gauge, unless noted otherwise on the wiring diagrams. For some circuits the wire is defined at a larger gauge than is strictly required, to provide the option of using that circuit with a higher-rated circuit breaker for alternative functions. Additionally, at the installer’s discretion, the installer may use a larger wire than is called for in the wiring diagrams, provided that the larger wire can still be terminated and connected properly for the application.

4.3 Wires may be labeled using any legible method that does not compromise the wire or insulation. These methods include but are not limited to: hot stamping, laser-marking, slip-on wire markers, and wrap-around labels generated by computer printout or by a label maker.

4.4 The wire number format that is used for internal console wires throughout this document identifies a wire by the diagram on which it is defined, with an index number. For instance, wire number G12132-4-14 is shown on diagram G12132-4. Certain wires may be found on more than one diagram but will be labeled the same on all diagrams in a set for a particular aircraft, configuration, or aircraft version and mod level.

4.5 At the installer’s discretion, any wire-numbering format may be used, provided that it allows unique identification of each wire. For instance, a wire might be labeled according to its connections at each end. Using the previous example, wire G12132-4-14 connects terminal 1 of switch ESN-10 to pin B of connector J2 in all five standard wiring diagram sets, so “ESN-10-1 J2:B” would be a reasonable label. If ESN-10 is mounted in its standard position (fourth from the forward edge of the right-hand switch rail), the wire might be labeled “SWR4:1 J2:B”.

5 DIODES AND DIODE CIRCUITS

5.1 Unless specified otherwise, diodes carry less than 3 amps of continuous current, at less than 50 volts, so these unspecified diodes may be any type of rectifier diode with maximum ratings of at least 3 amps and 50 volts.






Although provision is made for mounting up to seven diodes on the P132 and P122 consoles, and the standard wiring diagrams make maximum use of these provisions, the mounting location of diodes is at the installer’s discretion.

5.2 In cases where diodes are required but are not built into the console, it is the installer’s responsibility to provide diodes and mount them securely.

6 TERMINALS AND CONNECTORS

6.1 Unless noted otherwise, each wire that attaches to a screw or stud is terminated by a ring terminal of suitable size at each end that attaches with a screw or stud, and each wire that attaches to a connector is terminated by a connector pin or socket as appropriate. No connector pin or socket shall attach to more than one wire; if multiple wires must be routed to a single pin or socket, connect them together using a butt splice of the appropriate size. However, circuit breaker and switch terminals should have only one ring terminal attached, so if more than one wire is routed to the same terminal of a switch or circuit breaker, crimp the wires together into one ring terminal of suitable size. Also, the terminal block on the Overlay Power Supply may have either one or two ring terminals attached per position, so the wires connected to the output terminals may be grouped accordingly.

6.2 Geneva Aviation uses the following crimp terminals in building the consoles:

TERMINAL TYPE WIRE GAUGE TE CONNECTIVITY P/N #6 Ring Terminal 22 – 16 ga 36152 16 – 14 ga 326882 or 36158 #10 Ring Terminal 16 – 14 ga 36160 10 ga 31805 or 33457 8 ga 31807 or 33460 Butt Splice (if needed) 26 – 20 ga D-436-82 20 – 16 ga D-436-83 16 – 12 ga D-436-84

6.3 Connectors are recommended but not required. At the installer’s discretion, the connectors may be left out of the

installation entirely, and the aircraft wires may be connected to the switches and breakers either directly or through butt splices, provided that the wiring diagrams are updated to reflect the changes. At the installer’s discretion, connectors may be added to handle additional circuits beyond the capacity of the standard J1/P1, J2/P2 and J3/P3 connector pairs.

6.4 The connectors used by Geneva Aviation for the P132 console are as follows:

Connector Part Number Contact Type Contact Part Number Backshell Part Number J1 MS3471L22-55P 20ga pins M39029/4-110 M85049/51-1-22N P1 MS3476L22-55S 20ga sockets M39029/5-115 M85049/52-1-22N

J2 MS3471L24-31P 16ga pins M39029/4-111 M85049/51-1-24N P2 MS3476L24-31S 16ga sockets M39029/5-116 M85049/52-1-24N

J3 MS3471L24-31S 16ga sockets M39029/5-116 M85049/51-1-24N P3 MS3476L24-31P 16ga pins M39029/4-111 M85049/52-1-24N

6.5 For the P122 console “J” connectors, the MS3471 connector series is replaced with the MS3470 series. The pin

and socket contacts remain the same. The P122 aircraft-side “P” connectors use the M85049/51 backshells as listed above for the P132 “J” connectors. No backshells are used on the P122 console-side “J” connectors. The wires are secured directly to the connector bracket.

6.6 As an alternative to the MS3470 / MS3476 or MS3471 / MS3476 connector series pairs, the MS3120 / MS3126 or MS3121 / MS3126 series pairs may be used at the installer’s discretion.






6.7 In some installations, there may not be enough pins in the standard connectors for all of the connections that need to be made. In such a case, additional connectors from the series listed above may be used, provided that the contact size is suitable to the task. It is the responsibility of the installer to ensure that the types of additional connectors are selected to prevent cross-connections with each other or with the standard connectors.

6.8 All connector pins must be crimped with the proper tool. For the MS3470 / MS3471 / MS3476 series connectors, use the M22520/1-01 4-point crimper with M22520/1-02 positioning die.

7 CIRCUIT BREAKERS AND BREAKER CIRCUIT MODIFICATION

7.1 Circuit breakers are Mil-Spec type MS26574, or one of the following commercial equivalents: 4200-002-“amps”, 4200-001-“amps”, 7277-2-“amps”, or 7274-2-“amps”. Where possible, the breakers are numbered based on the fuses from the original Eurocopter console that they replace. The format is EFN-##, where ## is the fuse position number from the Eurocopter WDM 39.00.00 listing for mod 07.2760 for the B3, and mod 07.1736 for earlier models. Those breakers that are not direct replacements are designated EFN-N/A-1, EFN-N/A-2, etc, with the exception of EFN-71E and EFN-72K, which replace breakers on the later B3 models.

7.2 This numbering carries over to the Mod 350A07-3273, -3274, -3368 -3476 and -4280 versions where the same functions exist. Where possible, new systems are assigned to the same breakers as the older systems that they replace, and the rest are assigned to breakers whose original functions no longer exist in the newer definitions.

7.3 Circuit breakers are oriented with the key facing toward the center of the P132 console. On the P122 console, the key on the circuit breaker faces forward. The bus bars normally mount on the non-key side of the circuit breakers for both console types, except on the middle and forward (“top”) columns on the P122, where the bus bars mount on the key side.

7.4 At the installer’s discretion, a breaker circuit that is not used for its originally defined function may be assigned to another purpose, provided that the label is updated to reflect the change, both on the console and on the wiring diagrams. Breaker labels may be abbreviated as necessary, both on the console and on the drawings.

7.5 At the installer’s discretion, circuit breakers may be relocated on the bus to which they are connected, with the wire lengths adjusted as necessary. This includes moving breakers between the two PP6 bus segments in the middle right and bottom right breaker rails.

7.6 At the installer’s discretion, circuit breakers that are not required for their original functions may be moved to the optional rails, in order to supply power to additional equipment from alternate power sources such as voltage converters or relay-controlled power busses. In all such cases, it is the installer’s responsibility to ensure that the power source, components, wiring and connections are adequate for new functions.

7.7 Breakers assigned to required aircraft functions must not be moved between busses. In some cases, PP5 and PP6 provide backup or complementary functions in some areas (for instance, Engine Instruments), which would be defeated by placing both breakers on the same bus.

7.8 At the installer’s discretion, for optional breaker circuits the installer may replace a length of bus bar with two shorter lengths in order to power the sections from different sources, or may replace a length of bus bar with a shorter length in order to separate a breaker for use with a separate source wire. The installer may obtain these shorter lengths from Geneva Aviation, or may cut down the existing bus bar to suit the circuit requirements.

7.9 In cutting a bus bar, the installer must use the existing bar as a pattern to duplicate the existing spacing in the resulting pieces, in the following criteria:






7.9.1 Distance from the end to the nearest breaker connecting hole;

7.9.2 Position of the bus wire attachment hole with respect to the nearest breaker connecting holes;

7.9.3 Rounding the corners and smoothing the rough edges to prevent chafing any wires in the vicinity.

7.9.4 A properly modified section of bus bar will cover the full width of the circuit breaker terminal at each end of the bar, and will be separated from an adjacent breaker terminal or bus bar section by not less than 1/4”.

7.10 A separate hole is always required for the bus supply wire. Do not attach a bus wire and a circuit breaker to a bus bar at the same hole.

7.11 3 Amp circuit breakers (MS26574-3 Eaton P/N: 4200-001-3) may be substituted for aircraft systems that use 2.5 amp circuit breakers (MS26575-2 ½) in production of the console. Use of the 3 amp circuit breakers will be reflected in all drawings for production of that console.






8 SWITCHES AND SWITCH CIRCUIT MODIFICATION

8.1 All switches used on the console are environmentally sealed toggle switches, normally of either single-pole (MS24523 or MS24658 series) or double-pole (MS24524, MS24659, MS24707 or MS27408 series) type. Those that are direct replacements for switches in the original Eurocopter console are designated ESN-##, referring to the position number of the Eurocopter switch per the WDM 39.00.00 listing for mod 07.1736. Those that are not direct replacements, or are replacements for switches not found in the mod 07.1736 version of the console, are designated OP-1, OP-2 etc.

8.2 Except where specified otherwise, all switches are mounted with the key slot facing forward. Most two-position switches are ON when the toggle is in the forward position, which connects terminals 1 and 2 together on most switches. The aft position connects terminals 2 and 3 together on most switches. On those switches that are mounted with the keyway facing aft, the forward position connects terminals 2 and 3 and the aft position connects terminals 1 and 2.

8.3 On switches with 3 positions, the center position is OFF. For MS2740x series 3-position switches, internal connections do exist in the center position and some circuits may be energized. For MS2452x or MS2465x series 3-position switches, all terminals are internally disconnected from each other in the center position. For most two-position switches, the aft position is OFF, although some such as the Crank and Sand Filter switches may energize an alternate circuit in this position.

8.4 On double-pole switches, terminals 4, 5 and 6 correspond to terminals 1, 2 and 3 respectively for the separate second pole. A double pole switch may be used as a substitute for a single pole switch, provided that the switch rating is suitable and the mounting clearance is adequate. Switches that directly drive incandescent lamps are required to be the double pole type, which has a higher lamp current rating per pole.

8.5 The type of toggle (standard or locking) is optional for most switches, and may be changed at the discretion of the installer. Changing the type of toggle will usually result in a change in the switch part number, which is acceptable provided that the replacement switch has an adequate current rating for the application. Any switch on the console may be upgraded to a Locking Toggle type to prevent accidental operation, provided that the lock does not interfere with the intended operation.

8.6 Switch toggles may be color-coded to help identify the switch. RED color coding is REQUIRED for the Master Cutoff switch, and may not be used elsewhere. YELLOW color coding is REQUIRED for the Hydraulic Test switch (if installed), and may not be used elsewhere. Any color that is clearly distinguishable from these may optionally be used for any other switch. Color may be applied by the use of paint, a plastic coating or cover, vinyl dip, or other methods that do not interfere with the operation of the switch.

8.7 If two switch functions that need only single-pole functionality are only used simultaneously, they may be combined into one double-pole switch, with each pole activating one function, provided that the switch current rating is adequate for the application.

8.8 If two switch functions that need only single pole ON-OFF functionality are never used simultaneously, they may be combined on a single center-OFF switch so that one function is ON when the switch is in the forward position and the other function is ON when the switch is in the aft position, provided that the switch current rating is adequate for the application. The LANDING / PULSE LIGHT switch circuit shown on diagram G12132-28 is an example of this method.

8.9 If one switch function is used only when another, independent switch function is already ON, and both functions need only single-pole ON-OFF functionality, then the two circuits may be combined on a single center-OFF switch using circuitry similar to the ANTI-COL ALL / TAIL switch circuit shown on diagram G12132-4, provided that the switch current rating is adequate for the application.






8.10 An available, unused switch may be connected in line between a breaker and its connector pin, provided that the switch rating is adequate for the application, the switch is labeled to reflect the new function, all wires connecting to the switch are assigned unique wire numbers, and the wiring diagrams are updated to reflect all changes.

8.11 Individual switch legends may be replaced easily in the field to accommodate circuit reassignments or operator labeling preferences. Switch labels may be abbreviated, both on the console and on the drawings.

8.12 For compliance with this STC, the functionality and labeling of 3-position switches must remain consistent with the current revision of the relevant Rotorcraft Flight Manual Supplement for the particular console model. Deviations from the specified functionality and labeling may not be installed during assembly at the factory, but must be performed by the installer after delivery, and the installer must seek a separate approval for a revised Rotorcraft Flight Manual Supplement from the appropriate Aviation Authority.

9 CUSTOMIZING THE STANDARD SWITCHES

9.1 THE FOLLOWING SWITCHES ARE REQUIRED FOR THE OPERATION OF THE AIRCRAFT, AND MUST NOT BE REWIRED OR REASSIGNED, EXCEPT AS REQUIRED TO PERFORM THEIR STANDARD FUNCTIONS OR FOR COMPLIANCE WITH SERVICE BULLETINS REGARDING THE CONSOLE OR THE AIRCRAFT:

ESN-1 (DPST LOCKING): BAT-EXT POWER ESN-2 (SPST): FUEL PUMP (FUEL PUMP 1 when FUEL PUMP 2 switch installed) ESN-3 (DPDT ON-OFF-MOMENTARY): GENERATOR ON / RESET ESN-5 (SPST MOMENTARY): CRANK ENGINE ESN-6 (DPDT LOCKING): MASTER CUTOFF ESN-7 (DPDT MOMENTARY-OFF-MOMENTARY): WARN / FIRE TEST ESN-8 (SPST): FUEL PUMP 2 (for B2 implementations; see alternate OP-3) ESN-11 (SPST LOCKING, (MOMENTARY on B3 Dual Hydraulic)): HYDRAULICS TEST / ACCU TST ESN-12 (DPDT): WARNING HORN ESN-13 (SPST): PITOT HEAT OP-2 (SPST): DIRECT BATTERY (for post-Mod 350A07-3273 B2 and B3 implementations only) OP-3 (DPST): FUEL PUMP 2 (for B1 and alternate for B2 predating Mod 350A03-3273) OP-3 (SPST MOMENTARY): SERVO TEST (for B3 implementations with Dual Hydraulic)

9.2 Depending on the console in question, some of this group of switches should not be moved from their standard

positions. Figures 1 and 2 identify these switches for the P122 and P132 consoles, respectively. The remaining switches may be customized to fit the requirements of the installation. The following are some of the ways in which this can be accomplished:

9.3 ESN-9 (DPDT Center-OFF): ANTI-COL ALL/TAIL may be reduced to SPST if no strobe light is installed other than the primary anti-collision light, or if a separate switch is available to use for the second strobe light circuit.

9.4 ESN-18 (SPST): LANDING LIGHT may be upgraded to a DPDT type switch (Center-OFF or normal) in order to add a second function, such as a PULSE LIGHT function. Alternatively, if the LANDING LIGHT function is moved to another location such as the Pilot's Collective Grip as described on G12132-4, then ESN-18 could be reassigned to another function entirely. On aircraft post-mod 350A07-3476 the LANDING LIGHT switch is located on Pilot’s Collective Grip and ESN-18 is a spare switch unless the installer explicitly relocates the LANDING LIGHT switch to the console.

9.5 ESN-10 (DPST): POSITION LIGHT and EFN-17 (DPST): TAXI LIGHT may NOT be reduced from the specified DP switches to SP, due to the current rating required for these functions. However, the switches may be upgraded to DPDT Center-OFF to permit combining two functions on a single switch similar to ESN-9. For instance, once suitable wiring is added to the console, the LANDING LIGHT function could be moved from ESN-18 to the second pole of ESN-17 upgraded to Center-OFF, and the switch could be used to activate the TAXI LIGHT in the forward position, and the LANDING LIGHT circuit in the aft position, or vice versa, thus permitting ESN-18 to be reassigned to an entirely different function. On aircraft post-mod 350A07-3476 the TAXI LIGHT






switch is located on Pilot’s Collective Grip and ESN-17 is a spare switch unless the installer explicitly relocates the TAXI LIGHT switch to the console.

9.6 ESN-14 (DPDT) and ESN-15 (DPDT): INSTRUMENT LIGHTS 1 and 2 are wired so as to duplicate the functionality of the original Eurocopter console circuitry. In aircraft that predate Mod 350A07-3273/-3274, this is necessary only if the original Eurocopter fiber optic lighting is used. If the fiber optic lighting system is replaced by post lights, the INSTRUMENT LIGHTS 2 circuit may be unnecessary. In those circumstances, as long as the wires connecting the INSTRUMENT LIGHTS 2 circuit to the INSTRUMENT LIGHTS 1 and Overlay Dimmer circuits are removed from the console, the circuit may be rewired and/or reassigned to another function. Note that this is NOT true of aircraft embodying mod 350A07-3273-3274 or later, where the differences in the Instrument Lights circuitry created by the introduction of the Direct Battery bus make both switch circuits necessary. On aircraft embodying mod 350A07-4280 the INSTRUMENT LIGHTS switches have been relocated off the console and ESN-14 and ESN-15 are spare switches that may be assigned to installer-specified functions.

9.7 ESN-21(DPDT): SAND FILTER has one pole wired through the SAND FILTER breaker. This is the only switch on the console that is normally wired for compatibility with the SAND FILTER circuit. However, if there is no SAND FILTER equipment installed on the aircraft, this circuit may be reassigned and/or rewired for another purpose.

9.8 ESN-24 (SPST): WINDSHIELD WIPER is normally wired for a single Windshield Wiper circuit only. It is connected through a breaker, and provides both a constantly-powered and a switched connection, as required by Windshield Wiper equipment. If this switch is not needed for its intended use (for instance, if no Windshield Wiper equipment is installed on the aircraft), this switch may be rewired and/or reassigned for another use. If both Pilot's and Copilot's Windshield Wipers are present, this switch might be upgraded to DPDT, with the second pole wired like the original in order to control the second wiper motor.

9.9 OPTIONAL SWITCHES: OP-1 (DPST) is not directly tied to a specific function, although it is generally identified by its most common usage (AVIONICS MASTER). On aircraft that do not require OP-2 for the DIRECT BATTERY control function, OP-2 is generally labeled CARGO HOOK. When OP-3 is not required for FUEL PUMP 2 or SERVO TEST, it is generally labeled SPARE SWITCH on the B3, or HOIST on earlier models. When not needed for the aforementioned required functions, these switches may be reassigned at the installer's discretion, subject to the amperage ratings of the switches and wiring used. Under these circumstances, OP-2 may be upgraded to DP, and along with OP-1 and OP-3, may be rewired as DPDT or upgraded to DPDT Center-Off at the installer's discretion.

9.10 The standard wiring diagrams define 20 switches each for the P122 and P132 consoles. The P122 console will hold a maximum of 24 switches (Figure 1) with lighted legends for all switches. The standard P132 console holds only the standard 20 switches, but supplemental switch mounting capacity with lighted legends may be added at the forward end of the radio bay of the P132 console using structural components identical to those which make up the top switch rail at the front of the unit (Figure 2, flag note 3). Additional switches mounted in these positions must be of the types listed in paragraph 8.1, or of 4-pole type from the MS24525, MS24660, MS27406 or MS27409 series (space permitting), to qualify for installation under this STC. The additional switches may be wired in-line between breakers and connector pins as needed, or wired to the aircraft through spare connector pins, or wired directly to the aircraft, provided that the wiring diagrams are updated to match.

9.11 The G12301 power supply installed in the P132 console is capable of driving the only one supplemental switch mounting rail, along with the overlays for the standard switch rails. Additional switch rails may be mounted, but a separate power supply and dimmer control must be installed, in an installer-defined location, to drive the additional overlays.






INSTRUMENT

LIGHTS 2

INSTRUMENT

LIGHTS 1

AVIONICS

MASTER

PANEL

DIMMER

ANTI-COL

ALL / TAIL

POSITION

LIGHTS

TAXI

LIGHT

P122 SWITCH OPTIONS

GENERATOR

ON / RESET

FUEL

PUMPHOIST

BAT-EXT

POWER

WARN / FIRE

TEST

WINDSHIELD

WIPER

SAND

FILTER

HYDRAULIC

TEST

PITOT

HEAT

CRANK

ENGINE

CARGO

HOOK

LANDING

LIGHT

WARNING

HORN

MASTER

CUTOFF

2

1 1

MASTER CUTOFF and BAT-EXT POWER should not be moved from their current positions

GENERATOR ON / RESET requires reverse orientation and must be mounted in one of the two positions shown

The PANEL DIMMER control must be mounted in one of these four positions, OR moved to the Aft Wall of the

console.

Once these provisions are met, the remaining switches may be relocated on the switch plate at the installer's

discretion.

EMPTY SWITCH POSITIONS: Any of the three empty switch positions (four, if the Dimmer is relocated to the

aft wall) may be used to mount additional switches, or for other purposes such as indicator lamps, at the

installer's discretion.

1

2

3

3

Figure 1: P122-specific Switch Options






Figure 2: P132-specific switch options

AVIONICS

WINDSHIELD

MASTER

FILTER

CARGO HOOK

SAND

WIPER

BAT-EXT

HOIST

FUEL PUMP

POWER

HYD TEST

GENERATOR ON / RESET

WARN / FIRE TEST

CRANK ENGINE

LANDING LIGHT

ALL / TAIL

LIGHT TAXI

POSITION LIGHTS

ANTI-COL

WARNING

INSTRUMENT LIGHTS 2

HORN

INSTRUMENT LIGHTS 1

MASTER CUTOFF HEAT

PITOT

SWITCH SPARE

SWITCH SPARE

SWITCH SPARE SPARE

SWITCH SWITCH SPARE SPARE

SWITCH

P132 SWITCH OPTIONS

1

3

2

The Top Switch Rail, and the forward switches in the left and right hand rails, SHOULD NOT be rearranged in any way.

All positions in the Left and Right Switch Rails can accommodate either SP or DP switches

Additional center switch rails may be added in the radio bay, to a maximum of 6, although the overlay lighting power supply will support only one. Due to the spacing of switch mounting holes, there is not room to mount two DP switches in adjacent positions in the center rails. DP switches may alternate with SP switches, or two SP switches may be installed side-by-side. A 4-pole switch must be separated from any adjacent switch by an empty mounting position.

As long as these conditions are met, the switches in the side rails, and any installed center rails other than the top rail, may be rearranged at the installer's discretion.

3

1

2

2






REVISION HISTORY for ALL PAGES of G12132

Rev Level

Date

Description of Changes

Approval

F 10/10/2007 Reorganized and expanded data in all sheets of G12132-1, added data from G12132-15-P132-Choices, and reformatted as a single document.

Reformatted and removed B3 circuitry and references from G12132-2 through G12132-

11. Removed Overlay data from G12132-11. Removed “Optional” from G12132-23 and renumbered wires to eliminate references to G12132-11. Added G12132-23-P122.

Added wiring diagram set G12132-2-073087 through G12132-11-073087 for AS350B3

and moved B3 data from original drawings to this set. Added wiring diagram set G12132-2-073273 through G12132-11-073273 for AS350B2

with VEMD-based instrumentation and Direct Battery bus. Added wiring diagram set G12132-2-073274 through G12132-11-073274 for AS350B3

with Direct Battery bus. Updated G12132-12, and added G12132-12-073273 for B2 and B3 with Direct Battery

bus. G12132-13-x, G12132-14-x, G12132-15-x: Replaced B3 outer views with 073087

versions. Updated B2 versions. Added 073273 and 073274 versions. Added D, B, B1 versions. Added corresponding P122 versions for all of these.

Updated G12132-16, G12132-17 and G12132-18, and added 073087, 073273 and

072374 versions of these. Deleted G12132-19, G12132-20, G12132-22, G12132-15-P102-Choices. Reformatted and rearranged G12132-21 for improved visual clarity Added G12132-26 Combined Hoist / Hook switch mod, G12132-27 Active-OFF

Avionics Master switch mod, G12132-28 Pulse Light Switch and Breaker mods (2 pages), G12132-29 Instrument Lights 2 Switch Mod for Relocated Direct Battery Bus, G12132-30 Engine Alt Air switch mod, and G12132-31 Float Switch Interface mod diagrams.

RBH

G 05/06/2008 Added G12132-32 Dual Hydraulics Circuitry mod diagram Corrected aircraft wiring for ESN-12 on G12132-3-073273 and G12132-3-073274 Added missing drawing references in the G12132-073273 and G12132-073274

drawing subsets Corrected drawing references on G12132-13-073087, G12132-13-073087-P122 and

G12132-13-073257-P122 Corrected typographical errors on G12132-9-073274, G12132-14-073273 and G12132-

14-073273-P122 Removed “OPTIONAL” from G12132-23-P122

RBH






H 09/25/2008 Revised color coding specifications in G12132-1 paragraph 8.6 Added note requiring YELLOW color coding for HYDRAULICS TEST switch on

G12132-3, G12132-3-073087, G12132-3-073273, G12132-3-073274, G12132-32.

RBH

J 03/23/2009 Added switch series MS27406 thru MS27409 in G12132-1 paragraphs 8.1 and 9.10, outlined the function of these series in paragraph 8.3, and clarified the limitations on modifying the “required” function switches in paragraph 9.1.

Incorporated MS27407-3 switch into WARN/FIRE TEST switch circuits in G12132-3,

G12132-3-073087, G12132-3-073273 and G12132-3-073274. Changed the following drawings to list the new switch type: G12132-15-B, G12132-15-B-P122, G12132-15-B2, G12132-15-B2-P122, G12132-15-073087, G12132-15-073087-P122, G12132-15-073273, G12132-15-073273-P122, G12132-15-073274 and G12132-15-073274-P122.

Updated G12132-073274 wiring set to make Dual Hydraulics standard, as follows:

Listed airframe wires for both Single and Dual Hydraulic circuits on G12132-3-073274. Changed standard OP-3 switch type and wiring for SERVO TEST on G12132-5-073274, and switch type on G12132-14-073274 , G12132-15-073274 and G12132-15-073274-P122. Changed label and references for EFN-N/A-1 on G12132-10-073274, G12132-14-073274 and G12132-14-073274-P122.

Updated G12132-32 to reflect Dual Hydraulics circuits being standard in the G12132-

073274 diagram set. Moved function of airframe wire WW1F / 1WW1F inside the B3 consoles to free up one

connector pin, affecting drawings G12132-3-073087, G12132-3-073274, G12132-6-073087, G12132-6-073274, G12132-13-073087, G12132-13-073087-P122, G12132-13-073257, G12132-13-073257-P122, G12132-13-073274 and G12132-13-073274-P122.

Updated airframe wire for EFN-94 on G12132-10-073274.

RBH

K 03/04/2010 Added drawings G12132-33 and G12132-34 to list under paragraph 1.3. Added wire PE2F or 1PE2F as appropriate to support Very Cold Starting function,

affecting drawings G12132-2, G12132-2-073087, G12132-2-073273 and G12132-2-073274.

Added wire DH112E or 1DH112E as appropriate, to support Eurocopter Mod 350A07-

3397, affecting drawings G12132-3, G12132-3-073087, G12132-3-073273, G12132-3-073274 and G12132-33.

Added symbols and note to connect airframe wire shields together for Warning Horn

circuit, affecting drawings G12132-3, G12132-3-073087, G12132-3-073273 and G12132-3-073274

Added PITOT indicator light option to drawings G12132-5-073273 and G12132-5-

073274 Removed erroneous airframe wire connections from EFN-57 HOIST breaker circuit,

affecting drawings G12132-7 and G12132-7-073273.

RBH






L 04/06/2010 Added wiring diagram set G12132-x-073368 for AS350B2 equipped with Rotor Tach Frequency Inverter and Updated Instrument Lighting system per mod 350A07-3368.

Updated G12132-1 throughout for the addition of a fifth template, and edited references

to mod levels to include mod 350A07-3368 where appropriate. Updated G12132-1 paragraph 1.2 of G12132-1 to match the current revision level of

G10251 and G12310. Updated G12132-1 section 1.4 to link the G12132-x-073274 drawing set to mod

OP.3346 (Dual Hydraulics), and to cover modifying the -073274 set for compatibility with the Instrument Lights in AS350B3 embodying mod 350A07-3368.

Updated G12132-1 paragraphs 3.4 and 3.6 through 3.10 to correct inconsistencies and

clarify drawing nomenclature. Updated G12132-1 Figure 2 Flag Note 3 to address 4-pole switches and the overlay

lighting power supply. Added G12132-1 paragraphs 8.12 and 9.11.

RBH

M 05/12/2010 Added wiring diagram G12132-35, affecting G12132-1 paragraph 1.3. Updated wiring diagram sets G12132-x-073274 and G12132-x-073368 to provide for

Eurocopter Mod 350A07-3476, affecting sheets 2 and 11 of each of these sets.

Changed recommended part number for 6A 50V diode on G12132-21 and -31.

RBH

N 12/20/2011 Added wiring diagram set G12132-x-074305 for AS350B3e equipped with the Arriel 2D engine.

Updated G12132-1 throughout for the addition of a sixth template, and edited

references to mod levels. Added wiring diagram G12132-36, affecting G12132-1 Paragraph 1.3.

RBH

P 2/24/2012 Added Section 7.11 allow substitution of 2.5 Amp Circuit Breakers with a 3 Amp Circuit Breaker.

CLB

Q 12/06/2012 Added wiring diagram set G12132-x-074280 for AS3503B aircraft with factory installed Multibloc console per mod 350A07-4280

Updated G12132-1 throughout for the addition of a seventh template, and edited

references to mod levels. Added wiring diagrams G12132-37 for AS3503B installations. Updated G12132-03-073273 to accommodate changes made to the Fire Detection

circuitry by Eurocopter EASB 26.00.02

GA






R 2/08/2013 Updated wiring diagram set G12132-x-074280 to accommodate aircraft wiring changes i.a.w Eurocopter SB 350A-00.01.66

Removed wiring diagram set G12132-x-074305 Added wiring diagram set G12132-x-073476 for aircraft post-mod 350A07-3476 Updated G12132-1 to cover drawing modifications listed above.

GA

S 9/17/2014 Added alternate part numbers for wires. GA

T 4/27/2017 Updated G12132-1 section 1.4.7 for aircraft embodying mod 350A07-4629 and 350A07-4677

Updated G12132-1 section 9.1 for HYD TEST change to momentary locking on B3

aircraft. Updated G12132-x-074280 for the following: Implementing changes made in mod

350A07-4629 and mod 350A07-4677 and changing ESN-11 switch type to locking momentary.

Added drawings G12132-14-074629 and G12132-14-074629-P122 to show FUEL

LOW breaker added on mod 350A07-4629. Updated G12132-3-073273 to correct WARN / FIRE TEST switch wiring. Updated G12132-3-073274, G12132-15-073274, and G12132-15-073274-P122 to

change ESN-11 switch type to locking momentary. Updated G12132-3-073476, G12132-15-073476, and G12132-15-073476-P122 to

change ESN-11 switch type to locking momentary. Updated G12132-30 to show wire number differences on Single and Dual Hydraulic

aircraft.

GA

U 10/20/2017 Added G12132-1 section 1.4.8 for G12132-x-074280B2 drawing set. Updated G12132-1 section 9.1 for HYD TEST change to momentary locking on B3

Dual Hydraulic aircraft. Added ACCU TST option for HYD TEST switch. Updated G12132-3-073274, G12132-15-073274, and G12132-15-073274-P122 to add

ACCU TST option for HYDRAULIC TEST switch. Updated G12132-3-073476, G12132-15-073476, and G12132-15-073476-P122 to add

ACCU TST option for HYDRAULIC TEST switch. Updated G12132-3-074280, G12132-15-074280, and G12132-15-074280-P122 to add

ACCU TST option for HYDRAULIC TEST switch. Updated G12132-10-074280, G12132-14-074629 and G12132-14-074629-P122 and

added drawings G12132-13-074629 and G12132-13-074629-P122 to show FUEL LOW breaker swapped with GYRO breaker.

Updated G12132-4-074280 for Anti-Collision Light external wiring change.

GA

Effectivity: AS350D, D1, B, BA, B1, and B2 predating mod 350A07-3273


1

2

3

4

5

6

UPDATED FORMAT, COMPANY INFO;

Changed from original Eurocopter circuitry:Use EU18E instead of PE1E as power source.

UPDATED INFOADDED AIRCRAFT VERSION INFO

RELABELED CONNECTORS

REPLACED P102 WITH P122 DATA;

BA

C

The toggle of this switch must be marked with the color RED

08/16/00

10/10/07

04/22/00GLHGLH

RBH

EU3F Z G12132-2-10Z

G12132-2-07

G12132-2-09

P1

EU18E T

MS24659-23D

G12132-2-08

J1

T

D6:A

D5:CD5:A

D6:C

ref: WDM 24.30.00ref: WDM 62.30.00ref: WDM 77.00.00

G12132-2-01

1

2

3

4

5

6G12132-2-02

G12132-2-03

ESN-6MASTER CUTOFF

PG2NE

PG3NE

PE2F (if installed) and PE2E

X

Y

W

MS24659-23D

P1G12132-2-04

G12132-2-05

G12132-2-06X

Y

W

J1

ESN-1BAT-EXT PWR

PG6NE S

PG1NEP1R

S

J1R

G12132-2 D

SWITCH DETAILSP132 and P122 CONSOLE WIRING

GLH 03/30/00

GLH 03/30/00

GA107 1

SEE NOTES ON G12132-1

NOTICE:The circuitry related to the BAT-EXT PWR switch and the MASTER ELECTRICAL CUTOFF switch has been changed from the Eurocopter original circuitry. The functions are the same, but the wiring is different. Install using this wiring, and use this drawing for future electrical trouble shooting.

ADDED AIRFRAME WIRE PE2FD 03/04/10 RBH

NOTE:This switch is installed with keyway facing aft.

G12132-3-05



UPDATED FORMAT, COMPANY INFO

B3 DATA OFF PAGE

ADDED AIRCRAFT VERSION NOTE

RELABELED CONNECTORSUPDATED INFO

REPLACED P102 WITH P122 DATA

UPDATED WIRE NUMBERS, MOVED

BA

C

EW39E or EU13E

EW38E or EU16E

EW37E or EU15E

EW36NE or EU17E

k

n

m

P1j

ref: WDM 62.30.00

08/16/0004/22/00

GLHGLH

10/10/07 RBH

ESN-12WARNING HORN

MS24524-23

1

2

3

4

5

6

G12132-3-16

G12132-3-14

G12132-3-15k

n

m

J1j

G12132-3-17

V

U

J1

M

N

P

The Generator switch has a center off position. The up position provides the normal GENERATOR ON function. The momentary down position provides the GENERATOR RESET function.

POST MOD 350A07-1686

MPA2E

PA1E N

PA4E

KK1E

KK2E

V

P

U

P1

ref: WDM 80.00.00ref: WDM 24.30.00

MS24524-31(Center off)

G12132-3-07

G12132-3-02

G12132-3-06

G12132-3-08

G12132-3-01

MS24523-26

CRANKESN-5

3

2

1

5

4


6

G12132-3-03ESN-3

2

3

1

G12132-3 F


GLH 03/30/00

GLH 03/30/00

GA107 1


HYD TEST

F

MS24658-23D

J1

R

J2

S

ref: WDM 29.00.00

CRANK

EFN-63

2.5A

PP6DH6NE

DH112E (if installed) and DH1E

DH5E

S

R

P2

F

P1

3

2

1

ESN-11

D1:A

G12132-3-12

G12132-3-13

G12132-3-11

D1:C

G12132-3-09

G12132-3-10

PP5

7.5A

EFN-36

HYDRAULICS

The toggle of this switch must be marked with the color YELLOW

ADDED ESN-11 COLOR CODINGD 09/25/08 RBH

LK16NE or PE4NE or GND

ref: WDM 26.10.00ref: WDM 31.50.00

G12132-3-04

b bWW2NE G12132-3-20

G12132-3-19

G12132-3-18WG4E dc c

d

P1 J1

1

2

3

4

5

6

(3-position)MS27407-3

WARN / FIRE TESTESN-7

G12132-3-23

G12132-23-09

GND for OVERLAYS

E CHANGED ESN-7 TYPE & WIRING 03/23/09 RBH

If wires EW38E and EW39E are installed in the aircraft, connect the shields of these two wires together outside of the P1 connector

ADDED EFN-7 NOTES

NOTE: ESN-7 maintains connections between terminals 2 and 3, and between terminals 4 and 5, when the switch toggle is in the center position.

DH112E TO HYDRAULICS CIRCUIT;

F 03/04/10 RBHAIRFRAME WIRES; ADDED WIREADDED SHIELD NOTE FOR ESN-12

This 3-position switch performs the FIRE TEST function in the aft position


G12301:1 DIMMER CONTROL (SEE G12132-23 or G12132-23-P122)

INSTRUMENT LIGHTS 1

G12132-4-10

LK43E

The INSTRUMENT LIGHTS 2 function is required when using the Eurocopter dimmer module for the Instrument Panel lighting. This function is not used when using the Geneva dimmer. If this function is not used, the two wires connecting ESN-15 to ESN-14may be removed, and the INSTRUMENT LIGHTS 2 circuit may then be used for another function, with suitable labeling.

LK44E

J1

g

h

P1G12132-4-05

G12132-4-06g

h

16ga.G12132-4-12

LK1E

LK2E

C

D

C

D

G12132-4-11

ESN-15

1

2

3

4

5

6

MS24524-23

G12132-4-09

J2P2

ESN-14

MS24524-23

INSTRUMENT LIGHTS 2

1

2

3

4

5

6

G12132-4-07

G12132-4-08

16ga.

PP6 INST. LTS-2

10A

EFN-75

INST. LTS-1

EFN-43AN16ga.

16ga.

PP5

10A

ref: WDM 33.10.00



POSITION LIGHTSESN-10

1

2

3

4

5

6

MS24524-23

ESN-17TAXI LIGHT

1

2

3

4

5

6

MS24524-23

ref: WDM 33.43.00

(Double pole switch used for current rating.)

LM2E

P2

G

LJ1E

P2

B

ref: WDM 33.41.00


J2

G

G12132-4-16

G12132-4-15

EFN-79

7.5A

PP6

J2

B

TAXI LIGHT

PP6

G12132-4-13

G12132-4-14 EFN-87

POSITION LTS

7.5A

CHANGED LANDING LIGHT CIRCUITRELABELED CONNECTORS

A 04/22/00 GLHUPDATED INFOB 08/16/00 GLHDIMMER CONTROLADDED OPTIONAL WIRING TOC 06/06/02 GLH

ADDED OPTIONAL CIRCUIT FORLANDING / PULSE LIGHT

D 09/02/03 GLH

E REFORMATTED; UPDATED INFO 10/10/07 RBH

G12132-4 E

LIGHTING CIRCUITSP132 and P122 CONSOLE WIRING

GLH 03/30/00

GLH 03/30/00

GA107 1

G12132-4-04

G12132-4-01AN16ga.

The original LANDING LIGHT circuit MUST be rewired to match this diagram. The diode is optional.

LM1E40L or 118L

LM7ELM6E-1

LM6EAN16ga.

ZY

J2

YZ

P2LANDING LIGHTPP9

20A

EFN-95

This LANDING LIGHT switch circuit is optional, at the installer's discretion. Another switch and location may be substituted for the switch and location specified, with appropriate labeling. If an alternate location is used for the LANDING LIGHT switch, then the switch and position specified here may be used for another circuit, with appropriate labeling.

The landing light switch can be located on the Pilot's Collective Grip if desired.

To Landing Light switch, closure to ground. Installer's discretion.

G12132-4-03p p

q q

J1 P1

LM5NE

ref: WDM 33.43.00

Wires LM1E and LM5NE may be 16 ga. and need to have strands trimmed off in order to fit into the connector.

G12132-23-01 18ga

G12132-23-01 18gaADDED AIRCRAFT VERSION NOTE

MS24524-21

ALL / TAIL

To optional Strobe unit L

P2

The STROBE LIGHT switch circuit is optional and is usually used for additional strobe lights. If no additional strobe light is installed, the switch may be replaced with an MS24523-23, and wires G12132-4-19 and G12132-4-21 may be deleted and G12132-4-20 routed from the breaker to the connector.

ref: WDM 33.41.00STROBE LIGHT

G12132-4-197.5A

EFN-45 G12132-4-20

PP5

L

J2

1

2

3

4

5

6

G12132-4-17

(Center off)

G12132-4-21

ESN-9PP6

1LX10E HG12132-4-18

H

EFN-83

ANTI-COL LT

ref: WDM 33.42.00

7.5A

ANTI-COLLISION LIGHT

G12132-4-023

2

1

MS24523-23

LANDING LIGHTESN-18

MOVED PULSE LIGHT OFF PAGE




CARGO HOOK

ref: WDM 30.42.00

W/S WIPER-1

EFN-91

G12132-5-15

G12132-5-16

AVIONICS MASTER

ref: WDM 30.30.00

SEE G12132-16 FOR SAMPLE OPTIONAL CIRCUITS

G12132-5-11

The OP-x switches and wiring are optional. If they are installed, they must be labeled to show their function.

1

2

3

4

5

6

MS24524-23

W

VG12132-5-13

G12132-5-12

W

V

FN1E

T

U

P2

AN16gaT

U

J2

G12132-5-10AN16ga

AA

J2P2

AN16ga

AN16ga

K

J

K

J

OP-1

MK1E Blue G12132-5-14MM

MS24523-23

3

2

1

ESN-2FUEL PUMP 1

PP5ESN-13

3

2

1

MS24523-23

J2P2

G12132-5-04

G12132-5-03

(ref: 21Q) QN1E

PITOT HEAT

ref: WDM 28.00.00

MS24523-23

MK1E White

EFN-39

PITOT HEAT

7.5A

DD

J1P1

DD

PP93

2

1

G12132-5-17

G12132-5-18

P

J2

P

P2

7.5A

W/S WIPERESN-24

FUEL PUMP-1

G12132-5-01

G12132-5-02

PP6

7.5A

EFN-67

G12132-5-09

ref: WDM 71.61.10

SWITCH CURRENT RATINGS:MS24523-23: Resistive: 20A, Inductive: 15A, Lamp: 5AMS24524-23: Resistive: 20A, Inductive: 15A, Lamp: 7A

KS2E

3

2

1

MS24523-23

OP-2

yy

G12132-5-07

G12132-5-19

KS3E

G12132-5-21

P1 J1

1

2

3

4

5

6

G12132-5-22

J1

x

P1

x

HH

GG

HH

GG

MS24524-23

G12132-5-08

Installer Defined

SAND FILTERESN-21

BB

CC

FF

BB

CC

FF

P1

EE

J1

EE

EFN-66

G12132-5-20

PP6

G12132-5-06

G12132-5-05

SAND FILTER

FUEL PUMP 2OP-3

1

2

3

4

5

6

MS24524-23


AB

GLH04/22/00GLH08/16/00

2.5A

(From EFN-68 Fuel Pump 2 breaker, wire G12132-5-23) P1:AA

Aircraft with only one Fuel Pump may use this entire circuit for another function.If used for something other than FUEL PUMP 2, the switch will be referred to on the documentation as OP-3, and must also be labeled to identify its use.

(ref: 34Q) QN8E

ref: WDM 28.00.00

G12132-5 C


GLH 03/30/00

GLH 03/30/00

GA107 1

UPDATED FORMAT, COMPANY INFOREPLACED P102 WITH P122 DATAADDED AIRCRAFT VERSION NOTE

C 10/10/07 RBH

On aircraft with only one fuel pump, this switch and breaker may be labeled FUEL PUMP with no number


Installer Defined

Installer Defined

Installer Defined

Installer Defined

Installer Defined

Installer Defined

Installer DefinedInstaller Defined

Installer Defined


D3:C

D3:Aref: WDM 62.30.00EFN-38

PITOT HEAT

Detailed on G12132-5PP5

7.5A

EFN-39

G12132-6-03P1

A

J1

A

HYDRAULICS

WARNING PANELref: WDM 39.00.00ref: WDM 31.50.00

ref: WDM 39.00.00

WW1E and WW1F

Detailed on G12132-3

G12132-6-022.5A

PP5

G12132-6-01

EFN-37

E

P2

E

J2

7.5A

PP5

7.5A

EFN-36

PP5


PP5

PP5

10A

EFN-43


ref: WDM 77.00.00ref: WDM 39.00.00

vv

INST. LTS-1

7.5A

EFN-42

P1 J1

T4 INDICATOR

G12132-6-05

PP5

PP5

ref: WDM 62.30.00ref: WDM 39.00.00

EFN-41

D

P1 J1

D

ref: WDM 25.80.00ref: G12132-17

Installer Defined

P1

t

EFN-40

t

J1

HOOK REL

2.5A

G12132-6-04

G12132-6-06

UPDATED INFOMOVED B3 DATA OFF PAGE

REPLACED P102 WITH P122 DATAUPDATED FORMAT, COMPANY INFO

RELABELED CONNECTORSAB

C

04/22/00 GLH

10/10/07

08/16/00

RBH

GLH

ref: WDM 77.00.00

ref: WDM 77.00.00

G12132-6 C

CIRCUIT BREAKER DETAILSP132 and P122 CONSOLE WIRING

GLH 03/30/00

GLH 03/30/00

GA107 1

NG INDICATORB2ROTOR TACH(all others)

EU29EEU3E

VERSION WIRE #

WIRE #

EW15EEW15EOVERSPEED

BLEED VALVEDB1

VERSION7.5A

ROTOR TACHB2 EU3E

EC5E or EC10E

Effectivity: AS350D, D1, B, BA, B1, and B2 predating mod 350A07-3273ADDED AIRCRAFT VERSION NOTE

2.5A2.5A

4

4

5

5

6

6

LABEL

RATINGLABEL



UPDATED FORMAT, COMPANY INFO

Installer Defined

(F8E)

ATTITUDE GYRO

HOIST RELEASE

Wire power directly to Attitude Gyro, or optionally wire power through an On/Off switch.

MOVED B3 DATA OFF PAGE

REPLACED P102 WITH P122 DATAADDED AIRCRAFT VERSION NOTE


C

BA

ref: WDM 39.00.00

ref: WDM 39.00.00ref: WDM 25.63.00ref: G12132-18

ref: WDM 34.20.00

uu G12132-7-05

RBH10/10/07

04/22/0008/16/00 GLH

GLH

AN16ga.

For optional uses, this breaker may be up to 15 amps.

PP5

2.5A

EFN-49

P1 J1

PP5

G12132-7-04N

P2

N

J2

2.5A

EFN-48

EZ1E

ENG. INST-1

STROBE LIGHT



EFN-46

G12132-7-03P1

s

J1

s

PP5

G12132-7-022.5A

D2:C

D2:A

PP5

EFN-45

7.5A

ref: G12132-18

G12132-7 D


GLH 03/30/00

GLH 03/30/00

GA107 1

G12132-7-01

G12132-7-09

ME2E or ME87E w w

RATING

ref: WDM 25.80.00ref: WDM 39.00.00

300lb450lb

CAPACITY 7

2.5A7.5A

EXT. LOAD

J1P1

EFN-58

2.5A

PP6

Installer Defined

7

FF

J2P2

EFN-57


AN16ga.

G12132-7-08

G12132-7-07

G12132-7-06

ref: WDM 25.63.00

ref: WDM 77.00.00ref: WDM 39.00.00

ref: WDM 39.00.00HOIST

EF1E

PP9

J1

EE

P1

TORQUE PP6

EFN-56

2.5A

ref: WDM 39.00.00

ref: WDM 79.00.00ref: WDM 77.00.00

ENG. INST-2

EZ2E

J1

KK

P1

EFN-55

2.5A

PP6

D4:C


D4:A

WIRES FROM EFN-57 TABLEREMOVED ERRONEOUS AIRFRAME D 03/04/10 RBH


ref: WDM 28.41.10

Installer defined

ref: WDM 39.00.00ref: WDM 30.42.00


EFN-62

7.5A

P2

Q

W/S WIPER 2

G12132-8-04J2

Q

PP6

AN16ga

2.5A

EFN-61

r

P1G12132-8-03

r

J1

ref: WDM 39.00.00

ref: WDM 39.00.00ref: WDM 28.00.00

ref: WDM 62.30.00ref: WDM 39.00.00

G12132-8-01

FUEL FLOW

QW1E C

P1

PP6

G12132-8-02C

J1

2.5A

EFN-60

FUEL GAUGE

B

PP6

B

ROTOR WARN

EFN-59

2.5A

P1 J1

PP6


PP6


ref: WDM 39.00.00ref: WDM 25.92.00

SAND FILTER

EFN-66

2.5A

J1P1

i i

2.5A

EFN-65

G12132-8-06

PP6

PP6

PP6

ref: WDM 77.00.00ref: WDM 39.00.00

SPRAYING

L

P1

L

J1

EFN-64

2.5A


CRANK

2.5A

EFN-63

G12132-8-05

G12132-8 C


GLH 03/30/00

GLH 03/30/00

GA107 1

UPDATED INFO

ADDED AIRCRAFT VERSION NOTEREPLACED P102 WITH P122 DATAUPDATED FORMAT, COMPANY INFO


C 10/10/07

08/16/0004/22/00 GLH

GLH

RBH

REMOVED LAPD AND B3 DATA

NTL IND.

LABELNG GAUGE EU5E

WIRE #

EU26E

MR23E

EU11E

QW11E or QW38E


VERSIOND

D1,B1,B2

8

8


DT5E or DT4E


ref: WDM 31.31.00ref: WDM 39.00.00

EFN-75

PP6INST. LTS-2

10A

G12132-9-02

PP9

H

P1

H

J1

2.5A

HOUR METER

EFN-70

FUEL PUMP-1

FUEL PUMP-2ref: WDM 39.00.00ref: WDM 28.00.00


G12132-9-01P1

AA

J1

AA

PP6

7.5A

EFN-68

PP6

EFN-67

7.5A




EFN-87

POSITION LTS PP6

7.5A

EFN-83

ANTI-COL LT PP6

7.5A

G12132-9-03JLE1E J


EFN-79

7.5A

TAXI LIGHT PP6

ref: WDM 33.10.00ref: WDM 39.00.00

CABIN LIGHTS

P1

EFN-76

2.5A

J1

PP6

UPDATED INFO



C 10/10/07

08/16/0004/22/00 GLH

GLH

RBH

G12132-9 C


GLH 03/30/00

GLH 03/30/00

GA107 1

ref: G12132-5

Jumper to P1:BB


For aircraft with only one Fuel Pump, this breaker is SPARE and the wiring is Installer Defined.

MOVED B3 DATA OFF PAGE

On aircraft with only one fuel pump, this breaker may be labeled FUEL PUMP with no number



ref: WDM 25.26.00POWER OUTLET

KK4E and KK4F

ref: WDM 80.00.00ref: WDM 39.00.00

MH1E

G12132-10-04X X

10A

EFN-94

P2 J2

START PP9

AN16ga

G12132-10-03a

P2

a

J2

EFN-93

15A

PP9

AN16ga

CARGO HOOK

W/S WIPER-1

ref: WDM 25.80.00ref: WDM 39.00.00

ME1E


G12132-10-02c

P2

c

J2

EFN-92

15A

PP9

AN16ga

7.5A

EFN-91

PP9

2.5A

G12132-10-06

G12132-10-01Installer Defined

Installer Defined

ref: WDM 34.20.00EFN-N/A-2

2.5A

a

P1

DIR. GYRO

a

J1

PP6

EFN-N/A-1

G

P1

G

J1

G12132-10-05

ref: WDM 39.00.00ref: WDM 24.22.00

TURN & BANK

XU1E b

P2

PP9

b

J2

AC INVERTER

15A

EFN-97

PP9

AN16ga

Detailed on G12132-4 20A

EFN-95

LANDING LT PP9

G12132-10 C


GLH 03/30/00

GLH 03/30/00

GA107 1

UPDATED INFO



C 10/10/07

08/16/0004/22/00 GLH

GLH

RBH

ADDED EFN-95Effectivity: AS350D, D1, B, BA, B1, and B2 predating mod 350A07-3273



PP6 BUS BAR, Bottom Right

BUS BAR, Top Left

BUS BAR, Middle Left

PP9 BUS BAR, Bottom Left

PP6 BUS BAR, Middle Right

PP5 BUS BAR, Top Right

Primary Power to Circuit Breakers

PP9E

Installer Defined Option


PP6E

PP5E

ref: WDM 24.30.00

AN8ga G12132-11-03

TB6

TB5

TB4

TB3

AN8ga G12132-11-04

AN8ga G12132-11-13

AN8ga G12132-11-14

TB2

TB1

AN8ga G12132-11-02

AN8ga G12132-11-01



G12135-80-9

G12135-80-12

G12135-80-10

G12135-80-9

G12135-80-10

G12135-80-12

CLB

GLHGLH

RBH

CHANGED OVERLAY CONNECTORS

RELABELED CONNECTORSCHANGED 8ga. WIRE CONNECTIONS

UPDATED FORMAT, COMPANY INFOREPLACED P102 WITH P122 DATA

MOVED LIGHTING INFO OFF PAGE

UPDATED INFOBA

C

D

06/11/0208/16/0004/22/00

10/10/07

G12132-11 D

BUS BAR DETAILSP132 and P122 CONSOLE WIRING

GLH 03/30/00

GLH 03/30/00

GA107 1




LEFT MIDDLE BUS BAR

NOTE:The word: SPAREmarked on this diagram is used to represent a breaker or wire that is installed but not assigned.

The word: BLANKmeans that the wires are installed but not the circuit breaker.

The word: VOIDmeans that the breaker is not installed and the wires for that breaker are not installed.

NOTE:ALL WIRES ON THIS DRAWING ARE 16 ga. UNLESS SHOWN OTHERWISE.RING TERMINALS FOR CIRCUIT BREAKERS ARE RED #6 (p/n 36152), EXCEPT FOR DUAL WIRES WHICH HAVE BOTH WIRES CRIMPED INTO ONE BLUE #6 RING TERMINAL (p/n 326882 or 36158).

NOTE:THE CIRCUIT BREAKER CURRENT RATINGS AND NAMES SHOWN ARE JUST AN EXAMPLE. ALL WIRES ARE SUITABLE FOR 15A BREAKERS, OR LESS.

PP

LTB-BUSVOID

LTB-1

2.5A G12132-12-19

G12132-12-20

LTB-BUS

LTB-BUSVOID

2.5A

LTB-2

2.5A

LTB-3

VOID

G12132-12-18

G12132-12-17

LTB-BUS

LTB-BUS

LTB-5

2.5A

LTB-4

VOID

5A

LTB-6VOID

G12132-12-16

G12132-12-14

G12132-12-15

??? = Installer Defined

???

???

VU

VU

???

???

T T

S S

???

???

???

R R

Q Q

VOID LTB-BUS

G12132-12-095A

LTB-BUS

LTB-BUS

5A

LTB-7

5A

VOID

LTB-8VOID

G12132-12-13

G12132-12-12

G12132-12-11

G12132-12-10

LTB-BUS

LTB-BUSLTB-9

7.5A

VOID

LTB-10

7.5A

VOID

G12132-12-08

G12132-12-07

G12132-12-06

G12132-12-05

LTB-BUS

LTB-BUS

LTB-11

10A

VOIDLTB-12

10A

VOID

G12132-12-03

G12132-12-04

G12132-12-02

G12132-12-01

???JJ

???

???

???

???

LL

N

M

N

M

K K

???

???

???

???

HG

HG

FE

FE

AIR

CR

AFT

FW

D

???

???

???

???

CD

CD

AB

J3

AB

P3LEFT TOP BUS BAR

???5A


G12132-12-31 ???

if installed.Installer defined g g

G12132-12-26

G12132-12-27

G12132-12-28

G12132-12-29

G12132-12-30

2.5A

2.5A

LMB-2VOID

LMB-1

VOIDLMB-3

LMB-BUS

LMB-BUS

5A

VOID

5A

LMB-4

VOIDLMB-5

LMB-BUS

LMB-BUS

dd

f f

e e

???

???

cc

b b

???

???

TB4

TB5

LMB-10

G12132-12-22

G12132-12-23

G12132-12-24

G12132-12-25

LMB-BUSVOID

7.5A

VOIDLMB-6

5A

VOIDLMB-7

LMB-BUS

LMB-BUS

7.5A

7.5A

VOID

LMB-8

VOID

LMB-9LMB-BUS

LMB-BUS

Z

a a

Z

???

???

X

YY

X

???

???

LMB-BUS

LTB-BUS

G12132-12-21

(p/n: G12135-80-12)

(p/n: G12135-80-10)

7.5A

VOID LMB-BUS

8 ga. or 10ga.

8 ga. or 10ga.G12132-11-14

W

P3J3

W???

G12132-11-13 Installer defined power source

Installer defined power source

G12132-12 D

OPTIONAL CIRCUIT BREAKERSP132 and P122 CONSOLE WIRING

GLH 03/30/00

GLH 03/30/00

GA107 1

GLH

RBH

GLHGLH

MADE NOISE FILTER OPTIONAL AND 10/30/00CCHANGED CIRCUIT NAMES

ALL NEW DRAWINGUPDATED INFO

AB

04/22/0008/16/00

UPDATED FORMAT, COMPANY INFOREPLACED P102 WITH P122 DATAADDED AIRCRAFT VERSION NOTE

D 10/10/07

Effectivity: AS350D, D1, B, BA, B1, B2 predating mod 350A07-3273, and B3 predating mod 350A07-3274

OPTIONAL NOISE FILTER MAY BE ADDED TO ANY BREAKER OUTPUT. CONNECT TO WIRES USING A BLUE BUTT SPLICE

FILTER TYPE: 120 uH, DALE # IND-3

G12132-4, ESN

-15IN

ST. LTS-2

FWD

G12132-4, ESN

-17

G12132-4, ESN

-18LAN

DIN

G LIG

HT

MS24523-23

G12132-4, ESN

-10PO

SITION

LTS

MS24524-21

G12132-4, ESN

-9AN

TI-CO

L LT

MS24524-23

TAXI LIGH

T

MS24524-23

G12132-4, ESN

-14

MS24524-23

INST. LTS-1

MS24524-23

WAR

NIN

G H

OR

N

G12132-3, ESN

-12M

S24524-23

G12132-6, 25.80.00

HO

OK R

EL.

FUEL G

AUG

E2.5A, PP6, EFN

-60G

12132-8, 62.30.00

CABIN

LTS2.5A, PP6, EFN

-76

ENG

. INST-1

G12132-7, 25.63.00

HO

IST REL.

G12132-7, 34.20.00

ATTITUD

E2.5A, PP5, EFN

-49G

12132-8, 25.92.00

G12132-9, 33.10.00

G12132-4, 33.43.00

TAXI LIGH

T7.5A, PP6, EFN

-79

G12132-4, 33.42.00

ANTI-C

OL LT

7.5A, PP6, EFN-83

POSITIO

N LT

7.5A, PP6, EFN-87

G12132-10, 34.20.00

DIR

. GYR

O2.5A, PP6, EFN

-N/A-2

G12132-4, 33.41.00

2.5A, PP6, EFN-63

G12132-8, 30.42.00

SPRAYIN

G2.5A, PP6, EFN

-65G

12132-8, 77.00.00SPAR

E2.5A, PP6, EFN

-64G

12132-3, 80.00.00C

RAN

K

W/S W

IPER-2

FUEL FLO

W

G12132-8, 28.41.10

7.5A, PP6, EFN-62

2.5A, PP6, EFN-61

G12132-8, 28.00.00

G12132-4, 33.10.00

INST. LTS-1

2.5A, PP5, EFN-46

G12132-7, 79.00.00

2.5A, PP5, EFN-48

G12132-4, 33.41.00

STRO

BE LT7.5A, PP5, EFN

-45

G12132-6, 77.00.00

SPARE

7.5A, PP5, EFN-42

G12132-6, 77.00.00

10A, PP5, EFN-43

SPARE

2.5A, PP5, EFN-41

SAND

FILTER

FUEL PU

MP

G12132-9, 28.00.00

SPARE

G12132-4, 33.10.00

INST. LTS-2

10A, PP6, EFN-75

2.5A, PP6, EFN-56

G12132-7, 79.00.00

ENG

. INST-2

7.5A, PP6, EFN-67

RO

TOR

WAR

N

G12132-5, 28.00.00

7.5A, PP6, EFN-68

EXT. LOAD

2.5A, PP6, EFN-58

2.5A, PP6, EFN-59

G12132-7, 25.80.00

G12132-7, 77.00.00

TOR

QU

E

G12132-5, 71.61.10

2.5A, PP6, EFN-66

2.5A, PP6, EFN-55

WAR

N PAN

EL7.5A, PP5, EFN

-37

G12132-6, 31.50.00

G12132-6, 62.30.00

RO

TOR

TACH

2.5A, PP5, EFN-38

G12132-5, 30.30.00

PITOT H

EAT7.5A, PP5, EFN

-39

2.5A, PP5, EFN-40

G12132-3, 29.00.00

HYD

RAU

LICS

7.5A, PP5, EFN-36


G12132-13-B --

CONSOLE BREAKER LAYOUTP132 RIGHT SIDE VIEW for AS350B

GA107 1

RBH 10/10/07

RBH 10/10/07

GA 10/10/07

CLB 10/10/07

Effectivity: AS350B, BA

G12132-4, ESN

-15IN

ST. LTS-2

FWD

G12132-4, ESN

-17

G12132-4, ESN

-18LAN

DIN

G LIG

HT

MS24523-23

G12132-4, ESN

-10PO

SITION

LTS

MS24524-21

G12132-4, ESN

-9AN

TI-CO

L LT

MS24524-23

TAXI LIGH

T

MS24524-23

G12132-4, ESN

-14

MS24524-23

INST. LTS-1

MS24524-23

WAR

NIN

G H

OR

N

G12132-3, ESN

-12M

S24524-23

G12132-6, 25.80.00

HO

OK R

EL.

FUEL G

AUG

E2.5A, PP6, EFN

-60G

12132-8, 62.30.00

CABIN

LTS2.5A, PP6, EFN

-76

ENG

. INST-1

G12132-7, 25.63.00

HO

IST REL.

G12132-7, 34.20.00

ATTITUD

E2.5A, PP5, EFN

-49G

12132-8, 25.92.00

G12132-9, 33.10.00

G12132-4, 33.43.00

TAXI LIGH

T7.5A, PP6, EFN

-79

G12132-4, 33.42.00

ANTI-C

OL LT

7.5A, PP6, EFN-83

POSITIO

N LT

7.5A, PP6, EFN-87

G12132-10, 34.20.00

DIR

. GYR

O2.5A, PP6, EFN

-N/A-2

G12132-4, 33.41.00

2.5A, PP6, EFN-63

G12132-8, 30.42.00

SPRAYIN

G2.5A, PP6, EFN

-65G

12132-8, 77.00.00N

TL IND

.2.5A, PP6, EFN

-64G

12132-3, 80.00.00C

RAN

K

W/S W

IPER-2

FUEL FLO

W

G12132-8, 28.41.10

7.5A, PP6, EFN-62

2.5A, PP6, EFN-61

G12132-8, 28.00.00

G12132-4, 33.10.00

INST. LTS-1

2.5A, PP5, EFN-46

G12132-7, 79.00.00

2.5A, PP5, EFN-48

G12132-4, 33.41.00

STRO

BE LT7.5A, PP5, EFN

-45

G12132-6, 77.00.00

T4 IND

.7.5A, PP5, EFN

-42

G12132-6, 77.00.00

10A, PP5, EFN-43

BLEED VALVE

2.5A, PP5, EFN-41

SAND

FILTER

FUEL PU

MP-1

G12132-9, 28.00.00

FUEL PU

MP-2

G12132-4, 33.10.00

INST. LTS-2

10A, PP6, EFN-75

2.5A, PP6, EFN-56

G12132-7, 79.00.00

ENG

. INST-2

7.5A, PP6, EFN-67

RO

TOR

WAR

N

G12132-5, 28.00.00

7.5A, PP6, EFN-68

EXT. LOAD

2.5A, PP6, EFN-58

2.5A, PP6, EFN-59

G12132-7, 25.80.00

G12132-7, 77.00.00

TOR

QU

E

G12132-5, 71.61.10

2.5A, PP6, EFN-66

2.5A, PP6, EFN-55

WAR

N PAN

EL7.5A, PP5, EFN

-37

G12132-6, 31.50.00

G12132-6, 62.30.00

RO

TOR

TACH

2.5A, PP5, EFN-38

G12132-5, 30.30.00

PITOT H

EAT7.5A, PP5, EFN

-39

2.5A, PP5, EFN-40

G12132-3, 29.00.00

HYD

RAU

LICS

7.5A, PP5, EFN-36


G12132-13-B1 --

CONSOLE BREAKER LAYOUTP132 RIGHT SIDE VIEW for AS350B1

GA107 1

RBH 10/10/07

RBH 10/10/07

GA 10/10/07

CLB 10/10/07

Effectivity: AS350B1

2.5A, PP5, EFN-49

G12132-7

2.5A, PP5, EFN-46

2.5A, PP5, EFN-48

G12132-7

HOIST REL.G12132-7

ENG. INST-12.5A, PP6, EFN-65

SPRAYINGG12132-8

ATTITUDE

2.5A, PP6, EFN-N/A-2

DIR. GYROG12132-10

G12132-4POSITION LTS7.5A, PP6, EFN-87

7.5A, PP6, EFN-83

ANTI-COL LTG12132-4

G12132-4

7.5A, PP6, EFN-79

TAXI LIGHT

CABIN LTSG12132-9

2.5A, PP6, EFN-76

10A, PP6, EFN-75

INST. LTS-2G12132-4

7.5A, PP6, EFN-67

G12132-9

7.5A, PP6, EFN-68

G12132-5

FUEL PUMP-2

FUEL PUMP-1

2.5A, PP6, EFN-66

G12132-5SAND FILTER

STROBE LT

G12132-4

BLEED VALVEG12132-6

G12132-6

7.5A, PP5, EFN-42

T4 INDICAT.

INST. LTS-1

G12132-6

PITOT HEATG12132-5

HOOK REL.

CRANK

G12132-8

G12132-3

2.5A, PP6, EFN-64

NTL IND.

7.5A, PP6, EFN-62

W/S WIPER-2G12132-8

2.5A, PP6, EFN-63

G12132-4

7.5A, PP5, EFN-45

10A, PP5, EFN-43

G12132-8

G12132-8

2.5A, PP6, EFN-61

FUEL FLOW

FUEL GAUGE

2.5A, PP6, EFN-59

ROTOR WARNG12132-8

2.5A, PP6, EFN-60

2.5A, PP5, EFN-41

2.5A, PP5, EFN-40

7.5A, PP5, EFN-39

HYDRAULICSG12132-3

G12132-6

WARN PANELG12132-6

G12132-7

TORQUEG12132-7

2.5A, PP6, EFN-58

EXT. LOAD

2.5A, PP6, EFN-55

ENG. INST-2G12132-7

2.5A, PP6, EFN-56

2.5A, PP5, EFN-38

ROTOR TACH

7.5A, PP5, EFN-37

7.5A, PP5, EFN-36

FWD


G12132-13-B1-P122 --


GA107 1

RBH 10/10/07

RBH 10/10/07

GA 10/10/07

CLB 10/10/07

71.61.10 79.00.00 29.00.00

28.00.00 77.00.00 31.50.00

28.00.00 25.80.00 62.30.00

33.10.00 62.30.00 30.30.00

33.10.00 28.00.00 25.80.00

33.43.00 28.41.10 77.00.00

33.42.00 30.42.00 77.00.00

33.41.00 80.00.00 33.10.00

34.20.00 77.00.00 33.41.00

25.92.00 79.00.00

25.63.00

34.20.00

Effectivity: AS350B1

G12132-4, ESN

-15IN

ST. LTS-2

FWD

G12132-4, ESN

-17

G12132-4, ESN

-18LAN

DIN

G LIG

HT

MS24523-23

G12132-4, ESN

-10PO

SITION

LTS

MS24524-21

G12132-4, ESN

-9AN

TI-CO

L LT

MS24524-23

TAXI LIGH

T

MS24524-23

G12132-4, ESN

-14

MS24524-23

INST. LTS-1

MS24524-23

WAR

NIN

G H

OR

N

G12132-3, ESN

-12M

S24524-23

G12132-6, 25.80.00

HO

OK R

EL.

FUEL G

AUG

E2.5A, PP6, EFN

-60G

12132-8, 62.30.00

CABIN

LTS2.5A, PP6, EFN

-76

ENG

. INST-1

G12132-7, 25.63.00

HO

IST REL.

G12132-7, 34.20.00

ATTITUD

E2.5A, PP5, EFN

-49G

12132-8, 25.92.00

G12132-9, 33.10.00

G12132-4, 33.43.00

TAXI LIGH

T7.5A, PP6, EFN

-79

G12132-4, 33.42.00

ANTI-C

OL LT

7.5A, PP6, EFN-83

POSITIO

N LT

7.5A, PP6, EFN-87

G12132-10, 34.20.00

DIR

. GYR

O2.5A, PP6, EFN

-N/A-2

G12132-4, 33.41.00

2.5A, PP6, EFN-63

G12132-8, 30.42.00

SPRAYIN

G2.5A, PP6, EFN

-65G

12132-8, 77.00.00N

TL IND

.2.5A, PP6, EFN

-64G

12132-3, 80.00.00C

RAN

K

W/S W

IPER-2

FUEL FLO

W

G12132-8, 28.41.10

7.5A, PP6, EFN-62

2.5A, PP6, EFN-61

G12132-8, 28.00.00

G12132-4, 33.10.00

INST. LTS-1

2.5A, PP5, EFN-46

G12132-7, 79.00.00

2.5A, PP5, EFN-48

G12132-4, 33.41.00

STRO

BE LT7.5A, PP5, EFN

-45

G12132-6, 62.30.00

T4 IND

.7.5A, PP5, EFN

-42

G12132-6, 77.00.00

10A, PP5, EFN-43

RO

TOR

TACH

2.5A, PP5, EFN-41

SAND

FILTER

FUEL PU

MP-1

G12132-9, 28.00.00

FUEL PU

MP-2

G12132-4, 33.10.00

INST. LTS-2

10A, PP6, EFN-75

2.5A, PP6, EFN-56

G12132-7, 79.00.00

ENG

. INST-2

7.5A, PP6, EFN-67

RO

TOR

WAR

N

G12132-5, 28.00.00

7.5A, PP6, EFN-68

EXT. LOAD

2.5A, PP6, EFN-58

2.5A, PP6, EFN-59

G12132-7, 25.80.00

G12132-7, 77.00.00

TOR

QU

E

G12132-5, 71.61.10

2.5A, PP6, EFN-66

2.5A, PP6, EFN-55

WAR

N PAN

EL7.5A, PP5, EFN

-37

G12132-6, 31.50.00

G12132-6, 77.00.00

NG

IND

.2.5A, PP5, EFN

-38

G12132-5, 30.30.00

PITOT H

EAT7.5A, PP5, EFN

-39

2.5A, PP5, EFN-40

G12132-3, 29.00.00

HYD

RAU

LICS

7.5A, PP5, EFN-36


REFERENCE TO EARLIER MODELS

REFORMATTED; RE-LABELEDB RBH10/10/07EFN-38, EFN-41, EFN-64; REMOVED

G12132-13-B2 B


GA107 1

GLH 04/16/00

GLH 04/16/00

GLH 04/16/00

GLH 04/16/00

Effectivity: AS350B2 predating mod 350A07-3273

2.5A, PP5, EFN-49

G12132-7

2.5A, PP5, EFN-46

2.5A, PP5, EFN-48

G12132-7

HOIST REL.G12132-7


SPRAYINGG12132-8

ATTITUDE


DIR. GYROG12132-10


7.5A, PP6, EFN-83

ANTI-COL LTG12132-4

G12132-4

7.5A, PP6, EFN-79

TAXI LIGHT

CABIN LTSG12132-9

2.5A, PP6, EFN-76

10A, PP6, EFN-75

INST. LTS-2G12132-4

7.5A, PP6, EFN-67

G12132-9

7.5A, PP6, EFN-68

G12132-5

FUEL PUMP-2

FUEL PUMP-1

2.5A, PP6, EFN-66

G12132-5SAND FILTER

STROBE LT

G12132-4

ROTOR TACHG12132-6

G12132-6

7.5A, PP5, EFN-42

T4 INDICAT.

INST. LTS-1

G12132-6

PITOT HEATG12132-5

HOOK REL.

CRANK

G12132-8

G12132-3

2.5A, PP6, EFN-64

NTL IND.

7.5A, PP6, EFN-62

W/S WIPER-2G12132-8

2.5A, PP6, EFN-63

G12132-4

7.5A, PP5, EFN-45

10A, PP5, EFN-43

G12132-8

G12132-8

2.5A, PP6, EFN-61

FUEL FLOW

FUEL GAUGE

2.5A, PP6, EFN-59

ROTOR WARNG12132-8

2.5A, PP6, EFN-60

2.5A, PP5, EFN-41

2.5A, PP5, EFN-40

7.5A, PP5, EFN-39

HYDRAULICSG12132-3

G12132-6

WARN PANELG12132-6

G12132-7

TORQUEG12132-7

2.5A, PP6, EFN-58

EXT. LOAD

2.5A, PP6, EFN-55

ENG. INST-2G12132-7

2.5A, PP6, EFN-56

2.5A, PP5, EFN-38

NG IND.

7.5A, PP5, EFN-37

7.5A, PP5, EFN-36

FWD


FOR EFN-38, EFN-64, EFN-67, EFN-87REFORMATTED; CHANGED LABELSA RBH10/10/07

G12132-13-B2-P122 A


GA107 1

CLB 01/13/03

CLB 01/13/03

CLB 01/13/03

CLB 01/13/03

71.61.10 79.00.00 29.00.00

28.00.00 77.00.00 31.50.00

28.00.00 25.80.00 77.00.00

33.10.00 62.30.00 30.30.00

33.10.00 28.00.00 25.80.00

33.43.00 28.41.10 62.30.00

33.42.00 30.42.00 77.00.00

33.41.00 80.00.00 33.10.00

34.20.00 77.00.00 33.41.00

25.92.00 79.00.00

25.63.00

34.20.00

Effectivity: AS350B2 predating mod 350A07-3273

2.5A, PP5, EFN-49

G12132-7

2.5A, PP5, EFN-46

2.5A, PP5, EFN-48

G12132-7

HOIST REL.G12132-7


SPRAYINGG12132-8

ATTITUDE


DIR. GYROG12132-10


7.5A, PP6, EFN-83

ANTI-COL LTG12132-4

G12132-4

7.5A, PP6, EFN-79

TAXI LIGHT

CABIN LTSG12132-9

2.5A, PP6, EFN-76

10A, PP6, EFN-75

INST. LTS-2G12132-4

7.5A, PP6, EFN-67

G12132-9

7.5A, PP6, EFN-68

G12132-5

SPARE

FUEL PUMP

2.5A, PP6, EFN-66

G12132-5SAND FILTER

STROBE LT

G12132-4

SPAREG12132-6

G12132-6

7.5A, PP5, EFN-42

SPARE

INST. LTS-1

G12132-6

PITOT HEATG12132-5

HOOK REL.

CRANK

G12132-8

G12132-3

2.5A, PP6, EFN-64

SPARE

7.5A, PP6, EFN-62

W/S WIPER-2G12132-8

2.5A, PP6, EFN-63

G12132-4

7.5A, PP5, EFN-45

10A, PP5, EFN-43

G12132-8

G12132-8

2.5A, PP6, EFN-61

FUEL FLOW

FUEL GAUGE

2.5A, PP6, EFN-59

ROTOR WARNG12132-8

2.5A, PP6, EFN-60

2.5A, PP5, EFN-41

2.5A, PP5, EFN-40

7.5A, PP5, EFN-39

HYDRAULICSG12132-3

G12132-6

WARN PANELG12132-6

G12132-7

TORQUEG12132-7

2.5A, PP6, EFN-58

EXT. LOAD

2.5A, PP6, EFN-55

ENG. INST-2G12132-7

2.5A, PP6, EFN-56

2.5A, PP5, EFN-38

ROTOR TACH

7.5A, PP5, EFN-37

7.5A, PP5, EFN-36

FWD


G12132-13-B-P122 --

CONSOLE BREAKER LAYOUTP122 RIGHT SIDE VIEW for AS350B

GA107 1

RBH 10/10/07

RBH 10/10/07

GA 10/10/07

CLB 10/10/07

71.61.10 79.00.00 29.00.00

28.00.00 77.00.00 31.50.00

28.00.00 25.80.00 62.30.00

33.10.00 62.30.00 30.30.00

33.10.00 28.00.00 25.80.00

33.43.00 28.41.10 77.00.00

33.42.00 30.42.00 77.00.00

33.41.00 80.00.00 33.10.00

34.20.00 77.00.00 33.41.00

25.92.00 79.00.00

25.63.00

34.20.00

Effectivity: AS350B, BA

G12132-4, ESN

-15IN

ST. LTS-2

FWD

G12132-4, ESN

-17

G12132-4, ESN

-18LAN

DIN

G LIG

HT

MS24523-23

G12132-4, ESN

-10PO

SITION

LTS

MS24524-21

G12132-4, ESN

-9AN

TI-CO

L LT

MS24524-23

TAXI LIGH

T

MS24524-23

G12132-4, ESN

-14

MS24524-23

INST. LTS-1

MS24524-23

WAR

NIN

G H

OR

N

G12132-3, ESN

-12M

S24524-23

G12132-6, 25.80.00

HO

OK R

EL.

FUEL G

AUG

E2.5A, PP6, EFN

-60G

12132-8, 62.30.00

CABIN

LTS2.5A, PP6, EFN

-76

ENG

. INST-1

G12132-7, 25.63.00

HO

IST REL.

G12132-7, 34.20.00

ATTITUD

E2.5A, PP5, EFN

-49G

12132-8, 25.92.00

G12132-9, 33.10.00

G12132-4, 33.43.00

TAXI LIGH

T7.5A, PP6, EFN

-79

G12132-4, 33.42.00

ANTI-C

OL LT

7.5A, PP6, EFN-83

POSITIO

N LT

7.5A, PP6, EFN-87

G12132-10, 34.20.00

DIR

. GYR

O2.5A, PP6, EFN

-N/A-2

G12132-4, 33.41.00

2.5A, PP6, EFN-63

G12132-8, 30.42.00

SPRAYIN

G2.5A, PP6, EFN

-65G

12132-8, 77.00.00N

G G

AUG

E2.5A, PP6, EFN

-64G

12132-3, 80.00.00C

RAN

K

W/S W

IPER-2

FUEL FLO

W

G12132-8, 28.41.10

7.5A, PP6, EFN-62

2.5A, PP6, EFN-61

G12132-8, 28.00.00

G12132-4, 33.10.00

INST. LTS-1

2.5A, PP5, EFN-46

G12132-7, 79.00.00

2.5A, PP5, EFN-48

G12132-4, 33.41.00

STRO

BE LT7.5A, PP5, EFN

-45

G12132-6, 77.00.00

T4 IND

.7.5A, PP5, EFN

-42

G12132-6, 77.00.00

10A, PP5, EFN-43

OVER

SPEED7.5A, PP5, EFN

-41

SAND

FILTER

FUEL PU

MP

G12132-9, 28.00.00

SPARE

G12132-4, 33.10.00

INST. LTS-2

10A, PP6, EFN-75

2.5A, PP6, EFN-56

G12132-7, 79.00.00

ENG

. INST-2

7.5A, PP6, EFN-67

RO

TOR

WAR

N

G12132-5, 28.00.00

7.5A, PP6, EFN-68

EXT. LOAD

2.5A, PP6, EFN-58

2.5A, PP6, EFN-59

G12132-7, 25.80.00

G12132-7, 77.00.00

TOR

QU

E

G12132-5, 71.61.10

2.5A, PP6, EFN-66

2.5A, PP6, EFN-55

WAR

N PAN

EL7.5A, PP5, EFN

-37

G12132-6, 31.50.00

G12132-6, 62.30.00

RO

TOR

TACH

2.5A, PP5, EFN-38

G12132-5, 30.30.00

PITOT H

EAT7.5A, PP5, EFN

-39

2.5A, PP5, EFN-40

G12132-3, 29.00.00

HYD

RAU

LICS

7.5A, PP5, EFN-36


G12132-13-D --

CONSOLE BREAKER LAYOUTP132 RIGHT SIDE VIEW for AS350D

GA107 1

RBH 10/10/07

RBH 10/10/07

GA 10/10/07

CLB 10/10/07

Effectivity: AS350D

2.5A, PP5, EFN-49

G12132-7

2.5A, PP5, EFN-46

2.5A, PP5, EFN-48

G12132-7

HOIST REL.G12132-7


SPRAYINGG12132-8

ATTITUDE


DIR. GYROG12132-10


7.5A, PP6, EFN-83

ANTI-COL LTG12132-4

G12132-4

7.5A, PP6, EFN-79

TAXI LIGHT

CABIN LTSG12132-9

2.5A, PP6, EFN-76

10A, PP6, EFN-75

INST. LTS-2G12132-4

7.5A, PP6, EFN-67

G12132-9

7.5A, PP6, EFN-68

G12132-5

SPARE

FUEL PUMP

2.5A, PP6, EFN-66

G12132-5SAND FILTER

STROBE LT

G12132-4

OVERSPEEDG12132-6

G12132-6

7.5A, PP5, EFN-42

T4 IND.

INST. LTS-1

G12132-6

PITOT HEATG12132-5

HOOK REL.

CRANK

G12132-8

G12132-3

2.5A, PP6, EFN-64

NG GAUGE

7.5A, PP6, EFN-62

W/S WIPER-2G12132-8

2.5A, PP6, EFN-63

G12132-4

7.5A, PP5, EFN-45

10A, PP5, EFN-43

G12132-8

G12132-8

2.5A, PP6, EFN-61

FUEL FLOW

FUEL GAUGE

2.5A, PP6, EFN-59

ROTOR WARNG12132-8

2.5A, PP6, EFN-60

2.5A, PP5, EFN-41

2.5A, PP5, EFN-40

7.5A, PP5, EFN-39

HYDRAULICSG12132-3

G12132-6

WARN PANELG12132-6

G12132-7

TORQUEG12132-7

2.5A, PP6, EFN-58

EXT. LOAD

2.5A, PP6, EFN-55

ENG. INST-2G12132-7

2.5A, PP6, EFN-56

2.5A, PP5, EFN-38

ROTOR TACH

7.5A, PP5, EFN-37

7.5A, PP5, EFN-36

FWD


G12132-13-D-P122 --

CONSOLE BREAKER LAYOUTP122 RIGHT SIDE VIEW for AS350D

GA107 1

RBH 10/10/07

RBH 10/10/07

GA 10/10/07

CLB 10/10/07

71.61.10 79.00.00 29.00.00

28.00.00 77.00.00 31.50.00

28.00.00 25.80.00 62.30.00

33.10.00 62.30.00 30.30.00

33.10.00 28.00.00 25.80.00

33.43.00 28.41.10 77.00.00

33.42.00 30.42.00 77.00.00

33.41.00 80.00.00 33.10.00

34.20.00 77.00.00 33.41.00

25.92.00 79.00.00

25.63.00

34.20.00

Effectivity: AS350D

MS2

4524

-23

AVIO

NIC

S

FWD

Opt

iona

l

Opt

iona

lG

1213

2-10

, 25.

26.0

010

A, P

P9, E

FN-9

4ST

ART

CAR

GO

HO

OK

PWR

OU

TLET

G12

132-

5, 3

0.42

.00

W/S

WIP

ER-1

15A,

PP9

, EFN

-92

7.5A

, PP9

, EFN

-91

G12

132-

10, 2

5.80

.00

15A,

PP9

, EFN

-93

Opt

iona

l

?A, ?

bus,

LM

B-10

Opt

iona

l?A

, ?bu

s, L

MB-

8

?A, ?

bus,

LM

B-9

20A,

PP9

, EFN

-95

G12

132-

4, 3

3.43

.00

LAN

DIN

G L

T15

A, P

P9, E

FN-9

7G

1213

2-10

, 24.

22.0

0

AC IN

VER

TER

2.5A

, PP9

, EFN

-57

G12

132-

7, 2

5.63

.00

HO

IST

2.5A

, PP9

, EFN

-70

HO

UR

MET

ER2.

5A, P

P9, E

FN-N

/A-1

TUR

N &

BAN

K

G12

132-

9, 3

1.31

.00

G12

132-

10

?A, ?

bus,

LM

B-3

G12

132-

10, 8

0.00

.00

Opt

iona

l

Opt

iona

l

?A, ?

bus,

LM

B-7

?A, ?

bus,

LM

B-6

Opt

iona

l

?A, ?

bus,

LM

B-5

?A, ?

bus,

LM

B-4

Opt

iona

l

Opt

iona

l

Opt

iona

l

?A, ?

bus,

LM

B-2

?A, ?

bus,

LM

B-1

Opt

iona

l

Opt

iona

l

?A, ?

bus,

LTB

-9

Opt

iona

l

?A, ?

bus,

LTB

-12

Opt

iona

l

?A, ?

bus,

LTB

-11

Opt

iona

l

?A, ?

bus,

LTB

-10

G12

132-

2, E

SN-1

BAT-

EXT

PWR

MS2

4659

-23D

MS2

4523

-23

FUEL

PU

MP

G12

132-

5, E

SN-2

W/S

WIP

ERG

1213

2-5,

ESN

-24HO

IST

G12

132-

5, G

1213

2-18

, OP-

3

MS2

4524

-23

SAN

D F

ILTE

RG

1213

2-5,

ESN

-21

Opt

iona

l

Opt

iona

l

?A, ?

bus,

LTB

-8

Opt

iona

l

?A, ?

bus,

LTB

-7

Opt

iona

l

?A, ?

bus,

LTB

-6

?A, ?

bus,

LTB

-5

Opt

iona

l

Opt

iona

l

?A, ?

bus,

LTB

-4

?A, ?

bus,

LTB

-3

?A, ?

bus,

LTB

-1

Opt

iona

l

?A, ?

bus,

LTB

-2C

ARG

O H

OO

KG

1213

2-5,

G12

132-

17, O

P-2

MS2

4523

-23

MS2

4524

-23

MS2

4523

-23

G12

132-

5, O

P-1


G12132-14-B --

CONSOLE BREAKER LAYOUTP132 LEFT SIDE VIEW for AS350B

GA107 1

RBH 10/10/07

RBH 10/10/07

GA 10/10/07

CLB 10/10/07

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

Effectivity: AS350D, D1, B, BA

MS2

4524

-23

AVIO

NIC

S

FWD

Opt

iona

l

Opt

iona

lG

1213

2-10

, 25.

26.0

010

A, P

P9, E

FN-9

4ST

ART

CAR

GO

HO

OK

PWR

OU

TLET

G12

132-

5, 3

0.42

.00

W/S

WIP

ER-1

15A,

PP9

, EFN

-92

7.5A

, PP9

, EFN

-91

G12

132-

10, 2

5.80

.00

15A,

PP9

, EFN

-93

Opt

iona

l

?A, ?

bus,

LM

B-10

Opt

iona

l?A

, ?bu

s, L

MB-

8

?A, ?

bus,

LM

B-9

20A,

PP9

, EFN

-95

G12

132-

4, 3

3.43

.00

LAN

DIN

G L

T15

A, P

P9, E

FN-9

7G

1213

2-10

, 24.

22.0

0

AC IN

VER

TER

2.5A

, PP9

, EFN

-57

G12

132-

7, 2

5.63

.00

HO

IST

2.5A

, PP9

, EFN

-70

HO

UR

MET

ER2.

5A, P

P9, E

FN-N

/A-1

TUR

N &

BAN

K

G12

132-

9, 3

1.31

.00

G12

132-

10

?A, ?

bus,

LM

B-3

G12

132-

10, 8

0.00

.00

Opt

iona

l

Opt

iona

l

?A, ?

bus,

LM

B-7

?A, ?

bus,

LM

B-6

Opt

iona

l

?A, ?

bus,

LM

B-5

?A, ?

bus,

LM

B-4

Opt

iona

l

Opt

iona

l

Opt

iona

l

?A, ?

bus,

LM

B-2

?A, ?

bus,

LM

B-1

Opt

iona

l

Opt

iona

l

?A, ?

bus,

LTB

-9

Opt

iona

l

?A, ?

bus,

LTB

-12

Opt

iona

l

?A, ?

bus,

LTB

-11

Opt

iona

l

?A, ?

bus,

LTB

-10

G12

132-

2, E

SN-1

BAT-

EXT

PWR

MS2

4659

-23D

MS2

4523

-23

FUEL

PU

MP

1G

1213

2-5,

ESN

-2

W/S

WIP

ERG

1213

2-5,

ESN

-24

FUEL

PU

MP

2G

1213

2-5,

OP-

3

MS2

4524

-23

SAN

D F

ILTE

RG

1213

2-5,

ESN

-21

Opt

iona

l

Opt

iona

l

?A, ?

bus,

LTB

-8

Opt

iona

l

?A, ?

bus,

LTB

-7

Opt

iona

l

?A, ?

bus,

LTB

-6

?A, ?

bus,

LTB

-5

Opt

iona

l

Opt

iona

l

?A, ?

bus,

LTB

-4

?A, ?

bus,

LTB

-3

?A, ?

bus,

LTB

-1

Opt

iona

l

?A, ?

bus,

LTB

-2C

ARG

O H

OO

KG

1213

2-5,

G12

132-

17, O

P-2

MS2

4523

-23

MS2

4524

-23

MS2

4523

-23

G12

132-

5, O

P-1


G12132-14-B2 B

CONSOLE BREAKER LAYOUTP132 LEFT SIDE VIEW for AS350B2

GA107 1

GLH 04/22/00

GLH 04/22/00

GLH 04/22/00

GLH 04/22/00ESN-1; REMOVED REFERENCES TOVERSIONS PRIOR TO B1

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

B REFORMATTED; ADDED LOCK TO 10/10/07 RBH

Effectivity: AS350B2, B1

Optional?A, ?bus, LMB-1

Optional

Optional

?A, ?bus, LTB-1

?A, ?bus, LTB-2

?A, ?bus, LTB-3

Optional

?A, ?bus, LMB-4

?A, ?bus, LMB-9

Optional

?A, ?bus, LMB-8


Optional


?A, ?bus, LMB-6


Optional


Optional

Optional

?A, ?bus, LMB-3

Optional

Optional

Optional?A, ?bus, LTB-4

?A, ?bus, LTB-5

?A, ?bus, LTB-6

Optional

?A, ?bus, LTB-7

Optional

?A, ?bus, LTB-8

?A, ?bus, LTB-9

Optional

Optional

Optional

?A, ?bus, LTB-10

Optional

?A, ?bus, LTB-11

?A, ?bus, LTB-12

TURN & BANK2.5A, PP9, EFN-N/A-1

HOUR METERG12132-9

2.5A, PP9, EFN-70

G12132-7

2.5A, PP9, EFN-57

G12132-10

HOIST

15A, PP9, EFN-97

LANDING LTG12132-4

20A, PP9, EFN-95

G12132-10

10A, PP9, EFN-94

AC INVERTERG12132-10

START

7.5A, PP9, EFN-91

W/S WIPER-1G12132-5

15A, PP9, EFN-93

G12132-10

15A, PP9, EFN-92

PWR OUTLET

CARGO HOOK

G12132-10

FWD

G12132-12G12132-12

G12132-12

G12132-12

G12132-12

G12132-12

G12132-12

G12132-12

G12132-12

G12132-12

G12132-12

G12132-12

G12132-12

G12132-12

G12132-12

G12132-12

G12132-12

G12132-12

G12132-12

G12132-12

G12132-12

G12132-12


G12132-14-B2-P122 A


GA107 1

CLB 01/10/03

CLB 01/10/03

CLB 01/10/03

CLB 01/10/03A REFORMATTED 10/10/07 RBH

30.42.00

25.80.00

25.26.00

80.00.00

33.43.00

24.22.00

25.63.00

31.31.00

Effectivity: AS350D, D1, B, BA, B1, B2 Predating Mod 350A07-3273


WIPER

CARGO HOOK

SAND FILTER

G12132-5, OP-2

G12132-5, OP-1AVIONICS

MASTERAVIONICS

HOOKCARGO

G12132-5, ESN-24W/S WIPER

G12132-5, ESN-21

SANDFILTER

Effectivity: AS350B, BA, D, D1

BAT-EXT PWR

FUEL PUMPG12132-5, ESN-2

G12132-18, OP-3HOIST

WINDSHIELD

HOIST

MS24659-23D

G12132-2, ESN-1

PUMPFUEL

POWERBAT-EXT

G12

132-

5, E

SN

-13

PITO

T H

EAT

G12

132-

2, E

SN

-6

MS

2465

9-23

D

MS

2452

3-23

MA

STE

R C

UTO

FF

G12

132-

3, E

SN

-7

G12

132-

3, E

SN

-5

MS

2452

3-26

G12

132-

3, E

SN

-11

MS

2740

7-3

WA

RN

/ FI

RE

TE

ST

CR

AN

K E

NG

INE

G12

132-

3, E

SN

-3

MS

2465

8-23

D

MS

2452

4-31

GE

NE

RA

TOR

ON

HY

D T

EST

TESTWARN/FIRE

ON / RESETGENERATOR

TESTHYD

CUTOFFMASTER

ENGINECRANK PITOT

HEAT

LIGHTS

G12132-4, ESN-10POSITION LTS

ANTI-COL LTG12132-4, ESN-9

TAXI LIGHTG12132-4, ESN-17

LANDING LIGHTG12132-4, ESN-18

LANDINGLIGHT

TAXILIGHT

ANTI-COLALL / TAIL

G12132-4, ESN-15INST. LTS-2


WARNING HORNG12132-3, ESN-12

LIGHTS 2INSTRUMENT

POSITION

MS24524-23

LIGHTS 1INSTRUMENT

WARNINGHORN

MS24524-23

MS24524-23

G12132-15-B A

CONSOLE SWITCH LAYOUTP132 TOP VIEW for AS350B

GA107 1

RBH 10/10/07

RBH 10/10/07

GA 10/10/07

CLB 10/10/07

MS24523-23

MS24523-23

MS24523-23

MS24524-23

MS24523-23

MS24524-23

MS24524-23

MS24524-21

MS24524-23

MS24523-23

CHANGED ESN-7 SWITCH TYPEA RBH03/23/09


WIPER

REFORMATTED; ADDED LOCK TOESN-1; REMOVED REFERENCES TOVERSIONS PRIOR TO B1

B

CARGO HOOK

SAND FILTER

G12132-5, OP-2

G12132-5, OP-1AVIONICS

MASTERAVIONICS

HOOKCARGO

G12132-5, ESN-24W/S WIPER

G12132-5, ESN-21

SANDFILTER


10/10/07 RBH

FUEL PUMP 2

FUEL PUMP 1

BAT-EXT PWR

G12132-5, ESN-2

G12132-5, OP-3

WINDSHIELD

PUMP 2FUEL

MS24659-23D

G12132-2, ESN-1

PUMP 1FUEL

POWERBAT-EXT

G12

132-

5, E

SN

-13

PITO

T H

EAT

G12

132-

2, E

SN

-6

MS

2465

9-23

D

MS

2452

3-23

MA

STE

R C

UTO

FF

G12

132-

3, E

SN

-7

G12

132-

3, E

SN

-5

MS

2452

3-26

G12

132-

3, E

SN

-11

MS

2740

7-3

WA

RN

/ FI

RE

TE

ST

CR

AN

K E

NG

INE

G12

132-

3, E

SN

-3

MS

2465

8-23

D

MS

2452

4-31

GE

NE

RA

TOR

ON

HY

D T

EST

TESTWARN/FIRE

ON / RESETGENERATOR

TESTHYD

CUTOFFMASTER

ENGINECRANK PITOT

HEAT

LIGHTS

G12132-4, ESN-10POSITION LTS

ANTI-COL LTG12132-4, ESN-9

TAXI LIGHTG12132-4, ESN-17

LANDING LIGHTG12132-4, ESN-18

LANDINGLIGHT

TAXILIGHT

ANTI-COLALL / TAIL



WARNING HORNG12132-3, ESN-12

LIGHTS 2INSTRUMENT

POSITION

MS24524-23

LIGHTS 1INSTRUMENT

WARNINGHORN

MS24524-23

MS24524-23

MS24523-23

MS24524-23

MS24524-21

MS24524-23

MS24523-23

MS24523-23

MS24523-23

MS24524-23

MS24523-23

MS24524-23

G12132-15-B2 C

CONSOLE SWITCH LAYOUTP132 TOP VIEW for AS350B2

GA107 1

GLH 04/16/00

GLH 04/16/00

GLH 04/16/00

GLH 04/16/00

C CHANGED ESN-7 SWITCH TYPE 03/23/09 RBH


MS24523-26G12132-3, ESN-5

P122 CONSOLE LAYOUT

MS24523-23

MS24524-23G12132-4, ESN-17

G12132-5, ESN-13

G12132-4, ESN-15MS24524-23

VERSIONS PRIOR TO B1ESN-1; REMOVED REFERENCES TO REFORMATTED; ADDED LOCK TOA

MS24524-23G12132-5, OP-1

MS24524-23

AVIONICSMASTER

G12132-4, ESN-14


10/10/07 RBH

G12132-4, ESN-10MS24524-23 MS24524-21

G12132-4, ESN-9

PANELDIMMER

FUELPUMP 2

GENERATORON / RESET

MS24524-31G12132-3, ESN-3

INSTRUMENTLIGHTS 2

MS24524-23G12132-5, OP-3

MS24523-23

INSTRUMENTLIGHTS 1

G12132-5, ESN-2

FUELPUMP 1

G12132-2, ESN-1MS24659-23D

BAT-EXTPOWER

MS24658-23DG12132-3, ESN-11

G12132-5, ESN-21

POSITIONLIGHTS

MS24524-23

SANDFILTER

ANTI-COLLIGHT

G12132-5, ESN-24MS24523-23

WINDSHIELDWIPER

MS27407-3G12132-3, ESN-7

HYDRAULICTEST

WARN / FIRETEST

CARGOHOOK

G12132-4, ESN-18MS24523-23

G12132-5, OP-2MS24523-23

WARNINGHORN

MS24659-23DG12132-2, ESN-6

LANDINGLIGHT

G12132-3, ESN-12MS24524-23

TAXILIGHT

PITOTHEAT

MASTERCUTOFF

CRANKENGINE

G12132-15-B2-P122 B


GA107 1

GLH 01/10/03

GLH 01/10/03

GLH 01/10/03

GLH 01/10/03

CHANGED ESN-7 SWITCH TYPE 03/23/09 RBHB

G12132-3, ESN-5

P122 CONSOLE LAYOUT

MS24523-26

MS24523-23

MS24524-23G12132-4, ESN-17

G12132-5, ESN-13

G12132-15-B-P122 A

CONSOLE SWITCH LAYOUTP122 TOP VIEW for AS350B, BA, D, D1

GA107 1

RBH 10/10/07

RBH 10/10/07

GA 10/10/07

CLB 10/10/07


G12132-4, ESN-15MS24524-23

MS24524-23G12132-5, OP-1

AVIONICSMASTER

MS24524-23G12132-4, ESN-14

Effectivity: AS350B, BA, D, D1

G12132-4, ESN-10MS24524-23

PANELDIMMER

MS24524-21G12132-4, ESN-9

G12132-3, ESN-3

HOIST

GENERATORON / RESET

INSTRUMENTLIGHTS 2

MS24524-31

MS24524-23G12132-18, OP-3

INSTRUMENTLIGHTS 1

MS24523-23G12132-5, ESN-2

FUELPUMP

G12132-2, ESN-1MS24659-23D

BAT-EXTPOWER

MS24658-23DG12132-3, ESN-11

G12132-5, ESN-21

POSITIONLIGHTS

MS24524-23

SANDFILTER

ANTI-COLALL / TAIL

G12132-5, ESN-24MS24523-23

G12132-3, ESN-7

WINDSHIELDWIPER

MS27407-3

HYDRAULICTEST

WARN / FIRETEST

CARGOHOOK

G12132-4, ESN-18MS24523-23

G12132-5, OP-2MS24523-23

WARNINGHORN

LANDINGLIGHT

MS24659-23DG12132-2, ESN-6

G12132-3, ESN-12MS24524-23

TAXILIGHT

PITOTHEAT

MASTERCUTOFF

CRANKENGINE

A CHANGED ESN-7 SWITCH TYPE 03/23/09 RBH


MS24659-23D

G12132-5-11

AN16ga

AVIONICS MASTER

G12132-5-12

G12132-5-13

Sample AVIONICS circuit

RELAYAVIONICS

EXTERNAL TO CONSOLE

PP128 ga.50A

AVIONICSA1

UU(no connection)X1

(Airframe GND)

X2

W

V

W

V

Sample AVIONICS MASTER circuit

(no connection)

8 ga.

A2

TB4

T

P2

AN16gaT

J2

G12132-5-10

More samples on G12132-17SAMPLE OPTIONAL CIRCUITS

ALT. ENCODER

2.5A

TRANSPONDER

2.5A

AUDIO PANEL

2.5A

10A

COM2

CD CHANGER

2.5A

5A

GPS

10A

COM1 STEREO ICS

2.5A


PP9

G12132-10-05

AN16ga

AN16ga

1

2

3

4

5

6

OP-1

bb

new label: AVIONICS-1

15A

J2

EFN-97

P2

FROM G12132-10

AN16ga

PP6

G12132-8-04

AN16ga

AN16ga

G12132-5-13 AN16ga

G12132-5-12 AN16ga

G12132-5-10

QQ

P2

W W

VV

J2

U

TT

U


J2

EFN-62

P2

15A

1

2

3

4

5

6

MS24524-23

G12132-5-11

FROM G12132-8

AVIONICS MASTEROP-1

Replace existing 7.5A breaker with 15A breaker.

AN16ga

G12132-16-03AN16ga

AN16gaG12132-16-04

FROM G12132-5

G12132-16 C

AVIONICS SAMPLE CIRCUITP132 and P122 CONSOLE WIRING

GLH 03/30/00

GLH 03/30/00

GA107 1

ADDED NOTES, WIRE NUMBERSREPLACED P102 WITH P122 DATAUPDATED FORMAT, COMPANY INFO

RELABELED CONNECTORSADDED INFORMATION

AB

C

08/16/0004/22/00 GLH

GLH

10/10/07 RBH

Use existing 15A breaker.

Avionics breakers may be mounted in the Optional rails, or in an installer-defined location outside the console.

existing label: W/S WIPER 2

existing Label: AC INVERTER

AVIONICS-1 BUS

AVIONICS-2 BUS

G12132-16-01 AN16ga

G12132-16-02 AN16ga

Alternatively, separate AVIONICS-1 and AVIONICS-2 bus breakers may be mounted in the optional rails, or in an installer-defined location outside the console, and powered separately.

40

40

40


Sample CARGO HOOK circuit

ME3E

ref: WDM 25.80.00

tt

From G12132-6

G12132-17-01


ref: WDM 25.80.00ref: WDM 39.00.00 PP5

P1

EFN-40

J1

HOOK RELEASE

2.5A

G12132-6-06

3

2

1


From G12132-5

HOOK ARMED warning light.Installer shall provide suitable light and install in clear view of pilot, with appropriate label.

J2

J

K

P2

MS24523-23

J

K


CARGO HOOKOP-2

G12132-5-16

G12132-5-15


RELABELED CONNECTORSADDED ARMED LIGHT

AB

C

08/16/0004/22/00 GLH

GLH

10/10/07 RBH

G12132-17 C

CARGO HOOK SAMPLE CIRCUITP132 and P122 CONSOLE WIRING

GLH 03/30/00

GLH 03/30/00

GA107 1



SAMPLE HOIST CIRCUIT

From G12132-7

ref: WDM 25.63.00PP9

P2

F

EFN-57

F

J2

HOIST

G12132-7-09

G12132-18-02


ref: WDM 39.00.00ref: WDM 25.63.00

J2P2

N N

EFN-48

2.5A

G12132-7-04

PP5HOIST RELEASE

G12132-5-20

HOIST ARMED warning light.Installer shall provide suitable light and install in clear view of pilot, with appropriate label.


From G12132-5

ME36E

CC

BB

CC

FF

G12132-5-05

G12132-5-06BB

FF

MS24524-23

1

2

3

4

5

6


G12132-18-01J1P1

EE

G12132-5-19

EE

OP-3HOIST

ADDED AIRCRAFT VERSION NOTESREPLACED P102 WITH P122 DATAUPDATED FORMAT, COMPANY INFO

RELABELED CONNECTORSADDED ARMED LIGHT

AB

C

08/16/0004/22/00 GLH

GLH

10/10/07 RBH

G12132-18 C

HOIST SAMPLE CIRCUITP132 and P122 CONSOLE WIRING

GLH 03/30/00

GLH 03/30/00

GA107 1

450lb UNIT: ME101E 300lb UNIT: ME33E


CAPACITY

300lb 2.5A

RATING7.5A450lb

NOTE: On aircraft with two fuel pumps, OP-3 is normally assigned to the FUEL PUMP 2 function. If a HOIST circuit is needed on such an aircraft, implement it using a different optional switch, or using a switch mounted outside the console, or transfer the FUEL PUMP 2 function to another available switch.

99


1

2

3

4

5

6

MS24524-23

FLOAT ARM

G12132-5-20

G12132-21-14 AN18ga

G12132-21-15 AN18ga

G12132-21-17 AN12ga

G12132-21-18 AN12ga

INSIDE MASTER ELECTRICAL BOX

G12

132-

21-9

GAUGES; REARRANGED FOR VISUAL

AN12ga

If 3G1 and 3G2 breakers are connected through a 50A fuse or breaker, then they may be located outside the master electrical box if desired.

REFORMATTED; CORRECTED WIRE

CLARITY

E

With 50A fuse or breaker, use 10ga wire, otherwise use conductor with minimum 50,000 sq. mils. cross section.

From PP12 Bus, optionally through 50A fuse or breaker. G12132-21-33

G12132-21-7

25A

3G1

G12132-21-34

25A

3G2

AN12gaG12132-21-8

AN12ga 10A

G12132-21-21

10/10/07 RBH

X2

X1

G12132-21-6

G12132-21-22

A2

G12

132-

21-3

1A

N12

gaG

1213

2-21

-10

RELAY

A1

5G1

2.5A

8G1

G12132-21-13

G12132-21-12AN12ga

7G1

10A

4G1

A2

X2

RELAY

A1

X1

FLOAT INFLATE Switch:This switch is mounted on a bracket attached to the horizontal portion of the pilot's cyclic tube, such that the toggle points toward the ceiling and the switch key notch faces forward. To inflate the floats, the pilot can pull back on the guard and accuate the toggle in one motion. Optionally, use Switch Housing p/n G12138. Label for switch guard: FLOAT INFLATE

G12132-21-4

1

2

3

4

5

6

MS24524-23

FLOAT INFLATE SWITCH WITH REQUIREDMS25224-1 RED SWITCH GUARD

WITH FLOATS ARMED,

RAISE GUARD AND MOVE

TOGGLETO INFLATE

FLOATS.

G12132-21-5

G12132-5-06G12132-21-3

G12132-21-16

G12

132-

21-3

2

G12

132-

21-1

1

G12132-21-2

2.5A

AN

12ga

5G2

8G2

CC

BB

G12132-21-1

BB

CC G12132-5-05

J1

FF

EE

FF

EE

P1

G12132-5-19

G12

132-

21-2

4

G12132-21 G

EMERGENCY FLOATS ELECTRICALP132 and P122 CONSOLE WIRING

GLH 10/03/00

GLH 10/03/00

GA107 1

G12132-21-29 AN18ga

G12132-21-27 AN18ga

G12132-21-25

G12132-21-28

G12132-21-20 AN18ga

10A

4G2

G12132-21-26 AN18ga

G12132-21-30 AN18ga

A


E

DC

Float Connectors: PT08SE10-6S or equal

RH AERAZUR CYLINDER

LH AERAZUR CYLINDER

B

FB

CE

AD

F

AERAZUR 350/355 FLOATS, VERSION 1NOTES:All wire is AN20ga. unless otherwise noted.Wiring for switches and lights may optionally be AN22ga.Relay: Contact Rating: 20A @ 28VDC minimum. Coil Rating: 28VDC 1A maximum coil current. Coil Duty Cycle: ContinuousRecommended Relay: MS24166-D1 (#6041H200)Installer shall mount diodes securely.Circuit breakers and relays may be mounted in either tail baggage compartment, instrument panel pedestal area, or console.25A breakers may be substituted with 30A breakers.2.5A breakers may be substituted with 3A, 4A or 5A breakers.All wires connected to relay terminals A1 and A2 are AN12 gauge.

AIRFRAME GROUNDS FOR RELAYS, AND FOR FLOAT CYLINDERS, MUST BE MADE INDIVIDUALLY, NOT COMBINED

FLOATS ARMED Warning Lights:Installer shall provide suitable 28V lights, amber in color, and install lights in clear view of pilot, with appropriate label.

G12132-21-19 AN18ga

10A

7G2

FLOAT ARMSwitch location is any Console switch position. The switch position, wire labels, and console connector show here are for illustration purposes only and are optional.

OP-3

POWER DIODES MUST BE RATED AT 6A AND 50VDC MINIMUMRecommended Diode: 6A05-T (6A, 50V)

CLAMPING DIODES MUST BE RATED AT 1A AND 50VDC MINIMUM.

G12

132-

21-2

3

NEW DIODE P/N IN FLAG NOTE 2F 05/12/10 RBHREMOVED GREEN LAMP OPTIONG 02/10/11 RBH


INSTRUMENT LIGHTS 1

INSTRUMENT LIGHTS 2

3

USE #6 TERMINALS (RED CRIMP 36152)FOR CONNECTING WIRES TO TERMINAL BLOCK

PWR 1

PWR 2

1

2

DIMMER CONTROL

PWR POT

PWR OVERLAY

GND

G12301

4

5

G12132-23-09 AN20ga

1

G12301 OVERLAY DIMMER CONTROL

WIRING


4

5

1

2

ESN-14

6 3

4

5

1

2

100 OHM

ESN-15

6 3

QUICK DISCONNECT, FULLY INSULATEDFEMALE: T&B 18RA-2577MALE: T&B 18RA-251T

OVERLAY-LEFT-

OVERLAY-TOP-

OVERLAY-RIGHT-

3

2

DIMMER POT ASSEMBLYG12132-24

G12132-23-11 AN22ga

G12132-23-12 AN22ga

G12132-23-10 AN22ga

OVERLAY-LEFT+

OVERLAY-TOP+

OVERLAY-RIGHT+

G12132-23-07 AN22ga

G12132-23-08 AN22ga

G12132-23-06 AN22ga

WARN / FIRE TEST

4 1

ESN-7

5

6

2

3

ref: G12132-3 ref: G12132-4

G12132-23 C

SWITCH LEGEND LIGHTINGP132 CONSOLE WIRING

CLB 05/23/02

GLH 05/23/02

GA107 1

WIRE #'S, REMOVED "OPTIONAL"


UPDATED FORMAT, COMPANY INFOCORRECTED SWITCH NUMBERINGREMOVED BUTT SPLICES

B

A

10/10/07

11/16/06

RBH

CLB

Effectivity: AS350D, D1, B, BA, B1, B2 and B3,all versions through Mod 07.3274

ADDED ESN-7 AND REFS, UPDATED

F

F

F

M

M

M

G12132-24-01 AN22ga

G12132-24-02 AN22ga

G12132-23-02 AN18ga

G12132-23-01 AN18ga

G12132-23-14 AN22gaOPTIONAL ADDITIONAL CENTER SWITCH RAIL+F

G12132-23-13 AN22gaOPTIONAL ADDITIONAL CENTER SWITCH RAIL-M

C Changed Quick Diconnect Part Numbers 12/05/14 CLB


G12132-23-05 AN22ga

G12132-23-06 AN22ga

GND 3


PWR 1

PWR 2

1

2

DIMMER CONTROL

PWR POT

PWR OVERLAY

G12301

4

5

FM 22 GA 1

100 OHM


WIRING


OVERLAY LIGHT BOARDG12310-6-2

DIMMER POT ASSEMBLYG12132-24

MF

M

F

0.250" QUICK DISCONNECTMALE: T&B 18RA-251T

FEMALE: T&B 18RA-2577

F

M

22 GAG12132-24-02

G12132-24-01 3

2

OVERLAY -

OVERLAY +

ESN-14

ESN-15

INSTRUMENT LIGHTS 1

INSTRUMENT LIGHTS 2

G12132-23-09

ref: G12132-34 1

WARN / FIRE TEST

5

6

ESN-7

2

3

4

5

6

4

5

6

ref: G12132-41

2

3

1

2

3

G12132-23-P122 C

SWITCH LEGEND LIGHTINGP122 CONSOLE WIRING

RBH 10/10/07

CLB 10/10/07

GA107 1

Effectivity: AS350D, D1, B, BA, B1, B2 and B3,all versions through Mod 07.3274

G12132-23-02 AN18ga

G12132-23-01 AN18ga

G12132-23-03

G12132-23-04

DELETED "OPTIONAL"A RBH05/06/08REVISED P/N FOR LIGHT BOARDB CLB06/29/10

C Changed Quick Diconnect Part Numbers 12/05/14 CLB

0.250" QUICK DISCONNECTMALE: T&B 18RA-251T

FEMALE: T&B 18RA-2577



G12132-26 --

COMBINED HOIST / HOOK SWITCHP132 and P122 CONSOLE WIRING

RBH 10/10/07

CLB 10/10/07

GA107 1

MS24523-23

3

2

1

CARGO HOOK

JJ G12132-5-16

K K G12132-5-15

P2 J2

OP-2

ref: WDM 25.80.00ref: WDM 25.63.00

G12132-5-25

EE

J1

FF

CC

BB

FFME36E

CC

BB

RELEASE

EFN-48

P1

EE

2.5A

PP5

G12132-5-20

G12132-5-05

G12132-5-06

(Center OFF)MS24659-21A

1

2

3

4

5

6

HOIST / CARGO HOOK

G12132-5-19OP-3

HOIST

G12132-5-05

G12132-5-06

G12132-5-20

CC

BB

CC

BB

EE

FF

P1

EE

FF

J1

G12132-5-19

1

2

3

4

5

6

MS24524-23

OP-3

ref: AEG DWG 350A63-6159-00ref: AEG DWG 350A63-6158-00ref: AEG DWG 350A63-5017-00ref: AEG DWG 350A63-5016-00

Loop back to output pin of HOOK RELEASE breaker

To ME3E and installer provided HOOK ARMED indicator light

To ME101E or ME33E, and installer provided HOOK ARMED indicator light

Loop back to output pin of HOIST RELEASE breaker

Loop back to output pin of HOIST breaker

ME36ELoop back to output

pin of HOIST breaker

To ME101E or ME33E, and installer provided HOOK ARMED indicator light

To ME3E and installer provided HOOK ARMED indicator light

Effectivity: AS350D, D1, B, BA, B1, B2 through mod 350A07-3273, and B3 through mod 350A07-3274

STANDARD WIRINGref: G12132-17, G12132-18

Depending on the aircraft version and mod level, there may not be separate switches available for both the HOIST and CARGO HOOK functions, the on an aircraft that both.

This diagram shows how the OP-3 switch circuit may be modified to accommodate a combined HOIST and CARGO HOOK circuit. The modified circuit replaces the standard switch with a center-OFF, locking-toggle switch. The HOIST is active in the forward position, CARGO HOOK in the aft position. The diagram lists the replacement switch type.

One new wire must be routed from the RELEASE breaker to the switch. The standard wire routed from the RELEASE breaker to the connector may be disconnected, capped and stowed at the breaker end. All other changes to the switch wiring can be made at the switch. The wire number shown for the added wire is a suggestion; the installer must make sure that the actual label used does not duplicate a wire number already in use in the console.

MODIFIED WIRING

On the -073273 B2 version, the OP-3 switch is not included in the standard definition, as the FUEL PUMP 2 switch ESN-8 takes its place. On these aircraft, space must be made for the HOIST / HOOK switch in one of the following ways: (1) it may be mounted in an installer-defined location outside the console; (2) it may be mounted on the console in place of another switch whose standard function is not needed, or which has itself been moved outside the console; (3) the functions may be transferred to an available optional switch; (4) additional switch mounting may be made available. The P122 console contains provisions for mounting up to 4 switches beyond the standard set; the P132 console can be expanded by the use of additional center switch rails.

In the standard definition for older aircraft with dual Fuel Pumps, the FUEL PUMP 2 function is assigned to OP-3. For those aircraft, the FUEL PUMP 2 function may be transferred to OP-2 or another available optional switch to make OP-3 available for the combined HOIST / HOOK circuit, or a different switch may be added and designated ESN-8 for the FUEL PUMP 2 function, per the previous paragraph.

CONSOLE MODIFICATION FORCOMBINED HOIST / CARGO HOOK SWITCH



G12132-27 --

ACTIVE-OFF AVIONICS MASTERP132 and P122 CONSOLE WIRING

RBH 10/10/07

CLB 10/10/07

GA107 1

G12132-5-13 AN16ga

G12132-5-12 AN16ga

EXTERNAL TO CONSOLE

PP128 ga.

AVIONICS

50A

WW(Airframe GND)

8 ga.TB4

V

P2

V

J2

1

2

3

4

5

6

MS24524-23

AVIONICS MASTEROP-1

G12132-5-12 AN16ga

G12132-5-13 AN16ga

AVIONICSRELAY

EXTERNAL TO CONSOLE

A1

AVIONICSPP12

8 ga.50A A2

(Airframe GND)

X1

X2W

V

W

V

8 ga.TB4

P2 J2

MS24524-23

AVIONICS MASTER

1

2

3

4

5

6

OP-1

A4A3P1

G

J1

G G12132-10-06

EFN-N/A-1

MASTER RELAYPP9

7.5A

AVIONICSRELAY

A3A1

X2

X1

A2A4

NOTES:

CONSOLE MODIFICATION FOR ACTIVE-OFF AVIONICS MASTER CONTROL SWITCH

This diagram shows how the standard AVIONICS MASTER switch circuit may be modified for use as an Active-OFF Avionics Master Relay controller. In this circuit, the AVIONICS bus on TB4 is active when the relay is de-energized, such as when the bus supplying the Avionics Master Relay breaker is disabled.

The modified circuit uses the standard switch. The circuitry on the second pole of the switch is omitted for visual clarity.

All changes to the switch wiring can be made at the switch, without requiring any console wires to be re-routed.

The circuit breaker shown is for illustration only, and may be any unused breaker on any bus other than the output of the relay, or may be a breaker mounted in an installer-defined location outside the console. At the installer's discretion, the rating shown may be decreased to any available rating that will supply the required relay coil current.

SAMPLE ACTIVE-ON RELAY WIRING USING STANDARD SWITCH WIRING (ref: G12132-16)

SAMPLE ACTIVE-OFF RELAY WIRINGUSING MODIFIED SWITCH WIRING

AVIONICS

Effectivity: AS350D, D1, B, BA, B1, B2 through mod 350A07-3273, and B3 through mod 350A07-3274



G12132-28 --

PULSE LIGHT CONTROL CIRCUITSP132 and P122 CONSOLE WIRING

RBH 10/10/07

CLB 10/10/07

GA107 1 of 2

P2

To 3060S Taxi Light Power pin A6


G12132-8-04 AN16gaQ

J2

QEFN-62

7.5A

PP6

ref: AEC DWG 350A73-5881ref: WDM 33.43.00

G12132-4-03

G12132-4-023

2

1

MS24523-23

LANDING LIGHTESN-18

q q

P1J1

p p

To Airframe GND

To Landing Light relay

ESN-18

MS24524-21(Center OFF)

1

2

3

4

5

6

LANDING / PULSE LIGHTP2 J2

G12132-4-22

G12132-4-23

q q To Airframe GNDG12132-4-03 To Landing Light relay

P1G12132-4-02 p

J1

p

To 3060S Control line, pin 3

To Airframe GND

Effectivity: AS350D, D1, B, BA, B1, B2 predating mod 350A07-3273, and B3 predating mod 350A07-3274

d

e

d

e

PP6


1

2

3

4

5

6

LM2E G G

f fG12132-4-26

P2 J2

MS24524-23

ESN-17

G12132-4-16

G12132-4-15

TAXI LIGHT


TAXI LIGHT

7.5A

EFN-79

STANDARD SWITCH WIRINGref: G12132-4

new label: PULSE MAIN

MODIFIED BREAKER WIRING

MODIFIED SWITCH WIRING

CONSOLE MODIFICATION FOR PULSE LIGHT CONTROL

This diagram shows the modifications needed to power a Precise Flight 3060S pulse control module, and adapt the LANDING LIGHT switch to operate as a LANDING LIGHT / PULSE LIGHT switch.

The switch must be replaced with a DPDT center-OFF type switch, and 2 wires added to the console as shown in the Modified Switch Wiring diagram.

One circuit breaker will need to be assigned to provide power for the control circuitry, with the rating changed to 3A. (With the exception of the Taxi Light breaker EFN-79, all breakers shown are examples only.)

Power must supplied to the module separately for the lamp power supply. A wire may be added to the Taxi Light circuit to provide unswitched power directly from the breaker to the module; or, to avoid further wiring changes, an available breaker on PP6 may be used, provided that the breaker, wires and connector pin are adequate for the application.

(Continued on G12132-28 Sheet 2)

G12132-10-05 AN16gaTo 3060S Control Power pin 1

P2 J2existing label: AC INVERTER

EFN-97

PP9new label: PULSE CTRL

bb

new rating: 3Aexisting rating: 15A

(alternative to Taxi Light breaker wiring below)



G12132-28 --

PULSE LIGHT CONTROL CIRCUITSP132 and P122 CONSOLE WIRING

RBH 10/10/07

CLB 10/10/07

GA107 2 of 2


Effectivity: AS350B2 embodying mod 350A07-3273, or AS350B3 embodying mod 350A07-3274

CONSOLE MODIFICATION FOR PULSE LIGHT CONTROL

(Continued from G12132-28 Sheet 1)

On aircraft embodying mods 350A07-3273 or 350A07-3274, functions have been assigned to certain connector pins that are unused in the console definitions for earlier aircraft, including pins J2:d, J2:e and J2:f shown in the circuits on sheet 1. For those aircraft, the alternate circuits on this sheet apply.

To use these circuits, the installer must disconnect wires G12132-5-10 and G12132-5-11 from OP-1 in the left-hand switch rail and re-route them to ESN-18 in the right-hand switch rail. These wires may be renumbered as shown in the ESN-18 diagram at top right, or may retain their current wire numbers, so long as the wiring diagrams are updated to match.

Alternatively, wires G12132-5-10 and G12132-5-11 may be removed, or disconnected, capped and stowed, and new wires may be installed from the connector to switch ESN-18, as long as they are labeled appropriately and the wiring diagrams are updated to match.

To Airframe GND

To 3060S Control line, pin 3


MODIFIED BREAKER WIRING

LM2E


1

2

3

4

5

6

MS24524-23

G

J2P2

G

G12132-4-26

G12132-4-16

TAXI LIGHTESN-17

G12132-4-15

PP6


EFN-79

TAXI LIGHT

7.5A

G12132-10-05 AN16ga

MODIFIED ESN-18 SWITCH WIRING

q1

2

3

4

5

6

To 3060S Control Power pin 1

P2 J2

bb


LANDING / PULSE LIGHT

G12132-4-22

G12132-4-23

P2 J2

G12132-4-03

G12132-4-02

ESN-18

p

J1

q

existing label: AC INVERTER

EFN-97

To Landing Light relay

To Airframe GND

PP9

p

P1T T

U U

J J

G12132-5-11

AVIONICS MASTER

MS24524-23

1

2

3

4

5

6G12132-5-10

J2

T

V

W

U

P2

T

G12132-5-13 AN16ga

G12132-5-12 AN16gaV

W

AN16gaU

AN16ga

OP-1

Installer Defined

Installer Defined

STANDARD OP-1 SWITCH WIRINGref: G12132-5

Disconnect these two wires from OP-1 and route to ESN-18

new label: PULSE CTRL

new rating: 3Aexisting rating: 15A

SEE SHEET 1 FOR REV HISTORY



G12132-29 --

EXTERNAL INST LTS 2 BREAKERP132 and P122 CONSOLE WIRING

RBH 10/10/07

CLB 10/10/07

GA107 1

G12132-4-25 16ga.

G12132-4-12 16ga.1LK636E D D

1LK23E d d

P2 J2INST. LTS-2

EFN-75

10A

G12132-4-11 16ga.

MS24524-23

INSTRUMENT LIGHTS 2

1

2

3

4

5

6

ESN-15

G12301:2 DIMMER CONTROL (SEE G12132-23 OR G12132-23-P122)

G12132-4-25 16ga.

G12132-4-12 16ga.

dd

1LK637E

1LK23E

PP15

1LK636E D D

P2 J2

For this aircraft, The INSTRUMENT LIGHTS 2 breaker is mounted an installer-defined location outside the console.EFN-75

INST. LTS-2

10A

INSTRUMENT LIGHTS 2ESN-15

MS24524-23

1

2

3

4

5

6

ref: AEC DWG 350A64-7307-00ref: WDM 33.10.00

G12301:2 DIMMER CONTROL (SEE G12132-23 OR G12132-23-P122)


PP15

MODIFIED WIRING

STANDARD WIRINGref: G12132-4-073273, G12132-4-073274

CONSOLE MODIFICATION FOR RELOCATED PP15 (DIRECT BATTERY) BUS

For some installations, the installer may choose a location outside the console to house the PP15 bus and the attached circuit breakers, in order to reclaim the Left Middle breaker rail for other installer-defined circuits. As a result, the direct connection between the Instrument Lights 2 breaker and switch would no longer be possible. This diagram shows the necessary change to the circuit.

All changes to the console wiring can be made at the circuit breaker, without requiring the re-routing of any console wires. Wires G12132-4-11 and G12132-4-25 may be connected together using a blue butt splice (see G12132-1 for the splice part number).

Alternatively, wire G12132-4-25 may be removed from the wire bundle leading to the Left Middle breaker rail, and routed directly to the Instrument Lights 2 switch in the right hand switch rail. In most cases, the wire will be too short to reach the switch and must be extended.

Alternatively, a new wire of the proper length and gauge may be routed directly from pin J2:d to the Instrument Lights 2 switch, with appropriate labeling. For instance, at the installer's discretion, this wire might be labeled either G12132-4-11 or G12132-4-25, since it replaces both of the original wires.

All of these possible changes require that the installer update the wiring diagrams to reflect the changes.

G12132-4-11 16ga.

Splice existing wires together

G12132-23-02 18ga.

G12132-23-02 18ga.



G12132-30 A

OPTIONAL ENGINE ALT AIR CIRCUITP132 and P122 CONSOLE WIRING

RBH 10/10/07

CLB 10/10/07

GA107 1

y yKS2E G12132-5-09

ref: WDM 71.61.10

SAND FILTER

G12132-5-08

MS24524-23

1

2

3

4

5

6

Installer Defined

Installer Defined

J1P1

G12132-5-21

GG

HH

G12132-5-22

KS3E x

P1

GG

HH

x

J1

ESN-21SAND FILTER

G12132-5-07

EFN-66

PP6

G12132-5-21 GG GG

ref: Aerometals DWG 1350E1 (Single Hydraulic)

G12132-5-22

G12132-5-09

G12132-5-08

G12132-5-07

PP6

2.5A

EFN-66

ENG ALT AIR

1

2

3

4

5

6

G12132-5-24

G12132-5-23

MS24524-23

ESN-21ENGINE ALT AIR

3501B20

35010A20N

x

HH

y

x

HH

y

P1 J1

3502B20

BREAKER RATING VARIES WITH AIRCRAFT VERSION AND MOD LEVEL

STANDARD WIRING

MODIFIED WIRING

CONSOLE MODIFICATION FOR AEROMETALS INLET BARRIER FILTER SYSTEM(Was FDC/aerofilter)

This diagram shows how the standard SAND FILTER switch and breaker circuit may be modified for use with the Aerometals Inlet Barrier Filter system models 1350IN1-7 for aircraft with a single hydraulics system and 1350IN3-1 for aircraft with a dual hydraulics system. For both models the internal console wiring is the same, only the external wire numbers change.

Depending on the aircraft version and mod level, the standard SAND FILTER circuit breaker may be rated at 7.5A, and will need to be replaced.

The modified circuit uses the standard switch. All changes to the switch wiring can be made at the switch, without requiring the re-routing of any console wires. Two wires will need to be added at the switch, as shown. The ring terminals on wires G12132-5-07, -09 and -22 must be removed and the wire pairs shown in the diagram must be crimped into single terminals.

The wire numbers shown for the added wires are suggestions; the installer must make sure that the actual labels used do not duplicate wire numbers already in use in the console.

Effectivity: AS350D, D1, B, BA, B1, B2 and B3

10

10

ref: G12132-5

ref: Aerometals DWG 1350E2 (Dual Hydraulic)

A Added Dual Hudraulic option. Changed company name to Aerometals. 4/27/17 GA

Single Hyd: 35011A22 Dual Hyd: 3509A20


1

2

3

4

5

6

1

2

3

4

5

6

MS24524-23

FLOAT ARM

G12132-5-20GR4E

G12132-5-06

CC

BBBB

CC G12132-5-05

J1

FF

EE

FF

EE

P1

G12132-5-19

FLOATS ARMED Warning Lights:Installer shall provide suitable 28V lights, amber in color, and install lights in clear view of pilot, with appropriate label.

FLOAT ARM Switch location is any Console switch position. The switch position, wire labels, and console connector shown here are for illustration purposes only and are optional.

OP-3

G12132-21-23

POWER DIODES MUST BE RATED AT 6A AND 50VDC MINIMUM

NOTES:FOR USE WITH PRE-EXISTING FLOAT EQUIPMENT ONLYAll wire is AN20ga. unless otherwise noted.Wiring for switches and lights may optionally be AN22ga.Recommended Diode: 6A05-T (6A, 50V)Installer shall mount diodes securely.

GR1E

G12132-21-4

G12132-21-11

G12132-21-3

G12132-21-16

GR5E

GR2E

GR7NE

FLOAT INFLATE SWITCH WITH REQUIRED MS25224-1 RED SWITCH GUARD

WITH FLOATS ARMED, RAISE GUARD AND MOVE TOGGLE TO INFLATE FLOATS.

MS24524-23

FLOAT INFLATE Switch:This switch is mounted on a bracket attached to the horizontal portion of the pilot's cyclic tube, such that the toggle points toward the ceiling and the switch key notch faces forward. To inflate the floats, the pilot can pull back on the guard and accuate the toggle in one motion. Optionally, use Switch Housing p/n G12138. Label for switch guard: FLOAT INFLATE

G12132-21-2

G12132-21-1

UPDATED DIODE P/N IN NOTESA 05/12/10 RBH

11

11

11

www.genevaaviation.comwww.genevaaviation.com G12132-31 B

FLOAT SWITCH CIRCUITSP132 and P122 CONSOLE WIRING

RBH 10/10/07

CLB 10/10/07

GA107 1

REMOVED GREEN LAMP OPTIONFIXED INFLATE SWITCH WIRING;B 02/10/11 RBH

CONSOLE AND CIRCUITRY MODIFICATION FOR DUAL HYDRAULIC SYSTEM

The Dual Hydraulic system is an option for the AS350B3 only. Originally introduced as Mod OP3082 for aircraft pre-mod 350A07-3274, and as OP3346 with different airframe wire numbers for aircraft post-mod 350A07-3274, the dual system is now installed on all or nearly all new B3's.

The Dual Hydraulic System requires a separate circuit breaker on PP9 for the HYD MAIN function, an additional switch for the Servo Test function, and a modification to the WARN / FIRE switch circuit.

Use the TURN & BANK breaker for HYD MAIN. If a TURN & BANK breaker is needed, the function may be relocated to any available breaker on any bus supplied from the main PP12 bus, provided that the bus can handle the additional load.

The SERVO TEST switch must be single- or double-pole, momentary-ON. As of G12312 Revision J, OP-3 is wired for this function for aircraft post-mod 350A07-3274. For other B3 units, any unused switch position may be used for this function, but in nearly all cases the existing switch must be replaced with the proper type. The sample circuitry uses OP-3, which is the only switch that has no assigned function in the standard definition for these consoles.

The HYDRAULICS TEST switch circuitry inside the console does not require modification, but the airframe wire numbers will be different. The wire numbers will also differ between post-mod 350A07-3274 aircraft and earlier aircraft, throughout the Dual Hydraulic system wiring.

(Continued on G12132-32 Sheet 2)

Standard OP-3 Switch and Wiring(prior to G12132 Revision J)

FF

EE

BB

CC

Effectivity: AS350B3 with Dual Hydraulics


ref: AEC DWG 350A67-4165-00

Modified OP-3 Switch and Wiring(standard as of G12132 Revision J)

NEW G12132 REV J SWITCH TYPESTANDARDS FOR ESN-7 AND OP-3ADDED ESN-11 COLOR CODING

B

A

J1OP-3G12132-5-06

G12132-5-05

G12132-5-20

3

2

1

MS24523-26

FF

CC

BB

ref: WDM 29.10.20

SERVO TEST

03/23/09

09/25/08

RBH

RBH

P1

DH4NE or 1DH70NE

DH14E or 1DH14E

DH10E or 1DH74EFF

CC

BB

Installer Defined

Installer Defined

Installer Defined

Installer Defined FF

BB

CC

P1

EE

J1

ref: G12132-5-073274ref: G12132-5-073087

EFN-36

3

2

1

Standard ESN-11 Wiring

J1

J2

MS24658-23D

G12132-32 C

OPTIONAL DUAL HYDRAULICSP132 and P122 CONSOLE WIRING

RBH 05/06/08

CLB 05/06/08

GA107 1 of 2


1

2

3

4

5

6

MS24524-23

G12132-5-20

G12132-5-06

G12132-5-05

SPARE SWITCH

G12132-5-19

OP-3

(1DH112E and) 1DH1E

1DH5E R

S

P2

1DH6NE F

P1


G12132-3-12

G12132-3-13R

S

G12132-3-11F

G12132-3-10

D1:A

D1:C

ACCUMULATOR TEST

Modified ESN-11 Wiring

ESN-11or HYDRAULICS TEST

MS24658-23D

3

2

1

ESN-11HYD TEST

ref: G12132-3-073274ref: G12132-3-073087ref: WDM 29.00.00

(no connection for dual system)

DH5NE or 1DH93NE

DH50E or 1DH50E

S

R

P2

F

P1


ref: WDM 29.10.20ref: AEC DWG 350A67-4169-00

PP5

G12132-3-09

HYDRAULICS

7.5A

G12132-3-13

G12132-3-12

S

R

J2

G12132-3-11F

J1

D1:A

PP5

G12132-3-10

G12132-3-09

EFN-36

D1:C

HYDRAULICS

7.5A

ADDED WIRE 1DH112EC 03/04/10 RBH

ref: WDM 31.60.00ref: WDM 31.50.00ref: WDM 29.10.20ref: AEC DWG 350A67-4165-00

CONSOLE MODIFICATION FOR DUAL HYDRAULIC SYSTEM

(Continued from G12132-32 Sheet 1)

In addition, aircraft with Dual Hydraulic systems contain a wire from the Warning Light panel that requires a switched connection to ground, which must disconnect when the WARN / FIRE TEST switch is in the WARN TEST position, but connect when the WARN / FIRE TEST switch is at rest. Since the MS24524-27 switch used previously for the WARN / FIRE TEST function cannot make this connection internally, a different switch type (MS27407-3) is required to provide this functionality.

Effectivity: AS350B3 with Dual Hydraulics


EFN-N/A-1

Standard EFN-N/A-1 Wiringprior to G12132 Revision J

SEE SH. 1 FOR REVISION HISTORY

MS24524-27

WARN / FIRE TEST

Standard ESN-7 Wiring prior to G12132 Revision J

(FIRE TEST and Overlay circuitry omitted for clarity)

Installer Defined

ref: G12132-10-073274ref: G12132-10-073087

P1

G

1PE4NE or GND

1WW2NE

1WW82E25

ref: G12132-3-073087ref: G12132-3-073274

TURN & BANK

G12132-10-06J1

G2.5A

PP9

c c

b

P1

b

J1

G12132-3-20

G12132-3-19

1

2

3

4

5

6

(Center off)

ESN-7

EFN-N/A-1

Modified EFN-N/A-1 WiringStandard as of G12132 Revision J

This switch type maintains the following connections in the center OFF position: terminals 2 and 3 are connected together, and terminals 4 and 5 are connected together.

Prior to G12132 Revision F, an unused wire from ESN-7 terminal 3 to pin "d" of connector J1 was included in the standard B3 version console wiring. This wire was removed in revisions F, G and H, but is re-introduced in Revision J. If a particular console does not have this wire, then either a wire must be run from ESN-7 terminal 3 to an available connector pin for this purpose, or airframe wire 1DH6E must be wired directly to ESN-7 terminal 3.

Wire numbers shown are for aircraft embodying mod 350A07-3274. For earlier aircraft, wire number WW2NE replaces 1WW2NE, and wire number 1WW82E is replaced by either WW2NF or 1WW2NF, depending on the mod level. Diodes on these wires are required for both Single or Dual Hydraulics systems, and may be pre-existing on earlier aircraft. The installer shall confirm the presence of diodes in each branch of the circuit and shall provide suitable diodes for any branches without diodes. See G12132-1 section 5 for information on suitable diode types.

G12132-32 C

OPTIONAL DUAL HYDRAULICSP132 and P122 CONSOLE WIRING

RBH 05/06/08

CLB 05/06/08

GA107 2 of 2

27

26

25


G12132-10-06

G12132-3-18

G12132-3-19

G12132-3-20

Modified ESN-7 and EFN-N/A-1 WiringStandard as of G12132 Revision J

(FIRE TEST and Overlay circuitry omitted for clarity)

ref: G12132-10-073087ref: G12132-10-073274

DH1E or 1DH78F

DH6E or 1DH6E

1WW82E

1WW2NE

1PE4NE or GND

25

P1

G

J1

G

cc

d d

b

P1

b

J1

ref: G12132-3-073274ref: G12132-3-073087

WARN / FIRE TEST

27

1

2

3

4

5

6


ESN-7

2.5A

HYD MAINPP9

26



G12132-33 --

TWIST GRIP CIRCUIT (SB67.00.33)P132 and P122 CONSOLE WIRING

RBH 03/02/09

CLB 03/02/09

GA107 1

CONSOLE MODIFICATION FOR AS350B3 TWIST GRIPThis diagram shows how the standard FADEC breaker circuit may be modified for compliance with AEC Service Bulletin 67.00.33. This applies only to B3 aircraft pre-mod 350A07-3222, and is required only for P122 or P132 consoles manufactured under GA107 Revision F or later, that have the output of the MASTER CUTOFF switch internally connected to 1A FADEC and ROTOR breakers.

Refer to G12132-1 Revision H, paragraphs 6.1, 6.3, and 7.9 for specific requirements for reworking the console wiring.

The modification requires disconnecting the output wire from the currently installed 2.5A FADEC breaker and routing it to the output of a non-bussed 1A breaker which must be added or otherwise made available to the circuit; replacing the 2.5A breaker with a 7.5A breaker; and routing the output of the 7.5A breaker both to the input of the added 1A breaker, and to a separate output wire (if there was one originally connected to the 1A breaker, it may be used for this).

If there was no wire connected to the breaker, a new 20ga wire may be installed and routed through any available connector pin, or the KK161E wire may be routed directly to the 7.5A breaker.

Because this modification involves insertion of additional parts in line with circuits that are wholly contained within the console, the 1A breaker should be mounted inside the console. For a console with no SPARE breaker available, this may require that another circuit be moved outside the console.

Since the additional breaker in the FADEC circuit is not connected to a bus bar, select a breaker that is mounted at the forward or aft end of a rail, or at the split between two bus bars on the same rail, if one is available.

If a SPARE breaker is selected that is mounted in the middle of a bus bar, it may be moved to the extreme end of the bus bar area; all other breakers on the bar may be moved toward the source of the wiring bundle (DOWNWARD on a P122 console or FORWARD on a P132 console); and the bus bar may be shortened by one mounting hole. In this case, all breakers that are moved must be properly labeled in their new positions. Contact Geneva Aviation for information about replacement placards.

This example uses EFN-49 for the new 1A FADEC breaker, due to its proximity to the existing FADEC breaker, but any un-bussed breaker position will do.

It may be necessary to extend the existing wires to reach their new destination breakers. For those wires, the existing labels may be used, or the wires may be relabeled. Wire numbers shown for added wires are suggestions; the installer may assign other wire numbers, but must make sure that the actual labels used do not duplicate wire numbers already in use in the console.

ref: SB 67.00.33

MODIFIED WIRING

FADEC/TWIST

FADEC CONTROL

EMERGENCY-FADEC

Effectivity: AS350B3 post-mod 350A07-3084, pre-mod 350A07-3222, with SB 67.00.33 implemented

KK40E and KK51H Z Z

EFN-49 D2:A

G12132-2-14

EMER BUS BAR

EFN-72K

1A

D4:A

G12132-2-12

G12132-33-01

G12132-4-19

EFN-57

1A

7.5A

PP9

D2:C

G12132-2-13

J1

D4:C

P1

G12132-2-17

J1

u

P1

u KK161E

ref: WDM 80.00.00ref: G12132-2-073087

FADEC CONTROL

EMERGENCY-FADEC

STANDARD WIRING

ref: AEC DWG 350A08-5210

EMER BUS BAR

G12132-2-14

KK40E and KK51H

EFN-72K

1A

D4:A

G12132-2-13

Z

J1

Z

P1

D4:C

G12132-2-12

PP9

EFN-57

2.5A

D2:A

G12132-2-17

D2:C

EFN-49

G12132-4-19

SPARE

2.5A

PP9 P1J1

u u Installer Defined


ref: WDM 33.10.00

Effectivity: AS350B2 or AS350B3 embodying mod 350A07-3368

G12132-34 --

07-3368 LIGHTING CIRCUITSP132 and P122 CONSOLE WIRING

RBH 03/04/10

CLB 03/04/10

GA107 1 of 2www.genevaaviation.com

G12132-4-06 18ga.

1

2

3

4

5

67.5A

G12132-4-12 16ga.

G12132-4-25 16ga.

G12132-4-24 16ga.

G12132-4-10 18ga.

G12132-4-08 16ga.

G12132-4-05 18ga. N/C (was 1LK641E)

3LK675E (was 1LK636E)

N/C (was 1LK640E)

N/C (was 1LK633E)

1LK671E (was 1LK634E)

N/C (was 1LK44E)

N/C (was 1LK23E) d

D

g

d

D

g

C

e

f

K

C

e

f

KG12132-4-07 16ga.

G12132-4-11 16ga.

1

2

3

4

5

6

MS24524-23

G12132-4-09 18ga.

MS24524-23


PP15 INST. LTS-2

EFN-75

7.5A

EFN-43

P2 J2


PP5

G12132-23-01 18ga. to G12301 Dimmer Power Supply


CONSOLE MODIFICATION FOR AIRCRAFT WITH "217L" LIGHTING CONTROL MODULE

Aircraft that embody Mod 350A07-3368 use a different instrument panel lighting scheme than earlier AS350 aircraft, with a different control module ("217L") that requires less current and removes the interdependence of the Instrument Lights 1 and 2 switches.

On these aircraft, only the P2:C and P2:D connections are required, and are made using the airframe wires shown in the upper left diagram. The 10A Instrument Lights 1 and 2 breakers must be replaced with 7.5A breakers, as shown.

With the reduction of the breaker rating, all 16ga. and 18ga. internal console wiring shown in these circuits may be reduced to AN20ga in consoles specifically built for use with aircraft that embody Mod 350A07-3368.

At the installer's discretion, those console wires that terminate at "N/C" on the airframe side may be disconnected from the switches and breakers, and removed from the console or reassigned for other purposes. However, the switches must remain Double-Pole to take advantage of that switch type's higher lamp current rating.

If the PP15 bus is to be mounted outside the console, as specified in G12132-29, the P2:d connection will also be needed. The lower left diagram shows how the connections shown on G12132-29 may be modified for the new equipment.

Note that, as with all other modifications to the console or installation, the installer is required to update the wiring diagrams to reflect the actual connections used.


G12132-4-25 16ga.

G12132-4-12 16ga.

dd

G12132-34-01

PP15

3LK675E (was 1LK636E) D D

P2 J2

For this aircraft, The INSTRUMENT LIGHTS 2 breaker is mounted an installer-defined location outside the console.EFN-75

INST. LTS-2

7.5A


MS24524-23

1

2

3

4

5

6

MODIFIED PER G12132-29

G12132-4-11 16ga.

Splice existing wires together

G12132-23-02 18ga.

STANDARD CONSOLE WIRING

INST. LTS-1

www.genevaaviation.com G12132-34 --

07-3368 LIGHTING CIRCUITSP132 and P122 CONSOLE WIRING

RBH 03/04/10

CLB 03/04/10

GA107 2 of 2


EFN-95

LANDING LIGHT

20A

118L

NOTE: If a LANDING LIGHT indicator light is required, the installer shall provide a suitable light and install it within clear view of the pilot, with an appropriate label.

1LM7E

G12132-4-03

G12132-4-023

2

1

MS24523-23

LM1E

LANDING LIGHTESN-18

q q LM5NE

P1J1

p p

AN16ga.LM6E

LM6E-1 ZY

P2G12132-4-01

G12132-4-04AN16ga.

ZY

J2PP9

TAXI LIGHT

1

2

3

4

5

6

MS24524-23

NOTE: If a TAXI LIGHT indicator light is required, the installer shall provide a suitable light and install it within clear view of the pilot, with an appropriate label.

1LM2E


G

J2

G

P2

ref: WDM 33.43.00

TAXI LIGHT

EFN-79G12132-4-16

G12132-4-15

ESN-17

7.5A

PP6

EFN-95

LANDING LIGHT

20A

118L

1LM7E

LM1E

AN16ga.LM6E

LM6E-1 ZY

P2G12132-4-01

G12132-4-04AN16ga.

ZY

J2PP9

1LM2003E1LM2004NE

NOTE: If a LANDING LIGHT indicatorlight is required, the installer shall provide a suitable light and install it within clear view of the pilot, with an appropriate label.


TAXI LIGHT

1

2

3

4

5

6

MS24524-23



G

J2

G

P2

ref: WDM 33.43.00

TAXI LIGHT

EFN-79G12132-4-16

G12132-4-15

ESN-17

7.5A

PP6

1LM2E and1LM2008E

G12132-4-03

G12132-4-02

q q LM5NE

P1J1

p p3

2

1

MS24523-23

LANDING LIGHTESN-18

STD LAND LIGHT RELAY CIRCUIT

WIRED FOR MOD 350A07-3368

STD TAXI LIGHT CIRCUIT

WIRED FOR MOD 350A07-3368

ref: WDM 33.43.00

ref: WDM 33.43.00

CONSOLE MODIFICATION FOR AIRCRAFT WITH "217L" LIGHTING CONTROL MODULE (continued)

Aircraft that embody Mod 350A07-3368 also use the Landing Light and Taxi Light switch circuits to control part of the Instrument Lights circuits. This functionality requires additional connections in the Taxi Light switch circuit and the Landing Light Relay circuit.

At right, the additional wire (1LM2008E) is connected with the existing wire at the output of the Taxi Light switch.

At left, one pole of the Landing Light relay is reserved for the Lighting plate circuit (1LM2003E and 1LM2004NE).

SEE NOTES ON G12132-1Effectivity: AS350B3 embodying mod 350A07-3476

G12132-35 --

MASTER CUTOFF BYPASS CIRCUITP132 and P122 CONSOLE WIRING

RBH 5/12/10

CLB 5/12/10

GA107 1www.genevaaviation.com

CONSOLE MODIFICATION FOR MASTER CUTOFF BYPASS CIRCUIT PER MOD 350A07-3476

Aircraft that embody Mod 350A07-3476 supply power to the EMERGENCY bus when either the DIRECT BATTERY or the MASTER CUTOFF switch is engaged. This modification is not relevant to wiring diagram sets G12132-073273, G12132-073087 or the base G12132 wiring diagram set, and the current revision of the G12132-073274 and G12132-073368 wiring diagram sets provide this functionality. However, consoles built to earler revisions of the latter two wiring diagram sets may require modification to provide this functionality.

Airframe wire 3EU88E must be connected into the junction between the MASTER CUTOFF switch and the EMERGENCY bus bar inside the console.

At the installer's discretion, the connection may be made through the connector pin shown in the sample circuit, or through another available connector pin, or the airframe wire may be connected directly to the internal console circuit.

At the installer's discretion, the internal connection may be made by splicing the added wire into wire G12132-2-10 using an appropriately sized butt splice, or by replacing the ring terminal at either end of wire G12132-2-10 with an appropriately sized ring terminal and criming both wires into the terminal. Per document G12132-1 paragraph 6.1, do not add a second ring terminal at either the switch connection or the bus bar connection in order to connect the additional wire.

The wire number G12132-2-11 shown for the additional wire is only a suggestion. At the installer's discretion, if the additional wire is used, a different wire number may be assigned, provided that it uniquely identifies the wire. In any case the installer must update the wiring diagrams to reflect the actual connection method and wire number (if any) used in the installation.

EMER BUS BARG12135-2

G12132-2-10 AN16ga

1

2

3

4

5

6

MS24659-23D

MASTER CUTOFF


ESN-6

J1 P1

3EU18EG12132-2-09 T T

EMER BUS BARG12135-2

G12132-2-10 AN16ga

1

2

3

4

5

6

MS24659-23D

MASTER CUTOFF


ESN-6

3EU88EG12132-2-11 f f

J1 P1

3EU18EG12132-2-09 T T

UNMODIFIED MASTER CUTOFF SWITCH CIRCUITUNRELATED CIRCUITRY OMITTED FOR CLARITY

SAMPLE MODIFIED MASTER CUTOFF SWITCH CIRCUITUNRELATED CIRCUITRY OMITTED FOR CLARITY

Refer to drawing G12132-2-073274 or G12132-2-073368 (as appropriate) for the location of this bus bar

SEE NOTES ON G12132-1Effectivity: AS350B2 or AS350B3 embodying mods 350A07-3273 and 350A07-3274

G12132-36 --

ALTERNATE CARGO HOOK POWERP122 and P132 CONSOLE WIRING

RBH 8/30/11

CLB 8/30/11


CONSOLE MODIFICATION FOR ALTERNATE CARGO HOOK BREAKER POWER SOURCE

Per Eurocopter Service Bulletin AS350-25.01.09, AS350B3 aircraft post-mod 350A07-3273 and 350A07-3274 may be subject to startup failure if a short circuit occurs in the Cargo Hook circuitry. This Service Bulletin recommends separating the power source for the CARGO HOOK breaker from the PP9 bus used by the START and FADEC CONTROL breakers. Provision is made in the Service Bulletin for a similar change for AS350B2 aircraft.

This may be acomplished in the P132 or P122 console by physically moving the CARGO HOOK breaker to the end of the PP9 rail in which it is mounted, and shortening the bus bar so that it does not extend to the CARGO HOOK breaker position. For the P132 console, the new position would be at the aft end of the breaker rail; for the P122, it would be the uppermost position in the column. For tips on shortening the bus bar, see G12132-1 section 7.9.

If necessary, the output wire from the CARGO HOOK breaker may be extended to the new position using a blue butt splice; see G12132-1 section 6.2 for the appropriate part number.

The Service Bulletin also recommends reducing the rating of the CARGO HOOK breaker to 10A, as shown. See G12132-1 paragraph 7.1 for the appropriate breaker series.

Once the CARGO HOOK breaker is separated and replaced with the lower rating, at the installer's discretion, either it may be connected directly to airframe wire 1MY41E per the Service Bulletin, or wire 1MY41E may be connected to an available terminal post on the power terminal block and a separate 8 gauge or 10 gauge wire may be run from that post to the CARGO HOOK breaker.

The wire number G12132-36-01 shown here for the added wire is only a suggestion. Per G12132-1 Section 4, at the installer's discretion, if the additional wire is used, a different wire number may be assigned, provided that it uniquely identifies the wire. In any case the installer must update the wiring diagrams to reflect the actual connection method and wire number (if any) used in the installation.

UNMODIFIED CARGO HOOK BREAKER CIRCUIT

SAMPLE MODIFIED CARGO HOOK BREAKER CIRCUIT

CARGO HOOK

1ME1E G12132-10-02 AN16ga.J2P2

c c

15A

EFN-92

PP9

AN8ga G12132-11-041PP9E TB6

TB3

G12135-9 PP9 BUS BAR, Bottom Left

CARGO HOOK

1ME1E G12132-10-02 AN16ga.J2P2

c c

10A

EFN-92

TB3G12132-36-01 AN10ga. or AN8ga.

1MY41E

(N/C) (N/C)



The original 2E3 fuse holder between EU19E and EU18E, or between 3EU19E and 3EU18E, MUST be replaced with a circuit breaker as shown.

NOTICE: The circuitry related to the BAT-EXT PWR switch and the MASTER ELECTRICAL CUTOFF switch has been changed from the Eurocopter original circuitry. The functions are the same, but the wiring is different. Install using this wiring, and use this drawing for future electrical trouble shooting.

This circuitry is intended for AS350B3 aircraft that predate mod 350A07-3274. An AS350B3 which predates mod 350A07-3087, and does not incorporate Service Bulletin 80.00.05, will not need the P1:Z connection.

PRELIMINARYMM/DD/YY 00

P2

F

1

2

3

4

5

6

MS24659-23D

EFN-71E

1A

FADEC CONTROL

EFN-72K

1A

EFN-57

EMERGENCY-FADEC

EMERGENCY-NR INDICATOR

2.5A

J2G12132-2-08

D5:A

G12132-2-15

D5:CF

G12132-2-09

G12132-2-14

G12132-2-12

D4:A

D2:A

G12132-2-07

D6:C

G12132-2-17

G12132-2-13

D4:C

D2:C

D6:A

G12132-2-01

MASTER CUTOFF



1

2

3

4

5

6

PE2F (if installed) and PE2E

PG3NE

PG2NE

ESN-6

X

Y

W

X

Y

W

MS24659-23D

P1 J1

G12132-2-03

G12132-2-02

G12132-2-04

G12132-2-06

G12132-2-05

BAT-EXT PWRESN-1

EU3F or 3EU3F

ref: WDM 80.00.00ref: WDM 80.00.10

PG6NE S S G12132-2-02PG1NE R R G12132-2-03

G12132-2-10 16gaG12135-2

EMER BUS BAR, Middle Right Aft

EMER BUS BAR

PP9

EMER BUS BAR

These breakers replace fuses 71E and 72K, which are located in the hold on some aircraft.

T

Z

P1

T

J1

Z

EU18E or 3EU18E

KK40E and KK51H (MOD 350A07-3087 or SB80.00.05)1KK115E and 1KK128E (MOD 350A07-3257)

ROTOR TACH BAT

2.5ABATTERYAIRCRAFT + EU19E or 3EU19E

MASTER ELECTRICAL BOX

(REF: 2E3)

Effectivity: AS350B3 pre-dating mod 350A07-3274

G12132-2-073087 A


RBH 10/10/07

CLB 10/10/07

GA107 1

ADDED AIRFRAME WIRE PE2FA 03/04/10 RBH



LK16NE or PE4NE or GND

WW2NF or 1WW2NF, and WW2NE


G12132-3-05


ref: WDM 62.30.00ESN-12

EW36NE or 1EW93NE m m

EW37E or 1EW37E n n

EW39E or 1EW39E

EW38E or 1EW38EP1

j j

k k

J1

G12132-3-15

G12132-3-14

G12132-3-16

G12132-3-17

1

2

3

4

5

6

MS24524-23


PA1E N

KK53E or 1KK53E

KK55E or 1KK55E

PA2E

P

M

U

PA4E

P1

V

ref: WDM 80.00.00ref: WDM 80.00.10

ref: WDM 24.30.00

WARNING HORN

(Center off)MS24524-31

G12132-3-07N

G12132-3-02

G12132-3-08

G12132-3-06P

M

U

J1

VG12132-3-01

MS24523-26

CRANK

3

2

1

ESN-5


G12132-3-03 1

3

2

ESN-34

6

5

G12132-3-073087 C


RBH 10/10/07

CLB 10/10/07

GA107 1

1

2

3

4

5

6


WARN / FIRE TEST


WW38E

b

c c

b

e

P1

e

J1

G12132-3-19

G12132-3-20

G12132-3-21 G12132-3-04

ESN-7


G12132-23-09

GND for OVERLAYS

G12132-3-12

G12132-3-13

G12132-3-10

G12132-3-11

3

2

1

CRANK

2.5A

EFN-63

PP6

DH5E

DH112E (if installed) and DH1E S S

MS24658-23D

DH6NE

J2

R

P2

R

J1

F

P1

F

ESN-11HYD TEST

D1:A

ref: WDM 29.00.00

HYDRAULICS

EFN-36

7.5A

D1:C

G12132-3-09

PP5

ADDED ESN-11 COLOR CODINGA 09/25/08 RBH


CHANGED ESN-7 TYPE & WIRINGB 03/23/09 RBH

(No connection for Single Hydraulics) G12132-3-18d d

PP5 WARN PANEL 1

EFN-37

2.5A

G12132-3-22WW1E or 1WW1E E E

P2 J2

INTERNALIZED WW1F CIRCUIT

Connect the shields of EW38E and EW39E together outside of the P1 connector

ADDED EFN-7 NOTESDH112E TO HYDRAULICS CIRCUIT;

C 03/04/10 RBHAIRFRAME WIRES; ADDED WIREADDED SHIELD NOTE FOR ESN-12




INSTRUMENT LIGHTS 1

LK43E

The INSTRUMENT LIGHTS 2 function is required when using the Eurocopter dimmer module for the Instrument Panel lighting. This function is not used when using the Geneva dimmer. If this function is not used, the two wires connecting ESN-15 to ESN-14may be removed, and the INSTRUMENT LIGHTS 2 circuit may then be used for another function, with suitable labeling.

LK44E

J1

g

h

P1G12132-4-05

G12132-4-06g

h

16ga.G12132-4-12

LK1E

LK2E

C

D

C

D

G12132-4-11

ESN-15

1

2

3

4

5

6

MS24524-23

G12132-4-09

J2P2

ESN-14

MS24524-23

INSTRUMENT LIGHTS 2

1

2

3

4

5

6

G12132-4-07

G12132-4-08

16ga.

PP6 INST. LTS-2

10A

EFN-75

INST. LTS-1

EFN-43AN16ga.

16ga.

PP5

10A

ref: WDM 33.10.00




1

2

3

4

5

6

MS24524-23

ESN-17TAXI LIGHT

1

2

3

4

5

6

MS24524-23

ref: WDM 33.43.00


LM2E

P2

G

LJ1E

P2

B

ref: WDM 33.41.00


J2

G

G12132-4-16

G12132-4-15

EFN-79

7.5A

PP6

J2

B

TAXI LIGHT

PP6

G12132-4-13

G12132-4-14 EFN-87

POSITION LTS

7.5A

G12132-4-073087 --


RBH 10/10/07

CLB 10/10/07

GA107 1

G12132-4-04

G12132-4-01AN16ga.

The original LANDING LIGHT circuit MUST be rewired to match this diagram. The diode is optional.

LM1E40L or 118L

LM7ELM6E-1

LM6EAN16ga.

ZY

J2

YZ

P2LANDING LIGHTPP9

20A

EFN-95

This LANDING LIGHT switch circuit is optional, at the installer's discretion. Another switch and location may be substituted for the switch and location specified, with appropriate labeling. If an alternate location is used for the LANDING LIGHT switch, then the switch and position specified here may be used for another circuit, with appropriate labeling.

The landing light switch can be located on the Pilot's Collective Grip if desired.


G12132-4-03p p

q q

J1 P1

LM5NE

ref: WDM 33.43.00


G12132-23-01 18ga

G12132-23-01 18ga

MS24524-21

To optional Strobe unit L

P2


ref: WDM 33.41.00

STROBE LIGHT

G12132-4-197.5A

EFN-45 G12132-4-20

PP9

L

J2

1

2

3

4

5

6

G12132-4-17

(Center off)

G12132-4-21

ESN-9PP6

LX10E HG12132-4-18

H

EFN-83

ANTI-COL LT

ref: WDM 33.42.00

7.5A

ANTI-COLLISION LIGHTALL / TAIL


3

2

1

LANDING LIGHTESN-18

MS24523-23

G12132-4-02

G12132-4-10



CARGO HOOK

ref: WDM 30.42.00W/S WIPER

EFN-91

G12132-5-15

G12132-5-16

AVIONICS MASTER

ref: WDM 30.30.00

SEE G12132-16-073087 FOR SAMPLE OPTIONAL CIRCUITS

G12132-5-11


1

2

3

4

5

6

MS24524-23

W

VG12132-5-13

G12132-5-12

W

V

FN1E

T

U

P2

AN16gaT

U

J2

G12132-5-10AN16ga

AA

J2P2

AN16ga

AN16ga

K

J

K

J

OP-1

MK1E Blue G12132-5-14MM

MS24523-23

3

2

1

ESN-2FUEL PUMP

PP5ESN-13

3

2

1

MS24523-23

J2P2

G12132-5-04

G12132-5-03

(ref: 21Q) QN1E or 1QN1E

PITOT HEAT

ref: WDM 28.00.00

MS24523-23

MK1E White or Red

EFN-39

PITOT HEAT

7.5A

DD

J1P1

DD

PP93

2

1

G12132-5-17

G12132-5-18

P

J2

P

P2

7.5A

W/S WIPERESN-24

FUEL PUMP

G12132-5-01

G12132-5-02

PP6

7.5A

EFN-67

G12132-5-09

ref: WDM 71.61.10


KS2E

3

2

1

MS24523-23

OP-2

yy

G12132-5-07

G12132-5-19

Installer Defined

KS3E

G12132-5-21

P1 J1

1

2

3

4

5

6

G12132-5-22

J1

x

P1

x

HH

GG

HH

GG

MS24524-23

G12132-5-08

SAND FILTERESN-21

BB

CC

FF

BB

CC

FF

P1

EE

J1

EE

EFN-66

7.5A

G12132-5-20

PP6

G12132-5-06

G12132-5-05

SAND FILTER

SPARE SWITCHOP-3

1

2

3

4

5

6

MS24524-23

G12132-5-073087 --


RBH 10/10/07

CLB 10/10/07

GA107 1


Installer Defined

Installer Defined

Installer Defined

Installer Defined

Installer Defined

Installer Defined

Installer Defined

Installer Defined

Installer Defined

Installer Defined

Installer Defined



ref: WDM 77.00.10 EFN-38

Detailed on G12132-5-073087PITOT HEAT

ref: AEC DWG 350A67-0301-00

EU3E or 3EU3E

PP5

EFN-39

7.5A

G12132-6-03P1

A

J1

AD3:C

Detailed on G12132-3-073087

WARNING PANEL

HYDRAULICS

ref: WDM 39.00.00ref: WDM 62.30.00

PP5

G12132-6-022.5A

NR/NF

PP5

EFN-37

2.5A

D3:A

PP5

EFN-36

7.5A

13 LABELMOD LEVEL WIRE # v v

G12132-6-073087 A


RBH 10/10/07

CLB 10/10/07

GA107 1

INST. LTS-1

EFN-43

10A

GOV AGOV-1


ref: AEC DWG 350A67-0302-00

ORIGINAL07-3257

KK46E White or Red1KK46E Red


PP5

2.5A

EFN-41

EFN-42

7.5A

ORIGINALMOD LEVEL

ref: WDM 80.00.10

ref: AEC DWG 350A61-2643-00

ref: WDM 39.00.00ref: WDM 80.00.00

07-3257

P1

13

WW33E1WW72EASU1-3

ASU-1LABEL12 WIRE # D

P1

ref: WDM 31.41.00ref: WDM 39.00.00 12

G12132-6-05J1

PP5

G12132-6-04D

J1

PP5


MOVED EFN-37 WIRINGT OFF PAGEA RBH03/23/09


ATTITUDE GYRO

ref: WDM 39.00.00ref: WDM 31.60.00

ref: WDM 39.00.00ref: WDM 34.20.00

Installer Defined

G12132-7-07K

P1

K

J1

J1P1G12132-7-05

VEMD-2

EFN-55

7.5A

PP6

u u

EFN-49

2.5A

PP5

STROBE LIGHT

ref: WDM 31.60.00


ref: WDM 39.00.00

G12132-7-03s s

EFN-46

P1 J1

EFN-45

7.5A

VEMD-1 PP5

7.5A

PP9

G12132-7-01



ref: WDM 25.80.00EFN-58

2.5A

EXT. LOAD

ME87E w

P1 J1

w

PP9

EFN-57

2.5A

FADEC CONTROL PP9

G12132-7-08J1P1

WW31E E E

ref: WDM 39.00.00ref: WDM 31.50.00

2.5A

EFN-56

CAUTION PANEL PP6

2.5A

EFN-48

RELEASE PP5ref: WDM 39.00.00

Installer Defined G12132-7-04 AN16gaN N

P2 J2

ref: WDM 25.63.00 For optional uses, this breaker may be up to 15 amps.ref: WDM 25.80.00

G12132-7-073087 --


RBH 10/10/07

CLB 10/10/07

GA107 1

EW35E or 1EW35E

EW30E or 1EW30E



ref: WDM 39.00.00ref: WDM 80.00.00 2.5A

EFN-61

r

P1G12132-8-03

r

J1

ref: WDM 39.00.00ref: WDM 28.00.00

ref: WDM 80.00.00ref: WDM 39.00.00

G12132-8-01

C

P1

PP6

G12132-8-02C

J1

2.5A

EFN-60

FUEL GAUGE

B

PP6

B

EFN-59

7.5A

P1 J1

PP6


PP6Detailed on G12132-5-073087

ref: WDM 77.00.00ref: WDM 39.00.00

SAND FILTER

EFN-66

7.5A

J1P1

i i

2.5A

EFN-65

G12132-8-06

PP6

PP6

PP6

ref: WDM 39.00.00

L

P1

L

J1

EFN-64

7.5A

Detailed on G12132-3-073087CRANK

2.5A

EFN-63

G12132-8-05

ref: WDM 80.00.10

ref: WDM 80.00.10ref: WDM 77.00.10

ref: WDM 80.00.10

G12132-8-073087 --


RBH 10/10/07

CLB 10/10/07

GA107 1

ORIGINAL07-3257

MOD LEVELEM35E

1EM35E RedP. ENGINE

ENG P.

WIRE #

ORIGINAL07-3257

MOD LEVELInstaller defined1KK138E Red

(SPARE)GOV B

WIRE #

ORIGINAL07-3257

MOD LEVELKK39E White1KK137E Red

GOV-2GOV INDIC

WIRE #

ORIGINAL07-3257

MOD LEVELKK51E1KK51E

ENGINEENG CTL

LABEL WIRE #

QW1E or 1QW1E


14

15

16

17

LABEL

LABEL

LABEL

14

15

16

17


2.5Aref: WDM 39.00.00

DT5E


ref: WDM 31.31.00


EMERGENCY BUS

EFN-72K

EMERGENCY-FADEC

1A


EFN-71E

1A

EMERGENCY BUS

G12132-9-02H H

EFN-70

P1 J1

FUEL PUMP

ref: WDM 39.00.00ref: WDM 31.41.00


P1 J1G12132-9-01

PP9HOUR METER

AA AA

PP6

2.5A

EFN-68

PP6

EFN-67

7.5A



POSITION LTS

EFN-87

7.5A



PP6

EFN-83

ANTI-COL LT

PP6

7.5A

EFN-79

TAXI LIGHT

7.5A

G12132-9-03

ref: WDM 33.10.00ref: WDM 39.00.00

P1

JLE1E J

J1

CABIN LIGHTS

EFN-76

PP6

2.5A

Detailed on G12132-4-073087INST. LTS-2

EFN-75

PP6

10A

MOD LEVEL

07-3257ORIGINAL

LABEL

ASU1-2ASU-2

1WW34E

WIRE #WW34E

G12132-9-073087 --


RBH 10/10/07

CLB 10/10/07

GA107 1


18

18



ref: WDM 80.00.00ref: WDM 39.00.00

MH1E

G12132-10-04 AN16gaX X

10A

EFN-94

P2 J2

START PP9

AN16ga

G12132-10-03 AN16gaa

P2

a

J2

EFN-93

15A

PP9

AN16ga

CARGO HOOK

W/S WIPER

ref: WDM 25.80.00ref: WDM 39.00.00

ME1E G12132-10-02 AN16gac

P2

c

J2

EFN-92

15A

PP9

AN16ga

7.5A

EFN-91

PP9

2.5A

G12132-10-06

G12132-10-01(Installer Defined)

(Installer Defined)

ref: WDM 34.20.00EFN-N/A-2

2.5A

a

P1

DIR. GYRO

a

J1

PP6

EFN-N/A-1

G

P1

G

J1

G12132-10-05 AN16ga

ref: WDM 39.00.00ref: WDM 24.22.00

J2P2

TURN & BANK

XU1E b

PP9

b

AC INVERTER

15A

EFN-97 AN16ga

PP9


EFN-95

20A

LANDING LIGHT PP9



ref: WDM 80.00.10

KK4E or 1KK4E

G12132-10-073087 --


RBH 10/10/07

CLB 10/10/07

GA107 1




ref: WDM 24.30.00




PP9E TB6

TB5

TB4

AN8ga G12132-11-15

AN8ga G12132-11-13

AN8ga G12132-11-14

AN8ga G12132-11-04

PP6E

TB3

TB2

PP5E TB1

AN8ga G12132-11-03

AN8ga G12132-11-02

AN8ga G12132-11-01



G12135-80-2

G12135-80-12

G12135-80-10

G12135-80-9

G12135-80-8

G12135-80-10

G12135-80-9

PP5 BUS BAR, Top Right Fwd



BUS BAR, Top Left

BUS BAR, Middle Left

PP9 BUS BAR, Top Right Aft


G12132-11-073087 --


RBH 10/10/07

RBH 10/10/07

GA107 1

ref: G12132-2-073087

MASTER CUTOFF

G12132-2-10 AN16 ga1

2

3

4

5

6

MS24659-23D

ESN-6

EMER BUS BAR, Middle Right AftG12135-80-2


G12132-13-073087 B


GA107 1

RBH 10/10/07

RBH 10/10/07

GA 10/10/07

CLB 10/10/07

MS24524-23

INST. LTS-1

2.5A, PP5, EFN-38

NR

/NF

2.5A, PP6, EFN-68

CAU

TION

PNL

FWD


7.5A, PP6, EFN-59

2.5A, PP6, EFN-60

FUEL G

AUG

EEN

GIN

E7.5A, PP6, EFN-64

7.5A, PP6, EFN-83

ANTI-C

OL LT

EMER

-NR

IND

DIR

. GYR

O2.5A, PP6, EFN

-N/A-2

7.5A, PP6, EFN-87

POSITIO

N LT

1A, EMER

BUS, EFN

-72K

EMER

-FADEC

1A, EMER

BUS, EFN

-71E

2.5A, PP6, EFN-65

P. ENG

INE

SPARE

2.5A, PP6, EFN-76

CABIN

LTS

7.5A, PP6, EFN-79

TAXI LIGH

T

INST. LTS-2

10A, PP6, EFN-75

ASU-2

2.5A, PP6, EFN-61

2.5A, PP6, EFN-63

GO

V-2

CR

ANK

TAXI LIGH

T

10A, PP9, EFN-94

FADEC

CTR

L

START

LAND

ING

LIGH

TM

S24523-23

MS24524-21

MS24524-23

ANTI-C

OL LT

POSITIO

N LTS

INST. LTS-2

INST. LTS-1

RELEASE

ATTITUD

E

2.5A, PP9, EFN-57

2.5A, PP5, EFN-49

2.5A, PP5, EFN-48

VEMD

-17.5A, PP5, EFN

-46

2.5A, PP5, EFN-41

7.5A, PP5, EFN-39

PITOT H

EAT

7.5A, PP5, EFN-42

GO

V-1

10A, PP5, EFN-43

ASU-1

MS24524-23

MS24524-23

7.5A, PP6, EFN-55

VEMD

-2

2.5A, PP6, EFN-56

7.5A, PP6, EFN-66

7.5A, PP6, EFN-67

FUEL PU

MP

SAND

FILTERH

YDR

AULIC

S

WAR

N PAN

EL

7.5A, PP5, EFN-36

2.5A, PP5, EFN-37

MS24524-23

WAR

NIN

G H

OR

N

Effectivity: AS350B3 - Predating Mod 350A07-3257

FIXED EFN-71E WDM REFERENCEA 05/06/08 RBH

G12132-2-073087, 62.30.00

G12132-7-073087, 34.20.00

G12132-10-073087, 80.00.00

G12132-2-073087, 80.00.00

G12132-4-073087, ESN

-18

G12132-4-073087, ESN

-17

G12132-7-073087, 31.60.00

G12132-8-073087, 80.00.00

G12132-7-073087, 31.50.00

G12132-5-073087, 71.61.10

G12132-10-073087, 34.20.00

G12132-8-073087, 80.00.00

G12132-4-073087, 33.41.00

G12132-4-073087, 33.43.00

G12132-4-073087, 33.42.00

G12132-2-073087, 80.00.00

G12132-8-073087, 77.00.00

G12132-8-073087

G12132-3-073087, 80.00.00

G12132-5-073087, 28.00.00

G12132-9-073087, 31.41.00

G12132-4-073087, 33.10.00

G12132-9-073087, 33.10.00

G12132-8-073087, 28.00.00

G12132-3-073087, ESN

-12

G12132-3-073087, 29.00.00

G12132-4-073087, ESN

-15

G12132-4-073087, ESN

-10

G12132-4-073087, ESN

-9

G12132-6-073087, 80.00.00

G12132-7-073087, 31.60.00

G12132-7-073087, 25.80.00

G12132-4-073087, 33.10.00

G12132-3-073087, 31.50.00

G12132-6-073087, 31.41.00

G12132-5-073087, 30.30.00

G12132-6-073087, 62.30.00

G12132-4-073087, ESN

-14

CHANGED EFN-37 WIRING PAGEB RBH03/23/09


FIXED EFN-71E WDM REFERENCEA

Effectivity: AS350B3 - PredatingMod 350A07-3257

RBH05/06/08

34.20.00

33.41.00

7.5A, PP6, EFN-87

POSITION LTSG12132-4-073087

G12132-10-073087DIR. GYRO2.5A, PP6, EFN-N/A-2

G12132-8-07308777.00.00

2.5A, PP6, EFN-63

SPARE7.5A, PP6, EFN-64

G12132-3-073087

G12132-8-073087

CRANK

P. ENGINE2.5A, PP6, EFN-65

80.00.00

G12132-9-073087

33.42.00

33.43.00

33.10.00

TAXI LIGHT7.5A, PP6, EFN-79

G12132-4-073087

G12132-4-073087ANTI-COL LT7.5A, PP6, EFN-83

33.10.00

31.41.00

ASU-22.5A, PP6, EFN-68

G12132-9-073087

G12132-4-073087INST. LTS-210A, PP6, EFN-75

2.5A, PP6, EFN-76

CABIN LTSG12132-8-073087

2.5A, PP6, EFN-60

FUEL GAUGE

GOV-22.5A, PP6, EFN-61

G12132-8-073087

G12132-8-07308780.00.00

28.00.00

80.00.00

2.5A, PP6, EFN-56

G12132-7-073087VEMD-27.5A, PP6, EFN-55

G12132-7-073087CAUTION PNL

ENGINE7.5A, PP6, EFN-59

31.50.00

31.60.00

28.00.00

71.61.10

SAND FILTERG12132-5-073087

7.5A, PP6, EFN-66

FUEL PUMPG12132-5-073087

7.5A, PP6, EFN-67

EMER-NR IND1A, EMER, EFN-71E

G12132-2-073087

G12132-2-073087EMER FADEC1A, EMER, EFN-72K

62.30.00

80.00.00

FWD

G12132-7-073087

2.5A, PP5, EFN-48

2.5A, PP5, EFN-49

34.20.00

ATTITUDEG12132-7-073087

25.80.00, 25.63.00

31.60.00

RELEASEG12132-7-073087

INST. LTS-1

7.5A, PP5, EFN-42

7.5A, PP5, EFN-46

33.10.00G12132-4-073087

VEMD-1

80.00.00

10A, PP5, EFN-43

GOV-1G12132-6-073087

G12132-6-073087

7.5A, PP5, EFN-39

2.5A, PP5, EFN-41

PITOT HEAT

31.41.00G12132-6-073087ASU-1

30.30.00

62.30.00

G12132-5-073087

7.5A, PP5, EFN-36

2.5A, PP5, EFN-37

2.5A, PP5, EFN-38

WARN PANEL

HYDRAULICS

31.50.00

NR/NF

G12132-3-073087

29.00.00G12132-3-073087

FADEC CTRL

G12132-10-073087

2.5A, PP9, EFN-57

80.00.00

10A, PP9, EFN-94

START

80.00.00G12132-2-073087

G12132-13-073087-P122 B


GA107 1

RBH 10/10/07

RBH 10/10/07

GA 10/10/07

CLB 10/10/07

03/23/09CHANGED EFN-37 WIRING PAGEB RBH

MS2

4524

-23

AVIO

NIC

S

FWD

Opt

iona

l

Opt

iona

l

G12

132-

10-0

7308

7, 2

5.26

.00

7.5A

, PP9

, EFN

-45

STR

OBE

LT

CAR

GO

HO

OK

PWR

OU

TLET

G12

132-

5-07

3087

, 30.

42.0

0

W/S

WIP

ER15

A, P

P9, E

FN-9

2

7.5A

, PP9

, EFN

-91

G12

132-

10-0

7308

7, 2

5.80

.00

15A,

PP9

, EFN

-93

Opt

iona

l

?A, ?

bus,

LM

B-10

Opt

iona

l?A

, ?bu

s, L

MB-

8

?A, ?

bus,

LM

B-9

20A,

PP9

, EFN

-95

G12

132-

4-07

3087

, 33.

43.0

0

LAN

DIN

G L

T15

A, P

P9, E

FN-9

7G

1213

2-10

-073

087,

24.

22.0

0

AC IN

VER

TER

2.5A

, PP9

, EFN

-58

G12

132-

7-07

3087

, 25.

80.0

0

EXT.

LO

AD2.

5A, P

P9, E

FN-7

0H

OU

R M

ETER

2.5A

, PP9

, EFN

-N/A

-1TU

RN

& B

ANK

G12

132-

9-07

3087

, 31.

31.0

0

G12

132-

10-0

7308

7

?A, ?

bus,

LM

B-3

G12

132-

4-07

3087

, 33.

41.0

0

Opt

iona

l

Opt

iona

l

?A, ?

bus,

LM

B-7

?A, ?

bus,

LM

B-6

Opt

iona

l

?A, ?

bus,

LM

B-5

?A, ?

bus,

LM

B-4

Opt

iona

l

Opt

iona

l

Opt

iona

l

?A, ?

bus,

LM

B-2

?A, ?

bus,

LM

B-1

Opt

iona

l

Opt

iona

l

?A, ?

bus,

LTB

-9

Opt

iona

l

?A, ?

bus,

LTB

-12

Opt

iona

l

?A, ?

bus,

LTB

-11

Opt

iona

l

?A, ?

bus,

LTB

-10

G12

132-

2-07

3087

, ESN

-1

BAT-

EXT

PWR

MS2

4659

-23D

MS2

4523

-23

FUEL

PU

MP

G12

132-

5-07

3087

, ESN

-2

W/S

WIP

ERG

1213

2-5-

0730

87, E

SN-2

4

SPAR

E SW

ITC

HG

1213

2-5-

0730

87, O

P-3

MS2

4524

-23

SAN

D F

ILTE

RG

1213

2-5-

0730

87, E

SN-2

1

Opt

iona

l

Opt

iona

l

?A, ?

bus,

LTB

-8

Opt

iona

l

?A, ?

bus,

LTB

-7

Opt

iona

l

?A, ?

bus,

LTB

-6

?A, ?

bus,

LTB

-5

Opt

iona

l

Opt

iona

l

?A, ?

bus,

LTB

-4

?A, ?

bus,

LTB

-3

?A, ?

bus,

LTB

-1

Opt

iona

l

?A, ?

bus,

LTB

-2C

ARG

O H

OO

KG

1213

2-5-

0730

87, G

1213

2-17

, OP-

2

MS2

4523

-23

MS2

4524

-23

MS2

4523

-23

G12

132-

5-07

3087

, OP-

1

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12

G12

132-

12


G12132-14-073087 --


GA107 1

RBH 10/10/07

RBH 10/10/07

GA 10/10/07

CLB 10/10/07

Effectivity: AS350B3 Predating Mod 350A07-3274


Optional

Optional

?A, ?bus, LTB-1

?A, ?bus, LTB-2

?A, ?bus, LTB-3

Optional

?A, ?bus, LMB-4

?A, ?bus, LMB-9

Optional

?A, ?bus, LMB-8


Optional


?A, ?bus, LMB-6


Optional


Optional

Optional

?A, ?bus, LMB-3

Optional

Optional


?A, ?bus, LTB-5

?A, ?bus, LTB-6

Optional

?A, ?bus, LTB-7

Optional

?A, ?bus, LTB-8

?A, ?bus, LTB-9

Optional

Optional

Optional

?A, ?bus, LTB-10

Optional

?A, ?bus, LTB-11

?A, ?bus, LTB-12


HOUR METERG12132-9-073087

2.5A, PP9, EFN-70

G12132-7-073087

2.5A, PP9, EFN-58

G12132-10-073087

EXT. LOAD

15A, PP9, EFN-97

LANDING LTG12132-4-073087

20A, PP9, EFN-95

G12132-4-073087

7.5A, PP9, EFN-45

AC INVERTERG12132-10-073087

STROBE LT

7.5A, PP9, EFN-91

W/S WIPERG12132-5-073087

15A, PP9, EFN-93

G12132-10-073087

15A, PP9, EFN-92

PWR OUTLET

CARGO HOOK

G12132-10-073087

FWD

G12132-12G12132-12

G12132-12

G12132-12

G12132-12

G12132-12

G12132-12

G12132-12

G12132-12

G12132-12

G12132-12

G12132-12

G12132-12

G12132-12

G12132-12

G12132-12

G12132-12

G12132-12

G12132-12

G12132-12

G12132-12

G12132-12


G12132-14-073087-P122 --


GA107 1

RBH 10/10/07

RBH 10/10/07

GA 10/10/07

CLB 10/10/07

31.31.00

25.80.00

24.22.00

33.43.00

33.41.00

25.26.00

25.80.00

30.42.00

Effectivity: AS350B3 - Predating Mod 350A07-3274


WIPER

G12132-5-073087, ESN-24

G12132-5-073087, ESN-21

CARGO HOOK

SAND FILTER

G12132-5-073087, OP-2

G12132-5-073087, OP-1AVIONICS

MASTERAVIONICS

HOOKCARGO

W/S WIPER

SANDFILTER

Effectivity: AS350B3 PredatingMod 350A07-3274

G12132-2-073087, ESN-1

G12132-5-073087, ESN-2

BAT-EXT PWR

FUEL PUMP

G12132-5-073087, OP-3OP-3

WINDSHIELD

SWITCHSPARE

MS24659-23D

PUMPFUEL

POWERBAT-EXT

G12

132-

5-07

3087

, ES

N-1

3PI

TOT

HEA

T

G12

132-

2-07

3087

, ES

N-6

MS

2465

9-23

D

MS

2452

3-23

MA

STE

R C

UTO

FF

G12

132-

3-07

3087

, ES

N-7

G12

132-

3-07

3087

, ES

N-5

MS

2452

3-26

G12

132-

3-07

3087

, ES

N-1

1

MS

2740

7-3

WA

RN

/ FI

RE

TE

ST

CR

AN

K E

NG

INE

G12

132-

3-07

3087

, ES

N-3

MS

2465

8-23

D

MS

2452

4-31

GE

NE

RA

TOR

ON

HY

D T

EST

TESTWARN/FIRE

ON / RESETGENERATOR

TESTHYD

CUTOFFMASTER

ENGINECRANK PITOT

HEAT

LIGHTS

G12132-4-073087, ESN-10POSITION LTS

ANTI-COL LTG12132-4-073087, ESN-9

TAXI LIGHTG12132-4-073087, ESN-17

LANDING LIGHTG12132-4-073087, ESN-18

LANDINGLIGHT

TAXILIGHT

ANTI-COLALL / TAIL

G12132-4-073087, ESN-15INST. LTS-2

G12132-4-073087, ESN-14INST. LTS-1

WARNING HORNG12132-3-073087, ESN-12

LIGHTS 2INSTRUMENT

POSITION

MS24524-23

LIGHTS 1INSTRUMENT

WARNINGHORN

MS24524-23

MS24524-23

G12132-15-073087 A


GA107 1

RBH 10/10/07

RBH 10/10/07

GA 10/10/07

CLB 10/10/07

LANDING LTMS24523-23

MS24524-23

MS24524-21

MS24524-23

MS24523-23

MS24523-23

MS24524-23

MS24523-23

MS24524-23


MS24524-23


G12132-3-073087ESN-5, MS24523-26

P122 CONSOLE LAYOUT

G12132-5-073087

G12132-4-073087ESN-17, MS24524-23

ESN-13, MS24523-23

ESN-15, MS24524-23G12132-4-073087

G12132-5-073087OP-1, MS24524-23

G12132-4-073087

AVIONICSMASTER

ESN-14, MS24524-23

Effectivity: AS350B3 PredatingMod 350A07-3274

ESN-10, MS24524-23G12132-4-073087 G12132-4-073087

ESN-9, MS24524-21

PANELDIMMER

SPARESWITCH

GENERATORON / RESET

G12132-3-073087ESN-3, MS24524-31

INSTRUMENTLIGHTS 2

G12132-5-073087OP-3, MS24524-23

G12132-5-073087

INSTRUMENTLIGHTS 1

ESN-2, MS24523-23

FUELPUMP

ESN-1, MS24659-23DG12132-2-073087

BAT-EXTPOWER

G12132-3-073087ESN-11, MS24658-23D

ESN-21, MS24524-23G12132-5-073087

POSITIONLIGHTS

SANDFILTER

ANTI-COLALL / TAIL

ESN-24, MS24523-23G12132-5-073087

WINDSHIELDWIPER

G12132-3-073087ESN-7, MS27407-3

HYDRAULICTEST

WARN / FIRETEST

CARGOHOOK

ESN-18, MS24523-23G12132-4-073087

OP-2, MS24523-23G12132-5-073087

WARNINGHORN

G12132-2-073087ESN-6, MS24659-23D

LANDINGLIGHT

ESN-12, MS24524-23G12132-3-073087

TAXILIGHT

PITOTHEAT

MASTERCUTOFF

CRANKENGINE

G12132-15-073087-P122 A


GA107 1

RBH 10/10/07

RBH 10/10/07

GA 10/10/07

CLB 10/10/07A CHANGED ESN-7 SWITCH TYPE 03/23/09 RBH


MS24659-23D

G12132-5-11

AN16ga

AVIONICS MASTER

G12132-5-12

G12132-5-13


RELAYAVIONICS

EXTERNAL TO CONSOLE

PP128 ga.50A

AVIONICSA1

UU(no connection)X1

(Airframe GND)

X2

W

V

W

V


(no connection)

8 ga.

A2

TB4

T

P2

AN16gaT

J2

G12132-5-10

More samples on G12132-17-073087SAMPLE OPTIONAL CIRCUITS

ALT. ENCODER

2.5A

TRANSPONDER

2.5A

AUDIO PANEL

2.5A

10A

COM2

CD CHANGER

2.5A

5A

GPS

10A

COM1 STEREO ICS

2.5A


new label: AVIONICS-1PP9

G12132-10-05

AN16ga

AN16ga

1

2

3

4

5

6

OP-1

bb


15A

J2

EFN-97

P2

FROM G12132-10-073087

AN16ga


G12132-7-04 AN16ga

AN16ga

AN16ga

G12132-5-13 AN16ga

G12132-5-12 AN16ga

G12132-5-10

NN

P2

W W

VV

J2

U

TT

U

existing label: RELEASE

J2

EFN-48

P2

15A

1

2

3

4

5

6

MS24524-23

G12132-5-11

FROM G12132-7-073087

AVIONICS MASTEROP-1


G12132-16-03AN16ga

AN16gaG12132-16-04

FROM G12132-5-073087

G12132-16-073087 --


RBH 10/10/07

CLB 10/10/07

GA107 1



AVIONICS-1 BUS

AVIONICS-2 BUS

G12132-16-01 AN16ga

G12132-16-02 AN16ga

41

41


41



ME3E

ref: WDM 25.80.00

NN

From G12132-7-073087

G12132-17-01


ref: WDM 25.80.00ref: WDM 39.00.00 PP5

P2

EFN-48

J2

RELEASE

2.5A

G12132-7-04

3

2

1


From G12132-5-073087

HOOK ARMEDwarning light.Installer shall provide suitable light and install in clear view of pilot, with appropriate label.

J2

J

K

P2

MS24523-23

J

K


CARGO HOOKOP-2

G12132-5-16

G12132-5-15

G12132-17-073087 --


RBH 10/10/07

CLB 10/10/07

GA107 1



SAMPLE HOIST CIRCUIT FOR AS350B3

G12132-18-02


G12132-5-20



From G12132-5-073087

ME36E

CC

BB

CC

FF

G12132-5-05

G12132-5-06BB

FF

MS24524-23

1

2

3

4

5

6


G12132-18-01J1P1

EE

G12132-5-19

EE

OP-3HOIST

G12132-18-073087 --


RBH 10/10/07

CLB 10/10/07

GA107 1

Effectivity: AS350B3 Predating Mod 350A07-3274

450lb UNIT: ME101E300lb UNIT: ME33E20

??

J?

19

P?

??

???

HOIST20

G12132-?-??

CAPACITY?bus 450lb

300lb 2.5A7.5A

RATING19

From G12132-7-073087

ref: WDM 39.00.00ref: WDM 25.63.00

J2

N

P2

N

EFN-48

2.5A

G12132-7-04

RELEASE PP5

There is no breaker assigned to the HOIST function in the AS350B3 definitions of the console. If a HOIST circuit is required, implement it using a standard breaker that is available for reassignment, or an additional breaker installed in one of the OPTIONAL rails or in an installer-defined location outside the console

FWD

G12132-13-073257 A


GA107 1

RBH 10/10/07

RBH 10/10/07

GA 10/10/07

CLB 10/10/07


MS24524-23

INST. LTS-1

G12132-4-073087, ESN

-142.5A, PP5, EFN

-38

NR

/NF

G12132-6-073087, 62.30.00

G12132-7-073087, 31.50.00

2.5A, PP6, EFN-68

G12132-5-073087, 28.00.00

CAU

TION

PNL

7.5A, PP6, EFN-59

2.5A, PP6, EFN-60

FUEL G

AUG

EEN

G C

TL

G12132-8-073087, 80.00.10

G12132-10-073087, 34.20.00

Effectivity: AS350B3 EmbodyingMod 350A07-3257

G12132-3-073087, 80.00.10

7.5A, PP6, EFN-64

7.5A, PP6, EFN-83

ANTI-C

OL LT

G12132-4-073087, 33.42.00

EMER

-NR

IND

G12132-2-073087, 80.00.10

DIR

. GYR

O2.5A, PP6, EFN

-N/A-2

G12132-4-073087, 33.41.00

7.5A, PP6, EFN-87

POSITIO

N LT

1A, EMER

BUS, EFN

-72KG

12132-8-073087, 77.00.10

EMER

-FADEC

1A, EMER

BUS, EFN

-71EG

12132-2-073087, 80.00.10

G12132-8-073087, 80.00.10

2.5A, PP6, EFN-65

ENG

P.

GO

V B

2.5A, PP6, EFN-76

CABIN

LTS

7.5A, PP6, EFN-79

TAXI LIGH

T

G12132-4-073087, 33.43.00

G12132-9-073087, 33.10.00

INST. LTS-2

G12132-4-073087, 33.10.00

G12132-9-073087, 31.41.00

10A, PP6, EFN-75

ASU1-2

G12132-8-073087, 28.00.00

2.5A, PP6, EFN-61

G12132-8-073087, 80.00.10

GO

V IND

IC

2.5A, PP6, EFN-63

CR

ANK

TAXI LIGH

T

G12132-4-073087, ESN

-17

10A, PP9, EFN-94

FADEC

CTR

L

G12132-2-073087, 80.00.10

START

G12132-10-073087, 80.00.10

G12132-4-073087, ESN

-18

LAND

ING

LIGH

TM

S24523-23

MS24524-23

MS24524-21

MS24524-23

ANTI-C

OL LT

G12132-4-073087, ESN

-9

POSITIO

N LTS

G12132-4-073087, ESN

-10

INST. LTS-2

G12132-4-073087, ESN

-15

G12132-4-073087, 33.10.00

INST. LTS-1

G12132-7-073087, 25.80.00

RELEASE

ATTITUD

E

G12132-7-073087, 34.20.00

2.5A, PP9, EFN-57

2.5A, PP5, EFN-49

G12132-7-073087, 31.60.00

2.5A, PP5, EFN-48

VEMD

-17.5A, PP5, EFN

-46

2.5A, PP5, EFN-41

7.5A, PP5, EFN-39

PITOT H

EAT

G12132-5-073087, 30.30.00

7.5A, PP5, EFN-42

GO

V AG

12132-6-073087, 80.00.10

10A, PP5, EFN-43

ASU1-3

G12132-6-073087, 31.41.00

MS24524-23

MS24524-23

MS24524-23

7.5A, PP6, EFN-55

VEMD

-2

G12132-7-073087, 31.60.00

2.5A, PP6, EFN-56

7.5A, PP6, EFN-66

G12132-5-073087, 71.61.10

7.5A, PP6, EFN-67

FUEL PU

MP

SAND

FILTERH

YDR

AULIC

S

G12132-3-073087, 29.00.00

WAR

N PAN

EL

G12132-3-073087, 31.50.00

7.5A, PP5, EFN-36

2.5A, PP5, EFN-37

MS24524-23

WAR

NIN

G H

OR

N

G12132-3-073087, ESN

-12

03/23/09CHANGED EFN-37 WIRING PAGEA RBH

G12132-13-073257-P122 B


GA107 1

RBH 10/10/07

RBH 10/10/07

GA 10/10/07

CLB 10/10/07


FIXED EFN-63 WDM REFERENCEA


RBH05/06/08

G12132-4-073087

G12132-10-073087

POSITION LTS

DIR. GYRO34.20.00

33.41.00

7.5A, PP6, EFN-87


G12132-8-07308777.00.10

G12132-3-073087

G12132-8-073087GOV B

CRANK

ENG P.

2.5A, PP6, EFN-63

7.5A, PP6, EFN-64

2.5A, PP6, EFN-65

80.00.10

80.00.10

G12132-9-073087

G12132-4-073087

G12132-4-073087

TAXI LIGHT

ANTI-COL LT

33.42.00

33.43.00

33.10.00

7.5A, PP6, EFN-79

7.5A, PP6, EFN-83

G12132-9-073087

G12132-4-073087

ASU1-2

INST. LTS-2

CABIN LTS

33.10.00

31.41.00

2.5A, PP6, EFN-68

10A, PP6, EFN-75

2.5A, PP6, EFN-76

G12132-8-073087

G12132-8-073087

G12132-8-073087

FUEL GAUGE

GOV INDIC

2.5A, PP6, EFN-60

2.5A, PP6, EFN-61

80.00.10

28.00.00

80.00.10

G12132-7-073087

G12132-7-073087

VEMD-2

CAUTION PNL

ENG CTL

2.5A, PP6, EFN-56

7.5A, PP6, EFN-55

7.5A, PP6, EFN-59

31.50.00

31.60.00

G12132-5-073087

G12132-5-073087

SAND FILTER

FUEL PUMP28.00.00

71.61.10

7.5A, PP6, EFN-66

7.5A, PP6, EFN-67

G12132-2-073087

G12132-2-073087

EMER-NR IND

EMER-FADEC

1A, EMER, EFN-71E

1A, EMER, EFN-72K

77.00.10

80.00.10

FWD

G12132-7-073087

2.5A, PP5, EFN-48

2.5A, PP5, EFN-49

G12132-7-073087ATTITUDE34.20.00

G12132-7-073087RELEASE25.80.00

31.60.00

INST. LTS-1

7.5A, PP5, EFN-42

7.5A, PP5, EFN-46

G12132-4-073087

VEMD-1

33.10.00

G12132-6-073087GOV A80.00.10

10A, PP5, EFN-43

G12132-6-073087

PITOT HEAT7.5A, PP5, EFN-39

2.5A, PP5, EFN-41

G12132-6-073087ASU1-331.41.00

G12132-5-07308730.30.00

62.30.00

WARN PANEL

HYDRAULICS7.5A, PP5, EFN-36

2.5A, PP5, EFN-37

2.5A, PP5, EFN-38

G12132-3-073087

NR/NF

31.50.00

G12132-3-07308729.00.00

G12132-10-073087

FADEC CTRL2.5A, PP9, EFN-57

START80.00.10

10A, PP9, EFN-94

G12132-2-07308780.00.10

CHANGED EFN-37 WIRING PAGEB 03/23/09 RBH

Effectivity: AS350B2 embodying mod 350A07-3273


D5:AD5:C

The toggle on this switch must be marked with the color RED

MS24523-23

DIRECT BATTERY

G12132-2-08

G12132-2-09

G12132-2-193

2

1

OP-2

G12132-2-20

ref: AEC DWG 350A62-4100-00

G12132-2-01

MASTER CUTOFF

J1

ref: AEC DWG 350A62-4101-00ref: AEC DWG 350A64-7274-00

1PG1NE

1PG6NE

1PE2F (if installed) and 1PE2E W

R

S

P1

ref: WDM 24.30.00

BAT-EXT PWR

MS24659-23D

1

2

3

4

5

6

G12132-2-07

1

2

3

4

5

6

MS24659-23D

ESN-6

G12132-2-18

G12132-2-04W

G12132-2-03

G12132-2-02R

S

ESN-1

D6:C D6:A

G12132-2-05

G12132-2-06

NOTE: If the DIRECT BATTERY indicator light is required, the installer shall provide a suitable light and install it within clear view of the pilot, with an appropriate label.

G12132-2-073273 A

SWITCH DETAILS for B2P132 and P122 CONSOLE WIRING

RBH 10/10/07

CLB 10/10/07

GA107 1

(+28V VOYANT)DIRECT BATTERY

Changed from original Eurocopter circuitry: Use 1PE1E as power source for NR bridge light instead of 1LK656E

1PE1E

1LK655E

T

Z

T

Z

3PE28Ez z


3PW52E


1PG3NE

1PG2NEX X

P1J1

Y Y

ADDED AIRFRAME WIRE 1PE2FA 03/04/10 RBH

ref: AEC DWG 350A67-4154-00

1EW93NE

1EW37E

1EW38E

1EW39E

n

m

n

m

j

k

P1j

k

J1

ref: WDM 62.30.00

1

2

3

4

5

6

G12132-3-16

G12132-3-15

G12132-3-14

MS24524-23

WARNING HORN

G12132-3-17

ESN-12



G12132-3-02

G12132-3-06

G12132-3-07

G12132-3-081KK2E P P

1PA1E

1PA2E

N

M

N

M

1KK1E

1PA4E

J1P1

U

V

U

V

ref: WDM 80.00.00ref: WDM 24.30.00

G12132-3-01


3 6

3

2

1

MS24523-26

G12132-3-05

ESN-5CRANK

PP6


G12132-3-03ESN-3

1

2

4

5


G12132-3-073273 F


RBH 10/10/07

CLB 10/10/07

GA107 1


G12132-3-11

G12132-3-10

G12132-3-12

G12132-3-13


G12132-3-093

2

1

CRANK

2.5A

EFN-631DH5E

1DH112E (if installed) and 1DH1E S S

1DH6NE

J2

R

P2

R

MS24658-23D

J1

F

P1

F

ESN-11HYD TEST

D1:A

HYDRAULICS

EFN-36

D1:C

7.5A

PP5


Connect the shields of 1EW38E and 1EW39E together outside of the P1 connector


CORRECTED HORN SWITCH WIRINGA 05/06/08 RBHADDED ESN-11 COLOR CODINGB 09/25/08 RBHCHANGED ESN-7 TYPE & WIRINGC 03/23/09 RBHADDED EFN-7 NOTESDH112E TO HYDRAULICS CIRCUIT;

D 03/04/10 RBHAIRFRAME WIRES; ADDED WIREADDED SHIELD NOTE FOR ESN-12WIRING CHANGE FOR EASB 26.00.02 12/05/12 GAE ref: AEC DWG 350A67-2685-00

ref: AEC DWG 350A67-4166-00

ref: WDM 31.60.00ref: WDM 26.10.00

G12132-3-21

G12132-3-20

J1P1

1WW83E

1WW2NE

e

bb

e

D4:A

D2:A

D4:C

G12132-3-22

D2:C

ESN-7WARN / FIRE TEST

MS27407-3

1

2

3

4

5

6

G12132-3-04

G12132-23-09

GND for OVERLAYS1WG4E d G12132-3-18d

G12132-3-23

and 1WG18F c G12132-3-19c

(3-position)



ref: WDM 24.30.00

1PE4NE or GND

and 1WG4F

CORRECTED WARN/FIRE SWITCH 03/03/17 GAF


ref: AEC DWG 350A64-7308-00

MS24524-21



STROBE LIGHT

7.5A

EFN-45

PP5

ref: WDM 33.42.00

ANTI-COL LT

EFN-83

G12132-4-17

7.5A

1

2

3

4

5

6

(Center off)

G12132-4-21

ESN-9PP6




G12132-4-13

G12132-4-14


1

2

3

4

5

6

MS24524-23

1LJ1E B

P2

B

J2

ESN-10POSITION LIGHTS

G

P2

G

J2

PP6 POSITION LTS

7.5A

EFN-87

G12132-4-16

G12132-4-15


ESN-17TAXI LIGHT

1

2

3

4

5

6

MS24524-23

TAXI LIGHT

7.5A

EFN-79

PP61LM7E


The original LANDING LIGHT circuit MUST be rewired to match this diagram. The diode is optional. Another switch and location may be substituted for the switch and location specified, with appropriate labeling. If an alternate location is used forthe LANDING LIGHT switch, then the switch and position specified here may be used for another circuit, with appropriate labeling.

40L or 118L

LM1E

AN16ga.LM6E

LM6E-1

J2

ZY

P2G12132-4-01

G12132-4-04ZY

AN16ga. EFN-95

LANDING LIGHTPP9

20A

1LM2E

INST. LTS-1PP5

1

2

3

4

5

6

DD1LK636E

1LK23E d d

e e

1LK640E

1LK633E

g g

1LK641E

1LK44E

1LK634E C C

P2

f

K K

f

J2

G12132-4-12 16ga.

G12132-4-25 16ga.

ESN-15

1

2

3

4

5

6

INSTRUMENT LIGHTS 2

MS24524-23

G12132-4-24 16ga.

G12132-4-10 18ga.

G12132-4-09

G12132-4-08 16ga.

G12132-4-05 18ga.

G12132-4-06 18ga.

G12132-4-11 16ga.

PP15

G12132-4-07 16ga.

10A

EFN-75

INST. LTS-2

EFN-43

10A


ESN-14INSTRUMENT LIGHTS 1



At the installer's discretion, the entire PP15 bus, including the INSTRUMENT LIGHTS 2 breaker, may be mounted in an installer defined location outside the console. See G12132-29 for the resulting INSTRUMENT LIGHTS 2 switch circuit.

G12132-4-19

G12132-4-20


To optional Strobe unit

1LX10EG12132-4-18

H

P2

L

H

J2

L

G12132-4-073273 --


RBH 10/10/07

CLB 10/10/07

GA107 1


This circuit is optional, at the installer's discretion. The landing light switch can be located on the Pilot's Collective Grip if desired.


q q LM5NE

P1J1

p p


G12132-4-03

G12132-4-023

2

1

MS24523-23

LANDING LIGHTESN-18

ANTI-COLLISION LIGHTALL / TAIL

18ga.

G12132-23-01 18ga.

G12132-23-02 18ga.

MS24524-23

EFN-91


ref: AEC DWG 350A73-6089-00


ref: WDM 30.42.00


ref: WDM 30.30.00


ref: AEC DWG 350A67-6091-00

Installer Defined

Installer Defined

Installer Defined

Installer Defined

UUG12132-5-12 AN16ga.

G12132-5-13 AN16ga.W

V

W

V

OP-1

MS24524-23

1

2

3

4

5

6

G12132-5-11

AVIONICS MASTER

G12132-5-10

AN16gaT

P2

T

J2

AN16ga

NOTE: If a FUEL PUMP 1 indicator light is required, the installer shall provide a suitable light and install it within clear view of the pilot, with an appropriate label.

ref: AEC DWG 350A73-2686-00

PP5

1FN1E

G12132-5-033

2

1

J2

MS24523-23

AA

P2

G12132-5-04

PITOT HEATESN-13

ref: WDM 28.00.00

1QN11E

7.5A

EFN-39

1MK1E Blue

1MK1E Red

PITOT HEAT

1QN1E DD

P1 J1

DD

G12132-5-173

2

1

G12132-5-14

G12132-5-18

P

M

P2

P

M

J2

MS24523-23

W/S WIPERESN-24

PP9

G12132-5-02

G12132-5-01

FUEL PUMP 1

MS24523-23

3

2

1

ESN-2FUEL PUMP-1

EFN-67

PP6

7.5A

y y1KS2E G12132-5-09

G12132-5-073273 A


RBH 10/10/07

CLB 10/10/07

GA107 1

ref: WDM 71.61.10


ref: AEC DWG 350A67-2692-00


FUEL PUMP 2

MS24523-23

3

2

1

SAND FILTER

G12132-5-08

MS24524-23

1

2

3

4

5

6


Installer Defined

Installer Defined

1KS3E

7.5A

W/S WIPER

J1P1

G12132-5-21

GG

HH

G12132-5-22

x

P1

GG

HH

x

J1

1QN8E

ESN-21

P1

AA


1QN8G

ESN-8

SAND FILTER

G12132-5-07 7.5A

EFN-66

J1

AA

PP6

G12132-5-05

G12132-5-06

PP6

EFN-68

FUEL PUMP-2

7.5A

1LK639E

1FW2E

NOTE: If a PITOT indicator light is required, the installer shall provide a suitable light and install it within clear view of the pilot, with an appropriate label. Recommended maximum current 12mA.

A ADDED PITOT INDICATOR LIGHT 03/04/10 RBH


D3:C

D3:A

EFN-38

PITOT HEAT


1EU3E

PP5

7.5A

EFN-39

G12132-6-03P1

A

J1

A

HYDRAULICS

WARNING PANEL-1

ROTOR TACH

ref: WDM 31.50.00

ref: WDM 62.30.00

1WW1E and 1WW1F


G12132-6-022.5A

PP5

G12132-6-01

EFN-37

E

P2

E

J2

2.5A

PP5

7.5A

EFN-36

PP5


PP5

PP5

10A

EFN-43


Installer Defined vv

INST. LTS-1

7.5A

EFN-42

P1 J1

SPARE

G12132-6-05

PP5

PP5

1EW103E

EFN-41

D

P1 J1

D

VHIU-1

2.5A

ref: WDM 25.80.00

To HOOK Switch

P1

t

EFN-40

t

J1

HOOK RELEASE

2.5A

G12132-6-04

G12132-6-06ref: AEC DWG 350A62-4100-00ref: AEC DWG 350A67-2685-00

ref: AEC DWG 350A67-2689-00

ref: AEC DWG 350A63-6159-00

ref: AEC DWG 350A67-4166-00

ref: G12132-17-073273

ref: AEC DWG 350A63-6158-00

G12132-6-073273 A


RBH 10/10/07

CLB 10/10/07

GA107 1


ref: WDM 31.60.00

ADDED EFN-41 WDM REFERENCEA RBH05/06/08



HOIST RELEASEFor optional uses, this breaker may be up to 15 amps.

ref: G12132-18-073273

ATTITUDE

(1FF219E)

ref: AEC DWG 350A68-2542-01

To HOIST switch

Wire directly to the Attitude gyro, or through an On/Off switch; or, this function may be moved to a breaker that is supplied from a switched bus.

ADDED WDM REFERENCESA

ref: WDM 34.20.00

G12132-7-05u u

05/06/08 RBH

G12132-7-04 AN16ga.

PP5

2.5A

EFN-49

P1 J1

P2 J2

N N

EFN-48

2.5A

STROBE LIGHT

1EW30E

ref: AEC DWG 350A64-7326-00

ref: AEC DWG 350A63-6159-00ref: AEC DWG 350A63-5017-00ref: AEC DWG 350A63-5016-00


ref: WDM 25.63.00

ref: WDM 31.60.00

G12132-7-03

PP5

s s

PP5

7.5A

EFN-46

P1 J1

VEMD-1

PP5

EFN-45

7.5A

For optional uses, this breaker may be up to 15 amps.HOIST

ref: G12132-18-073273

G12132-7-073273 B


RBH 10/10/07

CLB 10/10/07

GA107 1

G12132-7-09 AN16ga.

G12132-7-01ww1ME87E


EXT. LOAD

2.5A

J1P1

EFN-58

PP6

Installer Defined

21

P2 J2

FF

EFN-57


G12132-7-07

G12132-7-08

ref: WDM 25.63.00

ref: AEC DWG 350A62-4100-00


ref: WDM 31.50.00

1WW31E

PP9

E

J1

E

P1

WARNING PANEL-2

2.5A

EFN-56

PP6

ref: AEC DWG 350A67-4166-00ref: WDM 31.60.00 VEMD-2

1EW35E

EFN-55

K

J1P1

K

7.5A

PP6

RATINGCAPACITY450 lb300 lb

21

7.5A2.5A

WIRES FROM EFN-57 TABLEREMOVED ERRONEOUS AIRFRAME B 03/04/10 RBH


1QW38E

2.5A

EFN-61

r

P1G12132-8-03

r

J1

ref: WDM 28.41.10

ref: WDM 28.00.00

G12132-8-01

FUEL FLOW

1QW1E C

P1

PP6

G12132-8-02C

J1

2.5A

EFN-60

FUEL GAUGE

1EW105E B

PP6

B

VHIU-2

EFN-59

2.5A

P1 J1

PP6



SAND FILTER

EFN-66

7.5A

Installer Defined

J1P1

i i

2.5A

EFN-65

G12132-8-06

PP6

PP6

PP6ref: WDM 77.00.00

1EU26E

SPARE

L

P1

L

J1

NTL IND

EFN-64

2.5A


CRANK

2.5A

EFN-63

G12132-8-05

ref: AEC DWG 350A67-2686-00

ref: AEC DWG 350A67-2695-00

ref: AEC DWG 350A67-2690-00

May be wired directly to the Fuel Flow meter, or through an On/Off switch

WINDSHIELD WIPER 2

Installer Defined G12132-8-04 16 ga.

EFN-62

7.5A

P2

Q

J2

Q

PP6ref: WDM 30.42.00ref: AEC DWG 350A67-6090-00

ref: AEC DWG 350A67-4166-00


G12132-8-073273 A


RBH 10/10/07

CLB 10/10/07

GA107 1

ref: WDM 31.60.00

ADDED EFN-59 WDM REFERENCEA RBH05/06/08


1DT5E


ref: WDM 31.31.00

EFN-75

PP15INST. LTS-2

10A

G12132-9-02

PP9

H

P1

H

J1

2.5A

HOUR METER

EFN-70

FUEL PUMP-1

FUEL PUMP-2


PP6

7.5A

EFN-68

PP6

EFN-67

7.5A




EFN-87

POSITION LTS PP6

7.5A

EFN-83

ANTI-COL LT PP6

7.5A

G12132-9-03J1LE1E J


EFN-79

7.5A

TAXI LIGHT PP6

ref: WDM 33.10.00 CABIN LIGHTS

P1

EFN-76

2.5A

J1

PP6

ref: AEC DWG 350A67-6087-00




G12132-9-073273 --


RBH 10/10/07

CLB 10/10/07

GA107 1



1KK4E and 1KK4F

ref: WDM 80.00.00

1MH1E

G12132-10-04 AN16gaX X

10A

EFN-94

P2 J2

START PP9

G12132-10-03 AN16gaa

P2

a

J2

EFN-93

15A

PP9

CARGO HOOK

W/S WIPER-1

ref: WDM 25.80.00

1ME1E G12132-10-02 AN16gac

P2

c

J2

EFN-92

15A

PP9

7.5A

EFN-91

PP9

2.5A

G12132-10-06

G12132-10-01(1FF210F)

(1FA1E)

ref: WDM 34.20.00

EFN-N/A-2

2.5A

a

P1

DIR. GYRO

a

J1

PP6

EFN-N/A-1

G

P1

G

J1

G12132-10-05 AN16ga

ref: WDM 24.22.00

J2P2

TURN & BANK

1XU1E b

PP9

b

AC INVERTER

15A

EFN-97

PP9


EFN-95

20A

LANDING LIGHT PP9



G12132-10-09

ref: AEC DWG 350A62-4101-00

g g

EFN-N/A-4

D-BAT CONTROL

P1

3A

J1

PP15

ref: AEC DWG 350A68-2543-01

ref: AEC DWG 350A68-2541-01

ref: AEC DWG 350A62-0049-00

ref: AEC DWG 350A63-6158-00

ref: AEC DWG 350A62-0045-00

ref: AEC DWG 350A67-2688-00

Wire directly to the Directional gyro, or through an On/Off switch; or, this function may be moved to a breaker that is supplied from a switched bus.

G12132-10-083PW54E and 3PW54F

P1

h h

J1

ref: AEC DWG 350A62-4101-00DIRECT BATTERY

EFN-N/A-3

PP6

2.5A

3PW53E and 3PW55E

Wire directly to the Turn & Bank Indicator, or through an On/Off switch; or, this function may be moved to a breaker that is supplied from a switched bus.

At the installer's discretion, the entire PP15 bus, including the D-BAT CONTROL breaker function, may be moved to an installer-defined location outside the console.


G12132-10-073273 A


RBH 10/10/07

CLB 10/10/07

GA107 1

ADDED WDM REFERENCESA RBH05/06/08

ref: WDM 24.30.00

ref: WDM 24.30.00




BUS BAR, Top Left

PP15 BUS BAR, Middle Left



PP5 BUS BAR, Top Right


1PP9E


1PP6E

1PP5E

ref: WDM 24.30.00

TB6

TB5

TB4

TB2

TB1


G12135-80-9

G12135-80-12

G12135-80-10

G12135-80-9

G12135-80-10

G12135-80-12

3PP23E


G12132-11-073273 --


RBH 10/10/07

CLB 10/10/07

GA107 1


At the installer's discretion, all or part of the left middle rail may be used for the PP15 bus, or the entire PP15 bus may be moved to an installer defined mounting location outside the console and the left middle rail used for other, installer-defined circuits.

TB3

AN8ga G12132-11-01

AN8ga G12132-11-02

AN8ga G12132-11-03

AN8ga G12132-11-04

AN8ga G12132-11-14

AN8ga G12132-11-13


LEFT MIDDLE BUS BAR

PP

LTB-BUSVOID

LTB-1

2.5A

LTB-BUS

LTB-BUSVOID

2.5A

LTB-2

2.5A

LTB-3

VOID

G12132-12-18

G12132-12-17

LTB-BUS

LTB-BUS

LTB-5

2.5A

LTB-4

VOID

5A

LTB-6VOID

G12132-12-16

G12132-12-14

G12132-12-15

???

???

VU

VU

???

???

T T

S S

???

???

???

R R

Q Q

VOID LTB-BUS

G12132-12-095A

LTB-BUS

LTB-BUS

5A

LTB-7

5A

VOID

LTB-8VOID

G12132-12-13

G12132-12-12

G12132-12-11

G12132-12-10

LTB-BUS

LTB-BUSLTB-9

7.5A

VOID

LTB-10

7.5A

VOID

G12132-12-08

G12132-12-07

G12132-12-06

G12132-12-05

LTB-BUS

LTB-BUS

LTB-11

10A

VOIDLTB-12

10A

VOID

G12132-12-03

G12132-12-04

G12132-12-02

G12132-12-01

???JJ

???

???

???

???

LL

N

M

N

M

K K

???

???

???

???

HG

HG

FE

FE

???

???

???

???

CD

CD

AB

J3

AB

P3LEFT TOP BUS BAR

???5A


G12132-12-31 ???

if installed.Installer defined g g

G12132-12-26

G12132-12-27

G12132-12-28

G12132-12-29

G12132-12-30

LMB-3

5A

VOID

2.5A

LMB-4

VOIDLMB-5

PP15

PP15

dd

f f

e e

???

???

cc

b b

???

???

TB4

TB5

LMB-2

G12132-12-22

G12132-12-23

G12132-12-24

G12132-12-25

PP15VOID

7.5A

VOIDLMB-6

5A

VOIDLMB-7

PP15

PP15

7.5A

7.5A

VOID

LMB-8

VOID

LMB-9PP15

PP15

Z

a a

Z

???

???

X

YY

X

???

???

PP15 BUS

LTB-BUS

G12132-12-21

(p/n: G12135-80-12)

(p/n: G12135-80-10)

2.5A

VOID PP15

8 ga. or 10ga.

8 ga. or 10ga.G12132-11-14

W

P3J3

W???

G12132-11-13 Installer defined power source

3PP23E

Installer definedif installed.

The PP15 bus normally powers minimal avionics functions, not shown here. At the installer's discretion, the PP15 bus may be moved to an installer-defined location outside the console, so that the left middle breaker rail may be used for additional installer-defined avionics circuits. In that case, the Instrument Lights 2 circuit will need to be modified. See sample Instrument Lights 2 circuit on G12132-29.






??? = Installer Defined


NOTE:ALL WIRES ON THIS DRAWING ARE 16 ga. UNLESS SHOWN OTHERWISE.RING TERMINALS FOR CIRCUIT BREAKERS ARE RED #6 (p/n 36152), EXCEPT FOR DUAL WIRES WHICH HAVE BOTH WIRES CRIMPED INTO ONE BLUE #6 RING TERMINAL (p/n 36158 OR 326882).

AIR

CR

AFT

FW

D

G12132-12-20

G12132-12-19


G12132-12-073273 --


RBH 10/10/07

CLB 10/10/07

GA107 1


G12132-4-073273, ESN

-15

INST. LTS-2

FWD

G12132-4-073273, ESN

-17

G12132-4-073273, ESN

-18

LAND

ING

LIGH

TM

S24523-23

G12132-4-073273, ESN

-10

POSITIO

N LTS

MS24524-21

G12132-4-073273, ESN

-9

ANTI-C

OL LT

MS24524-23

TAXI LIGH

T

MS24524-23

G12132-4-073273, ESN

-14

MS24524-23

INST. LTS-1

MS24524-23

WAR

NIN

G H

OR

N

G12132-3-073273, ESN

-12M

S24524-23

G12132-6-073273, 25.80.00

HO

OK R

EL

FUEL G

AUG

E2.5A, PP6, EFN

-60G

12132-8-073273, 31.60.00

CABIN

LTS2.5A, PP6, EFN

-76

VEMD

-1

G12132-7-073273, 25.63.00

HO

IST REL

G12132-7-073273, 34.20.00

ATTITUD

E2.5A, PP5, EFN

-49G

12132-8-073273

G12132-9-073273, 33.10.00

G12132-4-073273, 33.43.00

TAXI LIGH

T7.5A, PP6, EFN

-79

G12132-4-073273, 33.42.00

ANTI-C

OL LT

7.5A, PP6, EFN-83

POSITIO

N LT

7.5A, PP6, EFN-87

G12132-10-073273, 34.20.00

DIR

. GYR

O2.5A, PP6, EFN

-N/A-2

G12132-4-073273, 33.41.00

2.5A, PP6, EFN-63

SPARE

2.5A, PP6, EFN-65

G12132-8-073273, 77.00.00

NTL IN

D2.5A, PP6, EFN

-64G

12132-3-073273, 80.00.00

CR

ANK

FUEL FLO

W

G12132-8-073273, 28.41.10

2.5A, PP6, EFN-61

G12132-8-073273, 28.00.00

G12132-4-073273, 33.10.00

INST. LTS-1

7.5A, PP5, EFN-46

G12132-7-073273, 31.60.00

2.5A, PP5, EFN-48

G12132-4-073273, 33.41.00

STRO

BE LT7.5A, PP5, EFN

-45

G12132-6-073273, 62.30.00

SPARE

7.5A, PP5, EFN-42

G12132-6-073273

10A, PP5, EFN-43

RO

TOR

TACH

2.5A, PP5, EFN-41

SAND

FILTER

FUEL PU

MP-1

G12132-5-073273, 28.00.00

FUEL PU

MP-2

2.5A, PP6, EFN-56

G12132-7-073273, 31.60.00

VEMD

-27.5A, PP6, EFN

-67

G12132-5-073273, 28.00.00

7.5A, PP6, EFN-68

EXT. LOAD

2.5A, PP6, EFN-58

2.5A, PP6, EFN-59

G12132-7-073273, 25.80.00

G12132-7-073273, 31.50.00

WAR

N PN

L-2G

12132-5-073273, 71.61.107.5A, PP6, EFN

-66

7.5A, PP6, EFN-55

WAR

N PN

L-12.5A, PP5, EFN

-37

G12132-6-073273, 31.50.00

G12132-6-073273, 31.60.00

VHIU

-1

2.5A, PP5, EFN-38

G12132-5-073273, 30.30.00

PITOT H

EAT7.5A, PP5, EFN

-39

2.5A, PP5, EFN-40

G12132-3-073273, 29.00.00

HYD

RAU

LICS

7.5A, PP5, EFN-36


2.5A, PP6, EFN-N

/A-3

DIR

ECT BATT

G12132-10-073273, 24.30.00

7.5A, PP6, EFN-62

W/S W

IPER-2

G12132-8-073273, 30.42.00

VHIU

-2

G12132-13-073273 A


GA107 1

RBH 10/10/07

RBH 10/10/07

GA 10/10/07

CLB 10/10/07

Effectivity: AS350B2 Embodying Mod 350A07-3273


2.5A, PP5, EFN-49

G12132-7-073273

7.5A, PP5, EFN-46

2.5A, PP5, EFN-48

G12132-7-073273

HOIST REL.G12132-7-073273

VEMD-12.5A, PP6, EFN-65

SPAREG12132-8-073273

ATTITUDE


DIR. GYROG12132-10-073273

G12132-4-073273POSITION LTS7.5A, PP6, EFN-87

7.5A, PP6, EFN-83

ANTI-COL LTG12132-4-073273

G12132-4-073273

7.5A, PP6, EFN-79

TAXI LIGHT

CABIN LTSG12132-9-073273

2.5A, PP6, EFN-76


DIR BATTG12132-10-073273

7.5A, PP6, EFN-67

G12132-5-073273

7.5A, PP6, EFN-68

G12132-5-073273

FUEL PUMP-2

FUEL PUMP-1

7.5A, PP6, EFN-66

G12132-5-073273SAND FILTER

STROBE LT

G12132-4-073273

VHIU-1G12132-6-073273

G12132-6-073273

7.5A, PP5, EFN-42

SPARE

INST. LTS-1

G12132-6-073273

PITOT HEATG12132-5-073273

HOOK REL.

CRANK

G12132-8-073273

G12132-3-073273

2.5A, PP6, EFN-64

NTL IND.

7.5A, PP6, EFN-62

W/S WIPER-2G12132-8-073273

2.5A, PP6, EFN-63

G12132-4-073273

7.5A, PP5, EFN-45

10A, PP5, EFN-43

G12132-8-073273

G12132-8-073273

2.5A, PP6, EFN-61

FUEL FLOW

FUEL GAUGE

2.5A, PP6, EFN-59

VHIU-2G12132-8-073273

2.5A, PP6, EFN-60

2.5A, PP5, EFN-41

2.5A, PP5, EFN-40

7.5A, PP5, EFN-39

HYDRAULICSG12132-3-073273

G12132-6-073273

WARN PNL-1G12132-6-073273

G12132-7-073273

WARN PNL-2G12132-7-073273

2.5A, PP6, EFN-58

EXT. LOAD

7.5A, PP6, EFN-55

VEMD-2G12132-7-073273

2.5A, PP6, EFN-56

2.5A, PP5, EFN-38

ROTOR TACH

2.5A, PP5, EFN-37

7.5A, PP5, EFN-36

FWD


G12132-13-073273-P122 A


GA107 1

RBH 10/10/07

RBH 10/10/07

GA 10/10/07

CLB 10/10/07

71.61.10 29.00.00

28.00.00 31.50.00

28.00.00 25.80.00 62.30.00

30.30.00

33.10.00 28.00.00 25.80.00

33.43.00 28.41.10

33.42.00 30.42.00

33.41.00 80.00.00 33.10.00

34.20.00 77.00.00 33.41.00

25.63.00

34.20.00

Effectivity: AS350B2 - Embodying Mod 350A07-3273


24.30.00

31.60.00

31.60.00

31.60.00

31.60.00

31.50.00

MS2

4524

-23

AVIO

NIC

S

FWD

Opt

iona

l

Opt

iona

l

G12

132-

10-0

7327

3, 2

5.26

.00

10A,

PP9

, EFN

-94

STAR

T

CAR

GO

HO

OK

PWR

OU

TLET

G12

132-

5-07

3273

, 30.

42.0

0

W/S

WIP

ER-1

15A,

PP9

, EFN

-92

7.5A

, PP9

, EFN

-91

G12

132-

10-0

7327

3, 2

5.80

.00

15A,

PP9

, EFN

-93

Opt

iona

l

?A, P

P15,

LM

B-2

Opt

iona

l?A

, PP1

5, L

MB-

8

?A, P

P15,

LM

B-9

20A,

PP9

, EFN

-95

G12

132-

4-07

3273

, 33.

43.0

0

LAN

DIN

G L

T15

A, P

P9, E

FN-9

7G

1213

2-10

-073

273,

24.

22.0

0

AC IN

VER

TER

2.5A

, PP9

EFN

-57

HO

IST

2.5A

, PP9

, EFN

-N/A

-1TU

RN

& B

ANK

G12

132-

7-07

3273

, 25.

63.0

0

G12

132-

10-0

7327

3

?A, P

P15,

LM

B-3

G12

132-

10-0

7327

3, 8

0.00

.00

Opt

iona

l

Opt

iona

l

?A, P

P15,

LM

B-7

?A, P

P15,

LM

B-6

Opt

iona

l

?A, P

P15,

LM

B-5

?A, P

P15,

LM

B-4

Opt

iona

l

Opt

iona

l

Opt

iona

l

?A, ?

bus,

LTB

-9

Opt

iona

l

?A, ?

bus,

LTB

-12

Opt

iona

l

?A, ?

bus,

LTB

-11

Opt

iona

l

?A, ?

bus,

LTB

-10

G12

132-

2-07

3273

, ESN

-1

BAT-

EXT

PWR

MS2

4659

-23D

MS2

4523

-23

FUEL

PU

MP

1G

1213

2-5-

0732

73, E

SN-2

W/S

WIP

ERG

1213

2-5-

0732

73, E

SN-2

4

FUEL

PU

MP

2G

1213

2-5-

0732

73, E

SN-8

MS2

4524

-23

SAN

D F

ILTE

RG

1213

2-5-

0732

73, E

SN-2

1

Opt

iona

l

Opt

iona

l

?A, ?

bus,

LTB

-8

Opt

iona

l

?A, ?

bus,

LTB

-7

Opt

iona

l

?A, ?

bus,

LTB

-6

?A, ?

bus,

LTB

-5

Opt

iona

l

Opt

iona

l

?A, ?

bus,

LTB

-4

?A, ?

bus,

LTB

-3

?A, ?

bus,

LTB

-1

Opt

iona

l

?A, ?

bus,

LTB

-2D

IREC

T BA

TTG

1213

2-2-

0732

73, O

P-2

MS2

4523

-23

MS2

4523

-23

MS2

4523

-23

G12

132-

5-07

3273

, OP-

1

G12

132-

12-0

7327

3

G12

132-

12-0

7327

3

G12

132-

12-0

7327

3

G12

132-

12-0

7327

3

G12

132-

12-0

7327

3

G12

132-

12-0

7327

3

G12

132-

12-0

7327

3

G12

132-

12-0

7327

3

G12

132-

12-0

7327

3

G12

132-

12-0

7327

3

G12

132-

12-0

7327

3

G12

132-

12-0

7327

3

G12

132-

12-0

7327

3

G12

132-

12-0

7327

3

G12

132-

12-0

7327

3

G12

132-

12-0

7327

3G

1213

2-12

-073

273

G12

132-

12-0

7327

3

G12

132-

12-0

7327

3

G12

132-

12-0

7327

3


2.5A

, PP9

, EFN

-70

HO

UR

MET

ERG

1213

2-9-

0732

73, 3

1.31

.00

10A,

PP1

5, E

FN-7

5IN

ST.L

TS-2

G12

132-

4-07

3273

, 33.

10.0

0

3A, P

P15,

EFN

-N/A

-4D

-BAT

CTR

LG

1213

2-10

-073

273,

24.

30.0

0

G12132-14-073273 A


GA107 1

RBH 10/10/07

RBH 10/10/07

GA 10/10/07

CLB 10/10/07


ADDED EFN-N/A-4 WDM REFERENCECORRECTED BUS FOR EFN-N/A-1;A RBH05/06/08

D-BAT CTRL3A, PP15, EFN-N/A-4

Optional

Optional

?A, ?bus, LTB-1

?A, ?bus, LTB-2

?A, ?bus, LTB-3

Optional

?A, PP15, LMB-4

?A, PP15, LMB-9

Optional

?A, PP15, LMB-8

INST LTS 210A, PP15, EFN-75

Optional

Optional?A, PP15, LMB-5

?A, PP15, LMB-6


Optional


Optional

Optional

?A, PP15, LMB-3

Optional

Optional


?A, ?bus, LTB-5

?A, ?bus, LTB-6

Optional

?A, ?bus, LTB-7

Optional

?A, ?bus, LTB-8

?A, ?bus, LTB-9

Optional

Optional

Optional

?A, ?bus, LTB-10

Optional

?A, ?bus, LTB-11

?A, ?bus, LTB-12


HOUR METERG12132-9-073273

2.5A, PP9, EFN-70

G12132-7-073273

2.5A, PP9, EFN-57

G12132-10-073273

HOIST

15A, PP9, EFN-97

LANDING LTG12132-4-073273

20A, PP9, EFN-95

G12132-10-073273

10A, PP9, EFN-94

AC INVERTERG12132-10-073273

START

7.5A, PP9, EFN-91

W/S WIPER-1G12132-5-073273

15A, PP9, EFN-93

G12132-10-073273

15A, PP9, EFN-92

PWR OUTLET

CARGO HOOK

G12132-10-073273

FWD

G12132-4-073273G12132-12-073273

G12132-12-073273

G12132-12-073273

G12132-12-073273

G12132-12-073273

G12132-12-073273

G12132-12-073273

G12132-12-073273

G12132-12-073273

G12132-12-073273

G12132-12-073273

G12132-12-073273

G12132-10-073273

G12132-12-073273

G12132-12-073273

G12132-12-073273

G12132-12-073273

G12132-12-073273

G12132-12-073273

G12132-12-073273

G12132-12-073273


G12132-14-073273-P122 A


GA107 1

RBH 10/10/07

RBH 10/10/07

GA 10/10/07

CLB 10/10/07

31.31.00

25.63.00

24.22.00

33.43.00

80.00.00

25.26.00

25.80.00

30.42.00


33.10.00

CORRECTED BUS FOR EFN-N/A-1;ADDED EFN-N/A-4 WDM REFERENCE

A RBH05/06/08

24.30.00


CRANKENGINE

CR

AN

K E

NG

INE


WIPER

FILTER

DIRECTBATTERY

AVIONICSMASTER

AVIONICS

MS24523-23

MS24524-23

G12132-5-073273, OP-1

G12132-2-073273, OP-2DIRECT BATT

W/S WIPERMS24523-23

MS24524-23

SAND FILTERG12132-5-073273, ESN-21

G12132-5-073273, ESN-24

SAND

FUEL

BAT-EXTPOWER

WINDSHIELD

BAT-EXT PWR

FUEL PUMP 1

MS24523-23

FUEL PUMP 2G12132-5-073273, ESN-8

G12132-5-073273, ESN-2

MS24523-23

MS24659-23D

G12132-2-073273, ESN-1

HY

D T

EST

GE

NE

RA

TOR

ON

MS

2452

4-31

MS

2465

8-23

D

WA

RN

/ FI

RE

TE

ST

MS

2452

3-26

G12

132-

3-07

3273

, ES

N-3

G12

132-

3-07

3273

, ES

N-1

1

G12

132-

3-07

3273

, ES

N-7

GENERATORON / RESET

PUMP 2

FUELPUMP 1

WARN/FIREHYDTEST TEST

LIGHTS

G12132-15-073273 A


GA107 1

RBH 10/10/07

RBH 10/10/07

GA 10/10/07

CLB 10/10/07

MS24524-23

MS24524-21

MS24524-23

MS24523-23

LANDING LT

TAXI LIGHT

ANTI-COL LT

POSITION LTS

G12132-4-073273, ESN-18

G12132-4-073273, ESN-17

G12132-4-073273, ESN-9

G12132-4-073273, ESN-10

LIGHTTAXI

LIGHTLANDING

ALL / TAILANTI-COL

MS24524-23

MS24524-23

MS24524-23

WARNING HORN

INST. LTS-1

INST. LTS-2

G12132-3-073273, ESN-12

G12132-4-073273, ESN-14

G12132-4-073273, ESN-15M

AS

TER

CU

TOFF

MS

2452

3-23

MS

2465

9-23

D

PITO

T H

EAT

G12

132-

3-07

3273

, ES

N-5

G12

132-

2-07

3273

, ES

N-6

G12

132-

5-07

3273

, ES

N-1

3

MASTERCUTOFF HEAT

PITOT

POSITION

INSTRUMENTLIGHTS 2

HORNWARNING

INSTRUMENTLIGHTS 1

MS

2740

7-3



G12132-3-073273ESN-5, MS24523-26

P122 CONSOLE LAYOUT

G12132-5-073273

G12132-4-073273ESN-17, MS24524-23

ESN-13, MS24523-23

ESN-15, MS24524-23G12132-4-073273

G12132-5-073273OP-1, MS24524-23

G12132-4-073273

AVIONICSMASTER

ESN-14, MS24524-23 ESN-10, MS24524-23G12132-4-073273 G12132-4-073273

ESN-9, MS24524-21

PANELDIMMER

FUELPUMP 2

GENERATORON / RESET

G12132-3-073273ESN-3, MS24524-31

INSTRUMENTLIGHTS 2

G12132-5-073273ESN-8, MS24523-23

G12132-5-073273

INSTRUMENTLIGHTS 1

ESN-2, MS24523-23

FUELPUMP 1

ESN-1, MS24659-23DG12132-2-073273

BAT-EXTPOWER

G12132-3-073273ESN-11, MS24658-23D

ESN-21, MS24524-23G12132-5-073273

POSITIONLIGHTS

SANDFILTER

ANTI-COLALL / TAIL

ESN-24, MS24523-23G12132-5-073273

WINDSHIELDWIPER

G12132-3-073273ESN-7, MS27407-3

HYDRAULICTEST

WARN / FIRETEST

DIRECTBATTERY

ESN-18, MS24523-23G12132-4-073273

OP-2, MS24523-23G12132-2-073273

WARNINGHORN

G12132-2-073273ESN-6, MS24659-23D

LANDINGLIGHT

ESN-12, MS24524-23G12132-3-073273

TAXILIGHT

PITOTHEAT

MASTERCUTOFF

CRANKENGINE

G12132-15-073273-P122 A


GA107 1

RBH 10/10/07

RBH 10/10/07

GA 10/10/07

CLB 10/10/07A CHANGED ESN-7 TYPE & WIRING 03/23/09 RBH


MS24659-23D

G12132-5-11

AN16ga

AVIONICS MASTER

G12132-5-12

G12132-5-13


RELAYAVIONICS

PP128 ga.50A

AVIONICSA1

UU(no connection)X1

(Airframe GND)

X2

W

V

W

V


(no connection)

8 ga.

A2

TB4

T

P2

AN16gaT

J2

G12132-5-10


ALT. ENCODER

2.5A

TRANSPONDER

2.5A

AUDIO PANEL

2.5A

10A

COM2

CD CHANGER

2.5A

5A

GPS

10A

COM1 STEREO ICS

2.5A



G12132-10-05

AN16ga

AN16ga

1

2

3

4

5

6

OP-1 bb


15A

J2

EFN-97

P2

FROM G12132-10-073273

AN16ga


G12132-8-04

AN16ga

AN16ga

G12132-5-13

G12132-5-12

G12132-5-10

QQ

P2

W W

VV

J2

U

TT

U


J2

EFN-62

P2

15A

1

2

3

4

5

6

AN16ga

MS24524-23

G12132-5-11

AN16ga

FROM G12132-8-073273

AVIONICS MASTEROP-1

AN16ga

FROM G12132-5-073273

G12132-16-073273 --

AVIONICS SAMPLE CIRCUITSP132 and P122 CONSOLE WIRING

RBH 10/10/07

CLB 10/10/07

GA107 1

G12132-16-04AN16ga

AN16gaG12132-16-03




AVIONICS-1 BUS

AVIONICS-2 BUS

G12132-16-01 AN16ga

G12132-16-02 AN16ga

42

42

42 Alternatively, separate AVIONICS-1 and AVIONICS-2 bus breakers may be mounted in the optional rails, or in an installer-defined location outside the console, and powered separately.

FROM G12132-5-073273



1ME3E

tt

From G12132-6-073273

G12132-17-01


ref: WDM 25.80.00 PP5

P1

EFN-40

J1

HOOK RELEASE

2.5A

G12132-6-06

3

2

1



J?

??

??

P?

MS24523-23

??

??


CARGO HOOK???

G12132-?-??

G12132-?-??

G12132-17-073273 --


RBH 10/10/07

CLB 10/10/07

GA107 1


ref: WDM 25.80.0043

There is no standard switch assigned to the CARGO HOOK function in the -073273 version of the console. If a CARGO HOOK circuit is required, implement it using an available optional switch, or using a switch mounted in an installer-defined location outside the console, assigning unique wire numbers as appropriate.

43



From G12132-7-073273

ref: WDM 25.63.00PP9

P2

F

EFN-57

F

J2

HOIST

G12132-7-09

G12132-18-02


ref: WDM 25.63.00

J2P2

N N

EFN-48

2.5A

G12132-7-04

PP5HOIST RELEASE

G12132-?-??



1ME36E

??

??

??

??

G12132-?-??

G12132-?-????

??

MS24524-23

1

2

3

4

5

6


G12132-18-01J?P?

??

G12132-?-??

??

???HOIST

G12132-18-073273 --


RBH 10/10/07

CLB 10/10/07

GA107 1

300lb UNIT: 1ME33E450lb UNIT: 1ME101E


RATINGCAPACITY

300lb450lb

227.5A2.5A

22

There is no standard switch assigned to the HOIST function in the -073273 version of the console. If a HOIST circuit is required, implement it using an available optional switch, or using a switch mounted in an installer-defined location outside the console, assigning unique wire numbers as appropriate.

44

44



G12132-2-19

DIRECT BATTERY

EMER BUS BAR, Middle Right AftG12135-2


EMERGENCY-FADEC

FADEC CONTROL

1A

EFN-71E D5:A

G12132-2-08

D5:C

1A

PP9

EMER BUS BAR

2.5A

EFN-57

EFN-72K

EMER BUS BAR

G12132-2-10 AN16ga

G12132-2-14

D4:A

D2:A

G12132-2-12

D2:C

D4:C

ref: AEC DWG 350A62-0046-00ref: AEC DWG 350A62-4101-00ref: AEC DWG 350A67-0301-01ref: AEC DWG 350A67-0302-02

1

2

3

4

5

6

MS24659-23D

MASTER CUTOFF


ref: WDM 62.30.00

ref: WDM 80.00.10ref: WDM 77.00.10

ref: WDM 24.30.00

P1 J1

G12132-2-07

ESN-6

G12132-2-18

D7:C

D6:C

3PE28E

1PE2F (if installed) and 1PE2E

1PG6NE

1PG1NE

1PG3NE

1PG2NE

zz

X

Y Y

X

W

S

R R

S

W

D7:A

D6:A

G12132-2-20

G12132-2-06

G12132-2-05

G12132-2-04

G12132-2-02

G12132-2-03

1

2

3

4

5

6

MS24659-23D

BAT-EXT PWR

G12132-2-01

ESN-1

MS24523-23

G12132-2-073274 B


RBH 10/10/07

CLB 10/10/07

GA107 1

P2J2G12132-2-15

F F 3EU3F

3EU18E

G12132-2-13

G12132-2-17

Z Z

G12132-2-09 T T

J1 P1

1KK115E and 1KK128E



3PW52E

DIRECT BATTERY(+28V VOYANT)


3

2

1

OP-2

ADDED AIRFRAME WIRE 1PE2FA 03/04/10 RBHADDED 3EU88E CONNECTIONSB 05/12/10 RBH

3EU88E (post-mod 350A07-3368 & -3476 only)G12132-2-11 f f



ref: AEC DWG 350A67-0305-02

CORRECTED HORN SWITCH WIRINGA

ref: WDM 62.30.00

1EW93NE

1EW37E

1EW38E

1EW39E

n

m m

n

k

jP1

k

jJ1

05/06/08 RBH

G12132-3-161

2

3

4

5

6

G12132-3-15

G12132-3-14

MS24524-23

G12132-3-17

WARNING HORNESN-12


G12132-3-08

G12132-3-07

G12132-3-06

G12132-3-02

The Generator switch has a center off position. The forward position provides the normal GENERATOR ON function. The momentary aft position provides the GENERATOR RESET function.

PP1KK53E

1PA1E

1PA2E

N

M

N

M

1KK55E

1PA4E

P1 J1

U

V

U

V

ref: WDM 80.00.10ref: WDM 24.30.00

G12132-3-01


3 6

3

2

1

MS24523-26

G12132-3-05

ESN-5CRANK

PP6


G12132-3-03ESN-3

1

2

4

5


G12132-3-073274 F


RBH 10/10/07

CLB 10/10/07

GA107 1


G12132-3-09

ref: AEC DWG 350A67-6092-00

G12132-3-13

G12132-3-12

G12132-3-10

G12132-3-11

3

2

1

CRANK

2.5A

EFN-63

S S

J2

R

P2

R

J1

SINGLE: MS24658-23D

F

P1

F

ESN-11

D1:A

EFN-36

HYDRAULICS

D1:C

7.5A

PP5

ADDED ESN-11 COLOR CODINGB 09/25/08 RBH


NOTE: Diodes on wires 1WW82E (REF: 30ALP-D02) and 1WW2NE (REF: 30ALP-D01) must be implemented outside the console

ref: WDM 31.50.00

C CHANGED ESN-7 TYPE & WIRING; 03/23/09 RBHADDED DUAL HYD AIRFRAME WIRES

1DH1E and

TYPEDUAL

WIRE #(none)

1DH5ESINGLE

TYPEDUAL

WIRE #1DH50E

1DH6NESINGLE1DH93NE

TYPEDUAL

WIRE #

G12132-3-22

d d

1WW1E E

P2

E

J2

b

c

P1

ee

1

2

3

4

5

6

G12132-3-18

G12132-3-19

G12132-3-20b

c


WARN / FIRE TEST

G12132-3-21

G12132-3-04

J1

ee

ESN-7

WARN PANEL 1

GND for OVERLAYS

2.5A

EFN-37

PP5

G12132-23-09

WIRE #1DH6E(none)

1PE4NE or GND

1WW38E

TYPEDUAL

SINGLE

1WW2NE

1WW82E


INTERNALIZED 1WW1F CIRCUIT


ADDED EFN-7 NOTESDH112E TO HYDRAULICS CIRCUIT;

D 03/04/10 RBHAIRFRAME WIRES; ADDED WIREADDED SHIELD NOTE FOR ESN-12



1DH112ESINGLE(if installed)

ref: WDM 29.10.20ref: WDM 29.00.00

HYD TEST

ref: WDM 31.60.00ref: WDM 26.10.00

CHANGED ESN-11 SWITCH TYPEE 04/12/17 GA

DUAL: MS24658-26F

ACCU TST or

ADDED ACCU TST OPTION 10/20/17 GAF


ref: AEC DWG 350A64-7308-00

MS24524-21



STROBE LIGHT

7.5A

EFN-45

PP9

ref: WDM 33.42.00

ANTI-COL LT

EFN-83

G12132-4-17

7.5A

1

2

3

4

5

6

(Center off)

G12132-4-21

ESN-9PP6




G12132-4-13

G12132-4-14



1

2

3

4

5

6

MS24524-23

1LJ1E B

P2

B

J2

ESN-10POSITION LIGHTS

G

P2

G

J2

PP6 POSITION LTS

7.5A

EFN-87

G12132-4-16

G12132-4-15


ESN-17TAXI LIGHT

1

2

3

4

5

6

MS24524-23

TAXI LIGHT

7.5A

EFN-79

PP61LM7E


LM5NE

The original LANDING LIGHT circuit MUST be rewired to match this diagram. The diode is optional. Another switch and location may be substituted for the switch and location specified, with appropriate labeling. If an alternate location is used forthe LANDING LIGHT switch, then the switch and position specified here may be used for another circuit, with appropriate labeling.

40L or 118L

LM1E

q q

p

J1 P1

p

AN16ga.LM6E

LM6E-1

J2

ZY

P2G12132-4-01

G12132-4-04ZY

AN16ga.

This circuit is optional, at the installer's discretion. The landing light switch can be located on the Pilot's Collective Grip if desired.



EFN-95

LANDING LIGHTPP9

20A

1LM2E

INST. LTS-1PP5

1

2

3

4

5

6

DD1LK636E

1LK23E d d

e e

1LK640E

1LK633E

g g

1LK641E

1LK44E

1LK634E C C

P2

f

K K

f

J2

G12132-4-12 16ga.

G12132-4-25 16ga.

ESN-15

1

2

3

4

5

6

INSTRUMENT LIGHTS 2

MS24524-23

G12132-4-24 16ga.

G12132-4-10 18ga.

G12132-4-09

G12132-4-08 16ga.

G12132-4-05 18ga.

G12132-4-06 18ga.

G12132-4-11 16ga.

PP15

G12132-4-07 16ga.

10A

EFN-75

INST. LTS-2

EFN-43

10A


ESN-14INSTRUMENT LIGHTS 1



G12132-4-02

G12132-4-03


G12132-4-19

G12132-4-20



1LX10EG12132-4-18

H

P2

L

H

J2

L

G12132-4-073274 --


RBH 10/10/07

CLB 10/10/07

GA107 1

3

2

1

MS24523-23

LANDING LIGHTESN-18

ALL / TAILANTI-COLLISION LIGHT


18ga.

MS24524-23

G12132-23-02 18ga.

G12132-23-01 18ga.





ref: AEC DWG 350A67-6091-00

Installer Defined

Installer Defined

Installer Defined

Installer Defined

U U

G12132-5-13 AN16ga.

G12132-5-12 AN16ga.

W

V

W

V

AVIONICS MASTER

1

2

3

4

5

6

MS24524-23

G12132-5-11AN16ga

G12132-5-10

T

P2

T

J2

AN16ga

OP-1

NOTE: If a FUEL PUMP indicator light is required, the installer shall provide a suitable light and install it within clear view of the pilot, with an appropriate label.

ref: WDM 30.30.00

ref: AEC DWG 350A67-0306-02

(ref: 21Q) 1QN1E

PP5

1FN1E

G12132-5-033

2

1

J2

MS24523-23

A

P2

A

G12132-5-04

PITOT HEATESN-13

ref: WDM 28.00.00

1QW1G

7.5A

EFN-39

PITOT HEAT

DD

P1

DD

J1

G12132-5-02

G12132-5-013

2

1

MS24523-23

FUEL PUMPESN-2

EFN-67

7.5A

FUEL PUMPPP6

G12132-5-091KS2E yy

G12132-5-073274 B


RBH 10/10/07

CLB 10/10/07

GA107 1




1

2

3

4

5

6

MS24524-23

G12132-5-08

SAND FILTER

MS24523-26

Installer Defined

Installer Defined

1KS3E

G12132-5-21

P1 J1

HH

GG

G12132-5-22

P1

x

HH

GG

J1

x

ESN-21


G12132-5-20

G12132-5-05

G12132-5-063

2

1

OP-3SERVO TEST

BB

FF

CC

J1

SAND FILTER

G12132-5-07

EFN-66

7.5A

PP6

1DH74E

1DH14E

1DH70NEBB

FF

CC

P1

A CHANGED OP-3 LABEL & WIRING 03/23/09 RBH

EFN-91


1MK1E Blue

1MK1E Red

G12132-5-173

2

1

G12132-5-14

G12132-5-18

P

M

P2

P

M

J2

MS24523-23

W/S WIPERESN-24

PP9

7.5A

W/S WIPER


1LK639E

1FW2E

B ADDED PITOT INDICATOR LIGHT 03/04/10 RBH



NR/NFref: WDM 77.00.10 PP5

PITOT HEAT


ref: WDM 39.00.00ref: WDM 62.30.00

3EU3E

PP5

7.5A

EFN-39

G12132-6-03P1

A A

J1

EFN-38

2.5A

HYDRAULICS

WARNING PANEL 1


ref: AEC DWG 350A67-0301-00

PP5

EFN-37

2.5A

PP5

7.5A

EFN-36

G12132-6-073274 A


RBH 10/10/07

CLB 10/10/07

GA107 1

10A

EFN-43

INST. LTS-1

7.5A

EFN-42

ref: WDM 80.00.10



1KK46E Red v

P1

GOV A


v

PP5

G12132-6-05J1

PP5

EFN-41

2.5Aref: WDM 39.00.00ref: WDM 31.41.00ref: AEC DWG 350A61-2643-01

1WW72E

P1

D

ASU1-3

G12132-6-04J1

D

PP5

MOVED EFN-37 WIRING OFF PAGEA RBH03/23/09



STROBE LIGHT


EFN-45

7.5A

PP9

G12132-7-01



EFN-58

2.5A

EXT. LOAD

1ME87E w

P1 J1

w

PP9

EFN-57

2.5A

FADEC CONTROL PP9For optional uses, this breaker may be up to 15 amps.ref: WDM 25.80.00

ref: WDM 25.63.00

ref: WDM 39.00.00ref: WDM 34.20.00

Installer Defined

Installer Defined

ref: AEC DWG 350A68-2542-01

G12132-7-05u u

G12132-7-04

ATTITUDE GYRO

2.5A

J1

EFN-49

P1

PP5

J2

N

P2

N

EFN-48

2.5AAN16ga


ref: WDM 39.00.00

ref: WDM 31.60.00ref: WDM 39.00.00

EW30E or 1EW30E

ref: AEC DWG 350A67-0303-04

ref: AEC DWG 350A63-5017-00

G12132-7-03

RELEASE PP5

s s

VEMD-1

7.5A

J1

EFN-46

P1

PP5

K

P1

EFN-55

VEMD-2

EFN-56

WARNING PANEL 2

P1

E

ref: AEC DWG 350A62-0046-00

ref: WDM 31.50.00ref: WDM 39.00.00

1WW31E

ref: AEC DWG 350A67-0303-04

ref: WDM 31.60.00ref: WDM 39.00.00

1EW35E

G12132-7-08E

J1

PP6

2.5A

G12132-7-07K

J1

PP6

7.5A


ref: AEC DWG 350A63-6158-00

D3:C

D3:A

G12132-7-073274 --


RBH 10/10/07

CLB 10/10/07

GA107 1


G12132-7-06


ref: WDM 39.00.00

1KK137E Red

ref: WDM 80.00.102.5A

EFN-61

r

P1G12132-8-03

r

J1

1QW1E

1KK51E

ref: WDM 39.00.00ref: WDM 28.00.00

ref: WDM 80.00.10ref: WDM 39.00.00

G12132-8-01

GOV. INDIC.

C

P1

PP6

G12132-8-02C

J1

2.5A

EFN-60

FUEL GAUGE

B

PP6

B

EFN-59

7.5A

P1

ENG CTL

J1

PP6



ref: WDM 77.00.10ref: WDM 39.00.00

SAND FILTER

EFN-66

7.5A

1EM35E Red

J1P1

i i

2.5A

EFN-65

G12132-8-06

PP6

PP6

PP6ref: WDM 80.00.10

1KK138E Red

ENG. P.

L

P1

L

J1

EFN-64

7.5A

GOV B

CRANK

2.5A

EFN-63

G12132-8-05

ref: WDM 39.00.00

ref: AEC DWG 350A67-0302-02

ref: AEC DWG 350A67-0306-02

ref: AEC DWG 350A67-0302-02

ref: AEC DWG 350A67-0302-02

ref: AEC DWG 350A67-0301-01



G12132-8-073274 --


RBH 10/10/07

CLB 10/10/07

GA107 1


2.5A

ref: WDM 39.00.00

1DT5E


ref: WDM 31.31.00


EMER BUS BAR

EFN-72K

EMERGENCY FADEC

1A

EMERGENCY NR INDICATOR

EFN-71E

1A

EMER BUS BAR

G12132-9-02H H

EFN-70

P1 J1

FUEL PUMP

1WW34E

ref: WDM 39.00.00ref: WDM 31.41.00


P1 J1G12132-9-01

PP9HOUR METER

AA AA

PP6

2.5A

EFN-68

ASU1-2

PP6

EFN-67

7.5A



POSITION LTS

EFN-87

7.5A



PP6

EFN-83

ANTI-COL LT

PP6

7.5A

EFN-79

TAXI LIGHT

7.5A

G12132-9-03

ref: WDM 33.10.00ref: WDM 39.00.00

P1

J1LE1E J

J1

CABIN LIGHTS

EFN-76

PP6

2.5A


INST. LTS-2

EFN-75

PP15

10A

ref: AEC DWG 350A61-2643-01

ref: AEC DWG 350A67-6087-00



G12132-9-073274 A


RBH 10/10/07

CLB 10/10/07

GA107 1

CORRECTED TYPO ON EFN-72KA RBH05/06/08



Detailed on G12132-4-073274LANDING LIGHT

ref: AEC DWG 350A67-0302-02


ref: WDM 39.00.00ref: WDM 80.00.10

1KW4E

1MH1E

20A

05/06/08 RBH

EFN-95

G12132-10-03 AN16ga.

G12132-10-04 AN16ga.

EFN-94

PP9

P2

X

J2

X

PP9

10A

START

a

P2

a

J2

ref: AEC DWG 350A62-0045-00

ref: AEC DWG 350A63-6158-00

Detailed on G12132-5-073274W/S WIPER

CARGO HOOK

POWER OUTLETref: WDM 25.26.00

ref: WDM 39.00.00ref: WDM 25.80.00

1ME1E G12132-10-02 AN16ga.cc

PP9

15A

EFN-93

PP9

15A

EFN-92

P2 J2

PP9

EFN-91

7.5A

G12132-10-01


G12132-10-073274 C


RBH 10/10/07

CLB 10/10/07

GA107 1

G12132-10-09

G12132-10-08


3PW53E and 3PW55E g

P1

g

J1

ref: AEC DWG 350A62-4101-00

3PW54E and 3PW54F

ref: AEC DWG 350A62-4101-00

ref: WDM 24.30.00

ref: WDM 24.30.00

EFN-N/A-4

D-BAT CONTROL

P1

h

PP15

3A

h

J1

a

DIRECT BATTERY

EFN-N/A-3

(1FF210F)

PP6

2.5A

a


G12132-10-06

G12132-10-05 AN16ga.


G G

EFN-N/A-2

P1

DIR. GYRO

2.5A

J1

PP6

EFN-N/A-1

P1 J1

PP9

ref: AEC DWG 350A62-0049-00ref: WDM 39.00.00ref: WDM 24.22.00

P2

b

AC INVERTER

EFN-97

1XU1E b

J2

15A

PP9

2.5A

HYD MAIN

2.5A

REASSIGNED EFN-N/A-1B UPDATED EFN-94 AIRCRAFT WIRE; 03/02/09 RBH


C UPDATED EFN-N/A-1 CIRCUIT 03/23/09 RBH

DUALTYPE

SIMPLE1DH78F(none)

WIRE #







PP6 BUS BAR, Middle Right Fwd


BUS BAR, Top Left



AN8ga G12132-11-13TB4Installer Defined Option

1PP9E

3PP23E

TB6

TB5AN8ga G12132-11-14

AN8ga G12132-11-04

AN8ga G12132-11-15


ref: WDM 77.00.10ref: WDM 24.30.00

1PP6E

1PP5E

TB3

TB2

TB1AN8ga G12132-11-01

AN8ga G12132-11-02

AN8ga G12132-11-03


G12132-11-073274 A


RBH 10/10/07

CLB 10/10/07

GA107 1


G12135-10

G12135-12

G12135-9

G12135-2


ESN-6

MS24659-23D

1

2

3

4

5

6

MASTER CUTOFF

G12135-2

G12135-10

G12135-8

G12135-9

J1P1

f f(Post-Mod 350A07-3476 only) 3EU88EG12132-2-11

AN16ga G12132-2-10

ref: G12132-2-073274

A ADDED 3EU88E CONNECTIONS 05/12/10 RBH

MS24524-23

INST. LTS-1

2.5A, PP5, EFN-38

NR

/NF

2.5A, PP6, EFN-68

WAR

N PN

L 2

FWD

G12132-13-073274 b


GA107 1

RBH 10/10/07

RBH 10/10/07

GA 10/10/07

CLB 10/10/07


7.5A, PP6, EFN-59

2.5A, PP6, EFN-60

FUEL G

AUG

EEN

G C

TL


7.5A, PP6, EFN-64

7.5A, PP6, EFN-83

ANTI-C

OL LT

EMER

-NR

IND

DIR

. GYR

O2.5A, PP6, EFN

-N/A-2

7.5A, PP6, EFN-87

POSITIO

N LT

1A, EMER

BUS, EFN

-72K

EMER

-FADEC

1A, EMER

BUS, EFN

-71E

2.5A, PP6, EFN-65

ENG

P.

GO

V B

2.5A, PP6, EFN-76

CABIN

LTS

7.5A, PP6, EFN-79

TAXI LIGH

T

DIR

ECT BATT

2.5A, PP6, EFN-N

/A-3ASU

1-2

2.5A, PP6, EFN-61

GO

V IND

IC

2.5A, PP6, EFN-63

CR

ANK

TAXI LIGH

T

10A, PP9, EFN-94

FADEC

CTR

L

START

LAND

ING

LIGH

TM

S24523-23

ANTI-C

OL LT

POSITIO

N LTS

INST. LTS-2M

S24524-23

MS24524-21

INST. LTS-1

RELEASE

ATTITUD

E

2.5A, PP9, EFN-57

2.5A, PP5, EFN-49

2.5A, PP5, EFN-48

VEMD

-17.5A, PP5, EFN

-46

2.5A, PP5, EFN-41

7.5A, PP5, EFN-39

PITOT H

EAT

7.5A, PP5, EFN-42

GO

V A

10A, PP5, EFN-43

ASU1-3

MS24524-23

MS24524-23

7.5A, PP6, EFN-55

VEMD

-2

2.5A, PP6, EFN-56

7.5A, PP6, EFN-66

7.5A, PP6, EFN-67

FUEL PU

MP

SAND

FILTERH

YDR

AULIC

S

WAR

N PN

L 1

7.5A, PP5, EFN-36

2.5A, PP5, EFN-37

MS24524-23

WAR

NIN

G H

OR

N

G12132-4-073274, ESN

-18

G12132-4-073274, ESN

-17

G12132-4-073274, ESN

-15

G12132-4-073274, ESN

-9

G12132-4-073274, ESN

-10

G12132-4-073274, ESN

-14

G12132-3-073274, ESN

-12

G12132-3-073274, 29.00.00

G12132-3-073274, 31.50.00

G12132-6-073274, 62.30.00

G12132-6-073274, 31.41.00

G12132-6-073274, 80.00.10

G12132-5-073274, 30.30.00

G12132-7-073274, 31.60.00

G12132-7-073274, 25.80.00

G12132-4-073274, 33.10.00

G12132-7-073274, 34.20.00

G12132-2-073274, 80.00.10

G12132-10-073274, 80.00.10

G12132-7-073274, 31.60.00

G12132-7-073274, 31.50.00

G12132-8-073274, 28.00.00

G12132-8-073274, 80.00.10

G12132-8-073274, 80.00.10

G12132-8-073274, 80.00.10

G12132-3-073274, 80.00.10

G12132-8-073274, 77.00.10

G12132-2-073274, 80.00.10

G12132-2-073274, 77.00.10

G12132-5-073274, 71.61.10

G12132-5-073274, 28.00.00

G12132-9-073274, 31.41.00

G12132-10-073274, 24.30.00

G12132-9-073274, 33.10.00

G12132-4-073274, 33.42.00

G12132-4-073274, 33.43.00

G12132-4-073274, 33.41.00

G12132-10-073274, 34.20.00

ADDED EFN-N/A-3 WDM REFERENCEA 05/06/08 RBH03/23/09CHANGED EFN-37 WIRING PAGEB RBH

G12132-13-073274-P122 B


GA107 1

RBH 10/10/07

RBH 10/10/07

GA 10/10/07

CLB 10/10/07


ADDED EFN-N/A-3 WDM REFERENCEA


RBH05/06/08

G12132-10-073274

G12132-4-073274

34.20.00

33.41.00

7.5A, PP6, EFN-87

POSITION LTS

DIR. GYRO2.5A, PP6, EFN-N/A-2

G12132-8-07327477.00.10

G12132-3-073274

G12132-8-073274

2.5A, PP6, EFN-63

GOV B7.5A, PP6, EFN-64

CRANK

ENG P.2.5A, PP6, EFN-65

80.00.10

80.00.10

G12132-9-073274

G12132-4-073274

G12132-4-073274

33.42.00

33.43.00

33.10.00


ANTI-COL LT7.5A, PP6, EFN-83

G12132-10-073274

G12132-9-073274

24.30.00

31.41.00

ASU1-22.5A, PP6, EFN-68

DIR BATT2.5A, PP6, EFN-N/A-3

2.5A, PP6, EFN-76

CABIN LTSG12132-8-073274

G12132-8-073274

G12132-8-073274

2.5A, PP6, EFN-60

FUEL GAUGE

GOV INDIC2.5A, PP6, EFN-61

80.00.10

28.00.00

80.00.10

G12132-7-073274

G12132-7-073274

2.5A, PP6, EFN-56


WARN PNL-2

ENG CTL7.5A, PP6, EFN-59

31.50.00

31.60.00

G12132-5-073274

G12132-5-073274

28.00.00

71.61.10

SAND FILTER7.5A, PP6, EFN-66

FUEL PUMP7.5A, PP6, EFN-67

G12132-2-073274

G12132-2-073274EMER-NR IND1A, EMER, EFN-71E

EMER-FADEC1A, EMER, EFN-72K

77.00.10

80.00.10

FWD

G12132-7-073274

2.5A, PP5, EFN-48

2.5A, PP5, EFN-49

G12132-7-07327434.20.00

ATTITUDE

G12132-7-07327425.80.00

31.60.00

RELEASE

INST. LTS-1

7.5A, PP5, EFN-42

7.5A, PP5, EFN-46

G12132-4-07327433.10.00

VEMD-1

G12132-6-07327480.00.10

10A, PP5, EFN-43

GOV A

G12132-6-073274

7.5A, PP5, EFN-39

2.5A, PP5, EFN-41

PITOT HEAT

G12132-6-07327431.41.00

ASU1-3

G12132-5-07327430.30.00

62.30.00

7.5A, PP5, EFN-36

2.5A, PP5, EFN-37

2.5A, PP5, EFN-38

WARN PNL-1

HYDRAULICS

G12132-3-07327431.50.00

NR/NF

G12132-3-07327429.00.00

G12132-10-073274

FADEC CTRL2.5A, PP9, EFN-57

80.00.10

10A, PP9, EFN-94

START

G12132-2-07327480.00.10

CHANGED EFN-37 WIRING PAGEB RBH03/23/09

G12132-14-073274 B


GA107 1

RBH 10/10/07

RBH 10/10/07

GA 10/10/07

CLB 10/10/07


15A,

PP9

, EFN

-92

W/S

WIP

ERG

1213

2-5-

0732

74, 3

0.42

.00

CAR

GO

HO

OK

FWD

7.5A

, PP9

, EFN

-91

HO

UR

MET

ERH

YD M

AIN


AC IN

VER

TER

15A,

PP9

, EFN

-97

STR

OBE

LT

7.5A

, PP9

, EFN

-45

G12

132-

10-0

7327

4, 2

5.26

.00

G12

132-

10-0

7327

4, 2

5.80

.00

PWR

OU

TLET

15A,

PP9

, EFN

-93

G12

132-

4-07

3274

, 33.

41.0

0LA

ND

ING

LT

G12

132-

4-07

3274

, 33.

43.0

0

20A,

PP9

, EFN

-95

G12

132-

9-07

3274

, 31.

31.0

0

2.5A

, PP9

, EFN

-70

G12

132-

7-07

3274

, 25.

80.0

0

EXT.

LO

AD

2.5A

, PP9

, EFN

-58

G12

132-

10-0

7327

4, 2

4.22

.00

2.5A

, PP9

, EFN

-N/A

-1G

1213

2-10

-073

274,

29.

10.2

0

G12

132-

2-07

3274

, ESN

-1

MS2

4659

-23D

BAT-

EXT

PWR

G12

132-

5-07

3274

, ESN

-21

SAN

D F

ILTE

R

MS2

4524

-23

G12

132-

5-07

3274

, OP-

3

G12

132-

5-07

3274

, ESN

-24

W/S

WIP

ER

G12

132-

5-07

3274

, ESN

-2

FUEL

PU

MP

MS2

4523

-23

MS2

4523

-23

G12

132-

2-07

3274

, OP-

2

DIR

ECT

BATT

MS2

4523

-23

G12

132-

5-07

3274

, OP-

1

AVIO

NIC

S

MS2

4524

-23

10A,

PP1

5, E

FN-7

5IN

ST.L

TS-2

G12

132-

4-07

3274

, 33.

10.0

0?A

, PP1

5, L

MB-

9O

ptio

nal

G12

132-

12-0

7327

3?A

, PP1

5, L

MB-

8O

ptio

nal

G12

132-

12-0

7327

3?A

, PP1

5, L

MB-

7O

ptio

nal

G12

132-

12-0

7327

3?A

, PP1

5, L

MB-

6O

ptio

nal

G12

132-

12-0

7327

3?A

, PP1

5, L

MB-

5O

ptio

nal

G12

132-

12-0

7327

3?A

, PP1

5, L

MB-

4O

ptio

nal

G12

132-

12-0

7327

3?A

, PP1

5, L

MB-

3O

ptio

nal

G12

132-

12-0

7327

3?A

, PP1

5, L

MB-

2O

ptio

nal

G12

132-

12-0

7327

33A

, PP1

5, E

FN-N

/A-4

D-B

AT C

TRL

G12

132-

12-0

7327

3

Opt

iona

l

?A, ?

bus,

LTB

-1

G12

132-

12-0

7327

3

Opt

iona

l

?A, ?

bus,

LTB

-2

G12

132-

12-0

7327

3

Opt

iona

l

?A, ?

bus,

LTB

-3

G12

132-

12-0

7327

3

Opt

iona

l

?A, ?

bus,

LTB

-4

G12

132-

12-0

7327

3

Opt

iona

l

?A, ?

bus,

LTB

-5

G12

132-

12-0

7327

3

Opt

iona

l

?A, ?

bus,

LTB

-6

G12

132-

12-0

7327

3

Opt

iona

l

?A, ?

bus,

LTB

-7

G12

132-

12-0

7327

3

Opt

iona

l

?A, ?

bus,

LTB

-8

G12

132-

12-0

7327

3

Opt

iona

l

?A, ?

bus,

LTB

-9

G12

132-

12-0

7327

3

Opt

iona

l

?A, ?

bus,

LTB

-10

G12

132-

12-0

7327

3

Opt

iona

l

?A, ?

bus,

LTB

-11

G12

132-

12-0

7327

3

Opt

iona

l

?A, ?

bus,

LTB

-12

SER

VO T

EST

MS2

4523

-26

ADDED EFN-N/A-4 WDM REFERENCEA 05/06/08 RBH

G12

132-

10-0

7327

4, 2

4.30

.00

B EFN-N/A-1 & OP-3 NOW ASSIGNED 03/23/09 RBHTO DUAL HYDRAULICS FUNCTIONS

CARGO HOOK

PWR OUTLET

15A, PP9, EFN-92

15A, PP9, EFN-93

W/S WIPER7.5A, PP9, EFN-91

STROBE LT

AC INVERTER

20A, PP9, EFN-95

LANDING LT

15A, PP9, EFN-97

EXT. LOAD

G12132-10-073274

2.5A, PP9, EFN-58

HOUR METER


HYD MAIN

G12132-7-073274

G12132-10-073274

G12132-4-073274

G12132-10-073274

G12132-10-073274

G12132-5-07327430.42.00

25.80.00

25.26.00

33.43.00

24.22.00

25.80.00


FWD

ADDED EFN-N/A-4 WDM REFERENCEA


RBH05/06/08

OptionalG12132-12-073273

2.5A, PP9, EFN-70

G12132-9-07327431.31.00

7.5A, PP9, EFN-45

G12132-4-07327433.41.00

G12132-14-073274-P122 B


GA107 1

RBH 10/10/07

RBH 10/10/07

GA 10/10/07

CLB 10/10/07

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

?A, ?bus, LTB-12 10A, PP15, EFN-75

?A, PP15, LMB-9?A, ?bus, LTB-11

?A, ?bus, LTB-10 ?A, PP15, LMB-8







?A, ?bus, LTB-3 3A, PP15, EFN-N/A-4

?A, ?bus, LTB-2

?A, ?bus, LTB-1

24.30.00

D-BAT CTRLG12132-10-073274

G12132-4-07327433.10.00

INST LTS 2

RBH03/23/09ASSIGNED EFN-N/A-1 TO HYD MAINB

29.10.20


WIPER

G12132-5-073274, ESN-24

G12132-5-073274, ESN-21

DIRECT BATT

SAND FILTER

G12132-2-073274, OP-2

G12132-5-073274, OP-1

MS24524-23

MS24523-23

AVIONICSMASTER

AVIONICS

BATTERYDIRECT

MS24524-23

MS24523-23

W/S WIPER

SANDFILTER


G12132-2-073274, ESN-1

G12132-5-073274, ESN-2

BAT-EXT PWR

FUEL PUMP

G12132-5-073274, OP-3

WINDSHIELD

MS24659-23D

MS24523-23 PUMPFUEL

POWERBAT-EXT

G12

132-

5-07

3274

, ES

N-1

3

G12

132-

2-07

3274

, ES

N-6

G12

132-

3-07

3274

, ES

N-7

G12

132-

3-07

3274

, ES

N-5

G12

132-

3-07

3274

, ES

N-1

1

G12

132-

3-07

3274

, ES

N-3

PIT

OT

HE

AT

MS2

4659

-23D

MS2

4523

-23

MAS

TER

CU

TOFF

MS2

4523

-26

MS2

7407

-3

WAR

N /

FIR

E T

EST

CR

AN

K E

NG

INE

MS2

4658

-26F

MS2

4524

-31

GE

NE

RA

TOR

ON

HY

D T

EST

TESTWARN/FIRE

ON / RESETGENERATOR

TESTHYD

CUTOFFMASTER

ENGINECRANK PITOT

HEAT

LIGHTS

G12132-4-073274, ESN-10

G12132-4-073274, ESN-9

G12132-4-073274, ESN-17

G12132-4-073274, ESN-18

POSITION LTS

ANTI-COL LT

TAXI LIGHT

LANDING LT

LANDINGLIGHT

TAXILIGHT

MS24523-23

MS24524-23

ANTI-COLALL / TAIL MS24524-21

MS24524-23

G12132-4-073274, ESN-15

G12132-4-073274, ESN-14

G12132-3-073274, ESN-12

INST. LTS-2

INST. LTS-1

WARNING HORN

LIGHTS 2INSTRUMENT

POSITION

MS24524-23

LIGHTS 1INSTRUMENT

WARNINGHORN

MS24524-23

MS24524-23

G12132-15-073274 C


GA107 1

RBH 10/10/07

RBH 10/10/07

GA 10/10/07

CLB 10/10/07

OP-3

SERVOTESTMS24523-26

SET OP-3 LABEL FOR DUAL HYDCHANGED ESN-7 SWITCH TYPE,A 03/23/09 RBH

B CHANGED ESN-11 SWITCH TYPE, 04/12/17 GAADDED ACCU TST NOTE

Note: HYD TEST switch may be marked ACCU TST

C 10/20/17 GA


G12132-3-073274ESN-5, MS24523-26

P122 CONSOLE LAYOUT

G12132-5-073274

G12132-4-073274ESN-17, MS24524-23

ESN-13, MS24523-23

ESN-15, MS24524-23G12132-4-073274

G12132-5-073274OP-1, MS24524-23

G12132-4-073274

AVIONICSMASTER

ESN-14, MS24524-23


ESN-10, MS24524-23G12132-4-073274 G12132-4-073274

ESN-9, MS24524-21

PANELDIMMER

SERVOTEST

GENERATORON / RESET

G12132-3-073274ESN-3, MS24524-31

INSTRUMENTLIGHTS 2

G12132-5-073274OP-3, MS24523-26

G12132-5-073274

INSTRUMENTLIGHTS 1

ESN-2, MS24523-23

FUELPUMP

ESN-1, MS24659-23DG12132-2-073274

BAT-EXTPOWER

G12132-3-073274ESN-11, MS24658-26F

ESN-21, MS24524-23G12132-5-073274

POSITIONLIGHTS

SANDFILTER

ANTI-COLALL / TAIL

ESN-24, MS24523-23G12132-5-073274

WINDSHIELDWIPER

G12132-3-073274ESN-7, MS27407-3

HYDTEST

WARN / FIRETEST

DIRECT BATTERY

ESN-18, MS24523-23G12132-4-073274

OP-2, MS24523-23G12132-2-073274

WARNINGHORN

G12132-2-073274ESN-6, MS24659-23D

LANDINGLIGHT

ESN-12, MS24524-23G12132-3-073274

TAXILIGHT

PITOTHEAT

MASTERCUTOFF

CRANKENGINE

G12132-15-073274-P122 C


GA107 1

RBH 10/10/07

RBH 10/10/07

GA 10/10/07

CLB 10/10/07CHANGED ESN-7 SWITCH TYPE,SET OP-3 LABEL FOR DUAL HYD

A 03/23/09 RBHCHANGED ESN-11 SWITCH TYPE,B 04/12/17 GA


ADDED ACCU TST NOTEC 10/20/17 GA


MS24659-23D

G12132-5-11

AN16ga

AVIONICS MASTER

G12132-5-12

G12132-5-13

G12132-16-02 AN16ga


RELAYAVIONICS

EXTERNAL TO CONSOLE

PP128 ga.50A

AVIONICSA1

UU(no connection)X1

(Airframe GND)

X2

W

V

W

V


(no connection)

8 ga.

A2

TB4

T

P2

AN16gaT

J2

G12132-5-10


ALT. ENCODER

2.5A

TRANSPONDER

2.5A

AUDIO PANEL

2.5A

G12132-16-01 AN16ga

10A

COM2

CD CHANGER

2.5A

5A

GPS

10A

COM1 STEREO ICS

2.5A



G12132-10-05

AN16ga

AN16ga

1

2

3

4

5

6

OP-1 bb


15A

J2

EFN-97

P2

FROM G12132-10-073274

AN16ga


G12132-7-04

AN16ga

AN16ga

G12132-5-13

G12132-5-12

G12132-5-10

NN

AVIONICS-2 BUS

AVIONICS-1 BUS

P2

W W

VV

J2

U

TT

U


J2

EFN-48

P2

15A

1

2

3

4

5

6

AN16ga

MS24524-23

G12132-5-11

AN16ga

FROM G12132-7-073274

AVIONICS MASTEROP-1

AN16ga

FROM G12132-5-073274

G12132-16-073274 --


RBH 10/10/07

CLB 10/10/07

GA107 1

G12132-16-04AN16ga

AN16gaG12132-16-03




45

45


45

FROM G12132-5-073274



1ME3E

ref: WDM 25.80.00

NN

From G12132-7-073274

G12132-17-01


ref: WDM 25.80.00ref: WDM 39.00.00 PP5

P2

EFN-48

J2

RELEASE

2.5A

G12132-7-04

3

2

1



J?

??

??

P?

MS24523-23

??

??


CARGO HOOK???

G12132-?-??

G12132-?-??

G12132-17-073274 --


RBH 10/10/07

CLB 10/10/07

GA107 1


46

There is no standard switch assigned to the CARGO HOOK function in the -073274 version of the console. If a CARGO HOOK circuit is required, implement it using an available optional switch, or using a switch mounted in an installer-defined location outside the console, assigning unique wire numbers as appropriate.

46


G12132-18-02


From G12132-7-073274

J?

??

P?

??

???

HOIST

G12132-?-??

?bus

SAMPLE OPTIONAL CIRCUITSMore samples on G12132-16-073274

ref: WDM 25.63.00ref: WDM 39.00.00

N

J2P2

N

EFN-48

2.5A

G12132-7-04

RELEASE PP5

G12132-5-20

G12132-5-06

G12132-5-05

From G12132-5-073274

HOIST ARMEDwarning light.Installer shall provide suitable light and install in clear view of pilot, with appropriate label.


1ME36E

CC

BB

FF

BB

CC

FF


G12132-5-19


G12132-18-01 EE

P1 J1

EE

1

2

3

4

5

6

MS24524-23

HOISTOP-3

G12132-18-073274 --


RBH 10/10/07

CLB 10/10/07

GA107 1


RATINGCAPACITY

300lb450lb

247.5A2.5A

24

2323 There is no breaker assigned to the HOIST function in the AS350B3 definitions of the console. If a HOIST circuit is required, implement it using a standard breaker that is available for reassignment, or an additional breaker installed in one of the OPTIONAL rails or in an installer-defined location outside the console

www.genevaaviation.com G12132-2-073368 A


RBH 04/06/10

CLB 04/06/10

GA107 1


P1J1

TT

WW

SS

RR

YY

XX

zz

MASTER CUTOFF

1

2

3

4

5

6

MS24659-23D

ESN-6

MS24523-23

DIRECT BATTERY

3

2

1

OP-2

EMER BUS BAR, Top Right AftG12135-2

G12132-2-10 AN16ga

BAT-EXT PWR

MS24659-23D

1

2

3

4

5

6

ESN-1

D5:AD5:C

G12132-2-18D6:C D6:A


ref: WDM 77.00.10ref: WDM 24.30.00


(+28V VOYANT)DIRECT BATTERY

3PW52E


The toggle on this switch must be marked with the color RED

G12132-2-09

G12132-2-04

G12132-2-02

G12132-2-03

G12132-2-06

G12132-2-05

G12132-2-20

G12132-2-19

G12132-2-01

G12132-2-07


3PE28E

1PG2NE

1PG3NE

1PG1NE

1PG6NE


3EU18E

ffG12132-2-11 3EU88E (post-mod 350A07-3476 only)

ADDED 3EU88E CONNECTIONS 05/12/10 RBHA



ref: AEC DWG 350A67-4154-00

1EW93NE

1EW37E

1EW38E

1EW39E

n

m

n

m

j

k

P1j

k

J1

ref: WDM 62.30.00

1

2

3

4

5

6

G12132-3-16

G12132-3-15

G12132-3-14

MS24524-23

WARNING HORN

G12132-3-17

ESN-12



G12132-3-02

G12132-3-06

G12132-3-07

G12132-3-081KK2E P P

1PA1E

1PA2E

N

M

N

M

1KK1E

1PA4E

J1P1

U

V

U

V

ref: WDM 80.00.00ref: WDM 24.30.00

G12132-3-01


3 6

3

2

1

MS24523-26

G12132-3-05

ESN-5CRANK

PP6


G12132-3-03ESN-3

1

2

4

5


G12132-3-073368 --


RBH 04/06/10

CLB 04/06/10

GA107 1


G12132-3-11

G12132-3-10

G12132-3-12

G12132-3-13


G12132-3-093

2

1

CRANK

2.5A

EFN-631DH5E

1DH112E (if installed) and 1DH1E S S

1DH6NE

J2

R

P2

R

MS24658-23D

J1

F

P1

F

ESN-11HYD TEST

D1:A

HYDRAULICS

EFN-36

D1:C

7.5A

PP5



ref: WDM 24.30.00ref: WDM 26.10.00

G12132-3-21

G12132-3-20

J1P1

1WW83E

1WW2NE

e

bb

e

D4:A

D2:A

D4:C

G12132-3-22

D2:C

ESN-7WARN / FIRE TEST

MS27407-3

1

2

3

4

5

6

G12132-3-04

G12132-23-09

GND for OVERLAYS1WG4E d G12132-3-18d

G12132-3-23

1WG18NE or 1PE4NE or GND c G12132-3-19c

(3-position)




ref: AEC DWG 350A62-4100-02



ref: AEC DWG 350A64-7307-01

ref: AEC DWG 350A64-7316-00

ref: WDM 33.10.00

ref: WDM 33.43.00

ref: WDM 33.10.00

G12132-4-03

G12132-4-023

2

1

MS24523-23

LANDING LIGHTESN-18

q q LM5NE

P1J1

p p

G12132-4-073368 --


RBH 04/06/10

CLB 04/06/10

GA107 1


ref: AEC DWG 350A64-7312-01TAXI LIGHT

1

2

3

4

5

6

MS24524-23



G

J2

G

P2

ref: WDM 33.43.00

TAXI LIGHT

EFN-79G12132-4-16

G12132-4-15

ESN-17

7.5A

PP6




1

2

3

4

5

67.5A

G12132-4-123LK675E

1LK671E

D D

C C

G12132-23-02G12132-4-07

1

2

3

4

5

6

MS24524-23

MS24524-23INSTRUMENT LIGHTS 2

ESN-15PP15PP15

EFN-75

INST. LTS-2INST. LTS-2

EFN-75

7.5A

EFN-43

P2 J2


PP5

G12132-23-01

INST. LTS-1

ref: AEC DWG 350A64-7308-00

MS24524-21


1LJ5E or STR6A20 or Installer Defined

1LX10E or 1LX31E H

P2

L


STROBE LIGHT

7.5A G12132-4-19

EFN-45 G12132-4-20

PP5

G12132-4-18H

L

J2

ref: WDM 33.42.00

ANTI-COL LT

EFN-83

G12132-4-17

7.5A

1

2

3

4

5

6

(Center OFF)

G12132-4-21ALL / TAIL

ESN-9PP6

ref: AEC DWG 350A64-7309-00

1

2

3

4

5

6

MS24524-23

POSITION LIGHTS

1LJ1E

ref: WDM 33.41.00

POSITION LTS

EFN-87

PP6

G12132-4-13

G12132-4-14

B

J2

B

P2

7.5A

ESN-10

G12132-4-08

G12132-4-11

EFN-95

LANDING LIGHT

20A

118L

1LM7E

LM1E

AN16ga.LM6E

LM6E-1 ZY

P2G12132-4-01

G12132-4-04AN16ga.

ZY

J2PP9

1LM2003E1LM2004NE




The original LANDING LIGHT circuit MUST be rewired to match this diagram. The diode is optional. Another switch and location, such as the Pilot Colletive Grip, may be substituted for the switch and location specified, with appropriate labeling. If an alternate location is used for the LANDING LIGHT switch, then the switch and position specified here may be used for another circuit, with appropriate labeling. If the switch specified here is used, wires LM1E and LM5NE may be 16 ga. and need to have strands trimmed off in order to fit into the connector.


1LM2E and1LM2008E

(Double pole switches used for current rating.)

EFN-91


ref: AEC DWG 350A67-6089-00


ref: WDM 30.42.00


ref: WDM 30.30.00

If the OP-x switches and wiring are installed, they must be labeled to show their function.

ref: AEC DWG 350A67-6091-00

Installer Defined

Installer Defined

Installer Defined

Installer Defined

UUG12132-5-12 AN16ga.

G12132-5-13 AN16ga.W

V

W

V

OP-1

MS24524-23

1

2

3

4

5

6

G12132-5-11

AVIONICS MASTER

G12132-5-10

AN16gaT

P2

T

J2

AN16ga


ref: AEC DWG 350A67-2686-00

PP5

1FN1E

G12132-5-033

2

1

J2

MS24523-23

AA

P2

G12132-5-04

PITOT HEATESN-13

ref: WDM 28.00.00

1QN11E

7.5A

EFN-39

1MK1E Blue

1MK1E Red

PITOT HEAT

1QN1E DD

P1 J1

DD

G12132-5-173

2

1

G12132-5-14

G12132-5-18

P

M

P2

P

M

J2

MS24523-23

W/S WIPERESN-24

PP9

G12132-5-02

G12132-5-01

FUEL PUMP 1

MS24523-23

3

2

1

ESN-2FUEL PUMP-1

EFN-67

PP6

7.5A

y y1KS2E G12132-5-09

G12132-5-073368 --


RBH 04/06/10

CLB 04/06/10

GA107 1

ref: WDM 71.61.10


ref: AEC DWG 350A67-2692-00


FUEL PUMP 2

MS24523-23

3

2

1

SAND FILTER

G12132-5-08

MS24524-23

1

2

3

4

5

6


Installer Defined

Installer Defined

1KS3E

7.5A

W/S WIPER

J1P1

G12132-5-21

GG

HH

G12132-5-22

x

P1

GG

HH

x

J1

1QN8E

ESN-21

P1

AA


1QN8G

ESN-8

SAND FILTER

G12132-5-07 7.5A

EFN-66

J1

AA

PP6

G12132-5-05

G12132-5-06

PP6

EFN-68

FUEL PUMP-2

7.5A

1LK639E

1FW2E


ref: G12132-16-073368



2.5A

PITOT HEAT


3EU3E

EFN-39

7.5A

PP5

A A

EFN-38

P1 J1

HYDRAULICS

WARNING PANEL-1

ROTOR TACH


ref: AEC DWG 350A62-4100-02

ref: AEC DWG 350A67-2690-01

ref: WDM 24.30.00

ref: WDM 77.00.10

1WW1E and 1WW1F G12132-6-01E E

PP5

2.5A

EFN-37

P2 J2

PP5

7.5A

EFN-36

PP5

G12132-6-073368 --


RBH 04/06/10

CLB 04/06/10

GA107 1

7.5A

EFN-43

INST. LTS-1

1A

EFN-42


3EU72E v

P1

EMERGENCY-ROTOR TACH INVERTER


v

PP5

G12132-6-05J1

EMER BUS

EFN-41

2.5A

EFN-40

EMERGENCY-ROTOR TACH

1A

P1


1EW103E D

P1

3EU3F

VHIU-1

t


J1

G12132-6-04D

J1

G12132-6-06

PP5

t

EMER BUS

7.5A


G12132-6-02

D3:C

D3:A

G12132-6-07



RELEASEFor optional uses, this breaker may be up to 15 amps.

ref: G12132-17-073368

ATTITUDE

(1FF219E)

Installer Defined

Wire directly to the Attitude gyro, or through an On/Off switch and/or the Avionics Master Relay; or, this function may be moved to a breaker that is supplied from a switched bus.

ref: WDM 34.25.27

G12132-7-05u u

G12132-7-04 AN16ga.

PP5

2.5A

EFN-49

P1 J1

P2 J2

N N

EFN-48

2.5A

STROBE LIGHT

1EW30E

ref: AEC DWG 350A67-4166-01

ref: AEC DWG 350A63-6159-00


ref: WDM 25.00.00

ref: WDM 31.60.00

G12132-7-03

PP5

s s

PP5

7.5A

EFN-46

P1 J1

VEMD-1

PP5

EFN-45

7.5A

For optional uses, this breaker may be up to 15 amps.HOIST

ref: G12132-18-073368

G12132-7-073368 --


RBH 04/06/10

CLB 04/06/10

GA107 1

G12132-7-09 AN16ga.

G12132-7-01ww1ME87E


EXT. LOAD

2.5A

J1P1

EFN-58

PP6

P2 J2

FF

EFN-57


G12132-7-07

G12132-7-08

ref: WDM 25.63.00


1WW31E

PP9

E

J1

E

P1

WARNING PANEL-2

2.5A

EFN-56

PP6

ref: AEC DWG 350A67-4166-01ref: WDM 31.60.00 VEMD-2

1EW35E

EFN-55

K

J1P1

K

7.5A

PP6

Installer Defined

2.5Aref: G12132-18-073368

ref: AEC DWG 350A63-5016-00

ref: WDM 34.20.00



FUEL FLOWref: WDM 28.41.10

ref: AEC DWG 350A67-6090-00

Installer Defined

WINDSHIELD WIPER 2

(1QW38E)

ref: WDM 30.42.00

May be wired directly to the Fuel Flow meter, or through an On/Off switch

G12132-8-04 16 ga.Q Q

G12132-8-03

7.5A

EFN-62

P2 J2

PP6

EFN-61

2.5A

P1

r

J1

r

ref: AEC DWG 350A67-4166-01

ref: AEC DWG 350A67-2695-00

ref: AEC DWG 350A67-2686-00

1EW105E

ref: WDM 28.00.00

G12132-8-021QW1E C

P1

PP6

C

J1

FUEL GAUGE

EFN-60

2.5A

PP6

G12132-8-01

2.5A

EFN-59

P1

B

VHIU-2

J1

B

PP6

G12132-8-073368 --


RBH 04/06/10

CLB 04/06/10

GA107 1

EFN-65

J1

EFN-66

Detailed on G12132-5-073368SAND FILTER

7.5A

Installer Defined

P1

i

2.5A


PP6

G12132-8-06i

EFN-63

EFN-64

J1


3EU71E

SPARE

L

P1

ROTOR TACH INVERTER

2.5A


2.5A

PP6

G12132-8-05L

PP6

PP6

ref: WDM 31.60.00



ref: WDM 31.31.00


1DT5E

EFN-75

PP15INST. LTS-2

7.5A

PP9

P1

H H

J1

EFN-70

HOUR METER

2.5A

G12132-9-02


ref: AEC DWG 350A67-6087-00


FUEL PUMP-2

FUEL PUMP-1

PP6

EFN-68

7.5A

PP6

EFN-67

7.5A

G12132-9-073368 --


RBH 04/06/10

CLB 04/06/10

GA107 1



POSITION LTS

7.5A

EFN-87

PP6

ANTI-COL LT

EFN-83

7.5A

PP6


G12132-9-03J1LE1E J


7.5A

EFN-79

TAXI LIGHT PP6

ref: AEC DWG 350A64-7311-00ref: AEC DWG 350A64-7265-00ref: WDM 33.10.00 CABIN LIGHTS

EFN-76

P1 J1

2.5A

PP6



ref: AEC DWG 350A67-2688-00

LANDING LIGHT



ref: WDM 80.00.00

1KK4E and 1KK4F

1MH1E

20A

05/06/08 RBH

EFN-95

G12132-10-03 AN16ga.

G12132-10-04 AN16ga.

EFN-94

PP9

P2

X

J2

X

10A

START PP9

a

P2

a

J2

ref: AEC DWG 350A62-0045-00

ref: AEC DWG 350A63-6158-00

Detailed on G12132-5-073368W/S WIPER-1

CARGO HOOK

POWER OUTLET

ref: WDM 25.80.00

ref: WDM 25.26.00

1ME1E G12132-10-02 AN16ga.J2P2

15A

EFN-93

PP9

c c

15A

EFN-92

PP9

EFN-91

7.5A

PP9


G12132-10-01

G12132-10-073368 --


RBH 04/06/10

CLB 04/06/10

GA107 1

G12132-10-08

G12132-10-09


3PW53E and 3PW55E

P1

g g

J1

ref: AEC DWG 350A62-4101-00

3PW54E and 3PW54F


ref: WDM 24.30.00

h

P1

D-BAT CONTROL

EFN-N/A-4

PP15

3A

h

J1

EFN-N/A-3

DIRECT BATTERY

a(1FF210F)

PP6

2.5A

a


G12132-10-05 AN16ga.

G12132-10-06

ref: AEC DWG 350A68-2541-01


Wire directly to the Turn & Bank Indicator, or through an On/Off switch; or, this function may be moved to a breaker that is supplied from a switched bus. GG(1FA1E)

DIR. GYRO

P1

EFN-N/A-2

2.5A

J1

PP6

TURN & BANK

P1

EFN-N/A-1

J1

PP9

2.5A


EFN-97

AC INVERTER

b

P2

1XU1E b

J2

PP9

10A

ref: WDM 34.25.27

ref: WDM 34.20.00ref: WDM 34.26.03


www.genevaaviation.com G12132-11-073368 A


RBH 04/06/10

CLB 04/06/10

GA107 1







BUS BAR, Top Left



1PP9E

3PP23E

TB6

TB5 AN8ga G12132-11-14

AN8ga G12132-11-04


ref: WDM 77.00.10ref: WDM 24.30.00

1PP6E

1PP5E

TB3

TB2

TB1 AN8ga G12132-11-01

AN8ga G12132-11-02

AN8ga G12132-11-03



G12135-10

G12135-12

G12135-9

G12135-10

G12135-10

G12135-9

ref: G12132-16-073368

EMER BUS BAR, Top Right Aft

ESN-6

MS24659-23D

1

2

3

4

5

6

MASTER CUTOFF

ref: G12132-2-073368

G12135-2

J1P1

f f(Post-Mod 350A07-3476 only) 3EU88EG12132-2-11

AN16ga G12132-2-10

ADDED 3EU88E CONNECTIONS 05/12/10 RBHA


AIR

CR

AFT

FW

D






The PP15 bus normally powers minimal avionics functions, not shown here. At the installer's discretion, the PP15 bus may be moved to an installer-defined location outside the console, so that the left middle breaker rail may be used for additional installer-defined avionics circuits. In that case, the Instrument Lights 2 circuit will need to be modified. See the sample modified Instrument Lights 2 circuit on G12132-34.

LEFT MIDDLE BUS BAR


VOID LTB-BUS

2.5A

LTB-1

G12132-12-19

G12132-12-20

LTB-4

LTB-BUS

LTB-BUS

VOID

LTB-2

2.5A

LTB-3

2.5A

VOID

G12132-12-18

G12132-12-17

LTB-BUS

LTB-BUSLTB-5

2.5A

VOID

LTB-6

5A

VOID

G12132-12-16

G12132-12-15

G12132-12-14

Installer Defined

Installer DefinedVU

VU

Installer Defined

Installer DefinedT T

S S

Installer Defined

Installer Defined

Installer DefinedR R

Q

P

Q

P

LTB-BUSVOID

G12132-12-09

LTB-BUS

LTB-BUS

5A

5A

LTB-7VOID

LTB-8

5A

VOID

G12132-12-12

G12132-12-13

G12132-12-10

G12132-12-11

LTB-BUS

LTB-BUS

7.5A

LTB-9VOID

7.5A

LTB-10VOID

G12132-12-07

G12132-12-08

G12132-12-05

G12132-12-06

LTB-BUS

LTB-BUS

10A

LTB-11

VOID

10A

LTB-12

VOID

G12132-12-04

G12132-12-03

G12132-12-01

G12132-12-02


Installer Defined

Installer Defined

Installer Defined

Installer Defined

Installer Defined

L L

N

M

N

M

KJ

KJ

Installer Defined

Installer Defined

Installer Defined

Installer DefinedHG

HG

FE

FE


Installer Defined

Installer Defined

Installer Defined

Installer Defined

CD

CD

AB

J3

AB

P3LEFT TOP BUS BAR

G12132-12-073368 --


RBH 04/06/10

CLB 04/06/10

GA107 1

Installer DefinedG12132-12-30

G12132-12-31if installed.

Installer defined


g

f

Installer Definedg

f

G12132-12-29

G12132-12-28

G12132-12-27

G12132-12-26

2.5A

LMB-2

2.5A

LMB-3VOID PP15

LMB-5

LMB-4

VOID

VOID

VOID

PP15

PP15

5A

PP15

5A

e

d

Installer Definede

Installer Definedd

c

b

Installer Definedc

Installer Definedb


Installer DefinedG12132-12-21

G12132-12-25

G12132-12-24

G12132-12-23

G12132-12-22

LMB-8

LMB-7

LMB-6

7.5A

VOID

VOID

PP15

5A

PP15

if installed.Installer defined

LMB-9

7.5A

7.5A

VOID

VOID

PP15

PP15

Y Y

a

Z

Installer Defineda

Installer DefinedZ

X

W

Installer DefinedX

Installer Defined

W

(p/n: G12135-12)

(p/n: G12135-10)

G12132-11-13LTB-BUS

J3

PP15 BUS

P3

G12132-11-14AN8ga.

AN8ga.Installer defined power sourceTB4

3PP23ETB5

ref: WDM 24.30.00

G12132-7-073368, 24.30.00

G12132-5-073368, 28.00.00

G12132-6-073368, 77.00.10

G12132-13-073368 --


GA107 1

RBH 04/06/10

RBH 04/06/10

RBH 04/06/10

CLB 04/06/10

2.5A, PP5, EFN-38

WAR

N PN

L-2

7.5A, PP6, EFN-68

FUEL PU

MP-2

RO

TOR

TACH

MS24524-23

INST. LTS-1

G12132-4-073368, ESN

-14

FWD


G12132-7-073368, 25.80.00

VHIU

-22.5A, PP6, EFN

-59

2.5A, PP6, EFN-58

EXT. LOAD

G12132-10-073368, 34.20.00


G12132-8-073368, 28.41.10

G12132-4-073368, 33.42.00

W/S W

IPER-2

7.5A, PP6, EFN-62

7.5A, PP6, EFN-83

ANTI-C

OL LT

DIR

. GYR

OG

12132-4-073368, 33.41.00

2.5A, PP6, EFN-N

/A-2

7.5A, PP6, EFN-87

POSITIO

N LT

G12132-3-073368, 80.00.00

2.5A, PP6, EFN-64

INV N

RG

12132-8-073368, 77.00.10

G12132-8-073368

2.5A, PP6, EFN-65

SPARE

G12132-8-073368, 30.42.00

CR

ANK

2.5A, PP6, EFN-63

2.5A, PP6, EFN-76

CABIN

LTS

G12132-4-073368, 33.43.00

G12132-9-073368, 33.10.00

7.5A, PP6, EFN-79

TAXI LIGH

T

G12132-10-073368, 24.30.00

G12132-5-073368, 28.00.00

DIR

ECT BATT

2.5A, PP6, EFN-N

/A-3

G12132-8-073368, 31.60.00

2.5A, PP6, EFN-60

FUEL G

AUG

E

G12132-8-073368, 28.00.00

FUEL FLO

W2.5A, PP6, EFN

-61

G12132-7-073368, 25.00.00

2.5A, PP5, EFN-49

RELEASE

TAXI LIGH

T

G12132-4-073368, ESN

-17

G12132-7-073368, 34.20.00

ATTITUD

E

G12132-4-073368, ESN

-18

LAND

ING

LIGH

TM

S24523-23

MS24524-23

ANTI-C

OL LT

G12132-4-073368, ESN

-9

POSITIO

N LTS

G12132-4-073368, ESN

-10

INST. LTS-2

G12132-4-073368, ESN

-15

MS24524-21

G12132-6-073368, 77.00.10

EMER

-INV

G12132-4-073368, 33.41.00

STRO

BE LT

G12132-7-073368, 31.60.00

2.5A, PP5, EFN-48

7.5A, PP5, EFN-46

VEMD

-1

G12132-4-073368, 33.10.00

7.5A, PP5, EFN-45

INST. LTS-1

G12132-5-073368, 30.30.00

G12132-6-073368, 31.60.00

G12132-6-073368, 77.00.10

1A, EMER

, EFN-40

7.5A, PP5, EFN-39

PITOT H

EAT

VHIU

-12.5A, PP5, EFN

-41

1A, EMER

, EFN-42

EMER

-NR

MS24524-23

MS24524-23

G12132-7-073368, 31.60.00

7.5A, PP6, EFN-55

VEMD

-2

2.5A, PP6, EFN-56

G12132-5-073368, 71.61.10

7.5A, PP6, EFN-66

7.5A, PP6, EFN-67

FUEL PU

MP-1

SAND

FILTER

G12132-3-073368, 29.00.00

G12132-6-073368, 24.30.00

HYD

RAU

LICS

WAR

N PN

L-1

7.5A, PP5, EFN-36

2.5A, PP5, EFN-37

MS24524-23

WAR

NIN

G H

OR

N

G12132-3-073368, ESN

-12

7.5A, PP5, EFN-43


34.20.00

33.41.00

7.5A, PP6, EFN-87

POSITION LTSG12132-4-073368

G12132-10-073368DIR. GYRO2.5A, PP6, EFN-N/A-2

G12132-8-073368

2.5A, PP6, EFN-63

INV NR2.5A, PP6, EFN-64

G12132-3-073368

G12132-8-073368

CRANK

SPARE2.5A, PP6, EFN-65

77.00.10

80.00.00

G12132-9-073368

33.42.00

33.43.00

33.10.00


G12132-4-073368

G12132-4-073368ANTI-COL LT7.5A, PP6, EFN-83

24.30.00

28.00.00

FUEL PUMP-27.5A, PP6, EFN-68

G12132-5-073368

G12132-10-073368DIR BATT2.5A, PP6, EFN-N/A-3

2.5A, PP6, EFN-76

CABIN LTSG12132-8-073368

FUEL FLOW2.5A, PP6, EFN-61

G12132-8-073368

G12132-8-073368W/S WIPER-27.5A, PP6, EFN-62

30.42.00

28.41.10

28.00.00

EXT. LOAD2.5A, PP6, EFN-58

G12132-7-073368

2.5A, PP6, EFN-60

G12132-8-073368VHIU-22.5A, PP6, EFN-59

FUEL GAUGE

31.60.00

25.80.00

28.00.00

71.61.10

SAND FILTERG12132-5-073368

7.5A, PP6, EFN-66

FUEL PUMP-1G12132-5-073368

7.5A, PP6, EFN-67 2.5A, PP6, EFN-56

G12132-7-073368VEMD-27.5A, PP6, EFN-55

G12132-7-073368WARN PNL-2

24.30.00

31.60.00

FWD

G12132-7-073368

RELEASE2.5A, PP5, EFN-48

2.5A, PP5, EFN-49

34.20.00

ATTITUDEG12132-7-073368

31.60.00

25.00.00G12132-7-073368

INST. LTS-1

STROBE LT

7.5A, PP5, EFN-46

33.41.00G12132-4-073368

VEMD-1

33.10.00

7.5A, PP5, EFN-45

G12132-4-073368

G12132-6-073368

2.5A, PP5, EFN-41

1A, EMER, EFN-42

EMER-INVG12132-6-073368

31.60.00

77.00.10

G12132-6-073368VHIU-1

ROTOR TACH2.5A, PP5, EFN-38

7.5A, PP5, EFN-39

1A, EMER, EFN-40

EMER-NR

PITOT HEAT30.30.00G12132-5-073368

77.00.10G12132-6-073368

7.5A, PP5, EFN-36

2.5A, PP5, EFN-37

WARN PNL-1

HYDRAULICS

24.30.00G12132-6-073368

29.00.00G12132-3-073368


G12132-13-073368-P122 --


GA107 1

RBH 04/06/10

RBH 04/06/10

RBH 04/06/10

CLB 04/06/10

7.5A, PP5, EFN-437.5A, PP5, EFN-43

77.00.10

?A, ?

bus,

LTB

-6O

ptio

nal

G12

132-

12-0

7336

8

Opt

iona

lM

S245

23-2

3W

/S W

IPER

G12

132-

5-07

3368

, ESN

-24



Opt

iona

l

?A, P

P15,

LM

B-7

G12

132-

12-0

7336

8

Opt

iona

l

?A, P

P15,

LM

B-8

G12

132-

12-0

7336

8

Opt

iona

l

?A, P

P15,

LM

B-9

G12

132-

4-07

3368

, 33.

10.0

0

INST

.LTS

-2

7.5A

, PP1

5, E

FN-7

5

FWD

G12

132-

10-0

7336

8, 2

5.26

.00

7.5A

, PP9

, EFN

-91

CAR

GO

HO

OK

G12

132-

5-07

3368

, 30.

42.0

0

W/S

WIP

ER15

A, P

P9, E

FN-9

2G

1213

2-10

-073

368,

25.

80.0

0PW

R O

UTL

ET

15A,

PP9

, EFN

-93

G12

132-

4-07

3368

, 33.

43.0

0

LAN

DIN

G L

T

20A,

PP9

, EFN

-95

G12

132-

10-0

7336

8, 8

0.00

.00

G12

132-

10-0

7336

8, 2

4.22

.00

10A,

PP9

, EFN

-97

AC IN

VER

TER

Opt

iona

l

?A, P

P15,

LM

B-6

G12

132-

12-0

7336

8

?A, P

P15,

LM

B-5

G12

132-

12-0

7336

8

?A, ?

bus,

LTB

-12

BAT-

EXT

PWR

G12

132-

5-07

3368

, ESN

-8

?A, ?

bus,

LTB

-9O

ptio

nal

G12

132-

12-0

7336

8?A

, ?bu

s, L

TB-1

0O

ptio

nal

G12

132-

12-0

7336

8

Opt

iona

l

Opt

iona

lG

1213

2-12

-073

368

?A, ?

bus,

LTB

-11

G12

132-

12-0

7336

8?A

, ?bu

s, L

TB-8

Opt

iona

lG

1213

2-12

-073

368

?A, ?

bus,

LTB

-7O

ptio

nal

G12

132-

12-0

7336

8

MS2

4659

-23D

G12

132-

2-07

3368

, ESN

-1

MS2

4523

-23

FUEL

PU

MP

1G

1213

2-5-

0733

68, E

SN-2

FUEL

PU

MP

2

MS2

4523

-23

G12132-14-073368 --


GA107 1

RBH 04/06/10

RBH 04/06/10

RBH 04/06/10

CLB 04/06/10

TUR

N &

BAN

K

HO

UR

MET

ER

D-B

AT C

TRL

3A, P

P15,

EFN

-N/A

-4

G12

132-

12-0

7336

8

2.5A

, PP9

, EFN

-N/A

-1

G12

132-

9-07

3368

, 31.

31.0

0

G12

132-

7-07

3368

, 25.

63.0

02.

5A, P

P9, E

FN-7

0

G12

132-

10-0

7336

8

Opt

iona

l

?A, P

P15,

LM

B-3

G12

132-

12-0

7336

8

Opt

iona

l

?A, P

P15,

LM

B-4

Opt

iona

l

?A, P

P15,

LM

B-2

G12

132-

12-0

7336

8

G12

132-

10-0

7336

8, 2

4.30

.00

G12

132-

5-07

3368

, OP-

1

MS2

4524

-23

SAN

D F

ILTE

RG

1213

2-5-

0733

68, E

SN-2

1

Opt

iona

lG

1213

2-12

-073

368

G12

132-

12-0

7336

8?A

, ?bu

s, L

TB-4

?A, ?

bus,

LTB

-5O

ptio

nal

G12

132-

12-0

7336

8

Opt

iona

lG

1213

2-12

-073

368

?A, ?

bus,

LTB

-3

?A, ?

bus,

LTB

-1O

ptio

nal

?A, ?

bus,

LTB

-2O

ptio

nal

G12

132-

12-0

7336

8

G12

132-

12-0

7336

8

DIR

ECT

BATT

G12

132-

2-07

3368

, OP-

2

MS2

4523

-23

AVIO

NIC

S

MS2

4524

-23

10A,

PP9

, EFN

-94

STAR

T

HO

IST

2.5A

, PP9

EFN

-57


30.42.00

25.80.00

25.26.00

33.43.00

24.22.00

25.63.00


G12132-10-073368

CARGO HOOK

PWR OUTLET

15A, PP9, EFN-92

G12132-10-073368

15A, PP9, EFN-93

G12132-5-073368W/S WIPER-1

7.5A, PP9, EFN-91

START

G12132-10-073368AC INVERTER

20A, PP9, EFN-95

G12132-4-073368LANDING LT

10A, PP9, EFN-97

HOIST

G12132-10-073368

2.5A, PP9, EFN-57

G12132-7-073368

HOUR METER

TURN & BANK

G12132-12-073368

G12132-12-073368

G12132-12-073368

G12132-12-073368

G12132-12-073368

FWD Effectivity: AS350B2 EmbodyingMod 350A07-3368

24.30.00

G12132-12-073368

G12132-12-073368

G12132-10-073368

Optional

Optional

Optional

Optional

Optional

Optional

Optional2.5A, PP9, EFN-70

G12132-9-07336831.31.00

G12132-12-073368

G12132-12-073368

G12132-12-073368

G12132-12-073368

G12132-12-073368

G12132-12-073368

G12132-12-073368

G12132-12-073368

G12132-12-073368

G12132-12-073368

G12132-12-073368

G12132-12-073368Optional

Optional

Optional

Optional

Optional

Optional

Optional

Optional

Optional

Optional

10A, PP9, EFN-94

G12132-10-07336880.00.00

33.10.00

G12132-12-073368

G12132-4-073368

OptionalOptional

Optional

G12132-14-073368-P122 --


GA107 1

RBH 04/06/10

RBH 04/06/10

RBH 04/06/10

CLB 04/06/10

D-BAT CTRL

INST LTS 2

?A, ?bus, LTB-1

?A, ?bus, LTB-2

?A, ?bus, LTB-3

?A, ?bus, LTB-4

?A, ?bus, LTB-5

?A, ?bus, LTB-6

3A, PP15, EFN-N/A-4

?A, PP15, LMB-2

?A, PP15, LMB-4

?A, PP15, LMB-3

?A, ?bus, LTB-9

?A, ?bus, LTB-7

?A, ?bus, LTB-8

?A, ?bus, LTB-10

?A, ?bus, LTB-11

?A, ?bus, LTB-12

?A, PP15, LMB-7

?A, PP15, LMB-5

?A, PP15, LMB-6

?A, PP15, LMB-8

?A, PP15, LMB-9

7.5A, PP15, EFN-75


CRANKENGINE

CR

AN

K E

NG

INE


WIPER

FILTER

DIRECTBATTERY

AVIONICSMASTER

AVIONICS

MS24523-23

MS24524-23

G12132-5-073368, OP-1

G12132-2-073368, OP-2DIRECT BATT

W/S WIPERMS24523-23

MS24524-23

SAND FILTERG12132-5-073368, ESN-21

G12132-5-073368, ESN-24

SAND

FUEL

BAT-EXTPOWER

WINDSHIELD

BAT-EXT PWR

FUEL PUMP 1

MS24523-23

FUEL PUMP 2G12132-5-073368, ESN-8

G12132-5-073368, ESN-2

MS24523-23

MS24659-23D

G12132-2-073368, ESN-1

HY

D T

EST

GE

NE

RA

TOR

ON

MS

2452

4-31

MS

2465

8-23

D

WA

RN

/ FI

RE

TE

ST

MS

2452

3-26

G12

132-

3-07

3368

, ES

N-3

G12

132-

3-07

3368

, ES

N-1

1

G12

132-

3-07

3368

, ES

N-7

GENERATORON / RESET

PUMP 2

FUELPUMP 1

WARN/FIREHYDTEST TEST

LIGHTS

G12132-15-073368 --


GA107 1

RBH 04/06/10

RBH 04/06/10

RBH 04/06/10

CLB 04/06/10

MS24524-23

MS24524-21

MS24524-23

MS24523-23

LANDING LT

TAXI LIGHT

ANTI-COL LT

POSITION LTS

G12132-4-073368, ESN-18

G12132-4-073368, ESN-17

G12132-4-073368, ESN-9

G12132-4-073368, ESN-10

LIGHTTAXI

LIGHTLANDING

ALL / TAILANTI-COL

MS24524-23

MS24524-23

MS24524-23

WARNING HORN

INST. LTS-1

INST. LTS-2

G12132-3-073368, ESN-12

G12132-4-073368, ESN-14

G12132-4-073368, ESN-15M

AS

TER

CU

TOFF

MS

2452

3-23

MS

2465

9-23

D

PITO

T H

EAT

G12

132-

3-07

3368

, ES

N-5

G12

132-

2-07

3368

, ES

N-6

G12

132-

5-07

3368

, ES

N-1

3

MASTERCUTOFF HEAT

PITOT

POSITION

INSTRUMENTLIGHTS 2

HORNWARNING

INSTRUMENTLIGHTS 1

MS

2740

7-3


G12132-3-073368ESN-5, MS24523-26

P122 CONSOLE LAYOUT

G12132-5-073368

G12132-4-073368ESN-17, MS24524-23

ESN-13, MS24523-23

ESN-15, MS24524-23G12132-4-073368

G12132-23-073368OP-1, MS24524-23

G12132-4-073368

AVIONICSMASTER

ESN-14, MS24524-23


ESN-10, MS24524-23G12132-4-073368 G12132-4-073368

ESN-9, MS24524-21

PANELDIMMER

FUELPUMP 2

GENERATORON / RESET

G12132-3-073368ESN-3, MS24524-31

INSTRUMENTLIGHTS 2

G12132-5-073368ESN-8, MS24523-23

G12132-5-073368

INSTRUMENTLIGHTS 1

ESN-2, MS24523-23

FUELPUMP 1

ESN-1, MS24659-23DG12132-2-073368

BAT-EXTPOWER

G12132-3-073368ESN-11, MS24658-23D

ESN-21, MS24524-23G12132-5-073368

POSITIONLIGHTS

SANDFILTER

ANTI-COLALL / TAIL

ESN-24, MS24523-23G12132-5-073368

WINDSHIELDWIPER

G12132-3-073368ESN-7, MS27407-3

HYDRAULICTEST

WARN / FIRETEST

DIRECTBATTERY

ESN-18, MS24523-23G12132-4-073368

OP-2, MS24523-23G12132-2-073368

WARNINGHORN

G12132-2-073368ESN-6, MS24659-23D

LANDINGLIGHT

ESN-12, MS24524-23G12132-3-073368

TAXILIGHT

PITOTHEAT

MASTERCUTOFF

CRANKENGINE

G12132-15-073368-P122 --


GA107 1

RBH 04/06/10

RBH 04/06/10

RBH 04/06/10

CLB 04/06/10

G12132-5-073368

AVIONICS-1 BUS

AVIONICS-2 BUS

G12132-5-10


G12132-5-13

G12132-5-12

AN16ga


EXTERNAL TO CONSOLE

AVIONICSRELAY

PP128 ga.

AVIONICS

50AA1

(Airframe GND)

X2

W

V

W

V

(no connection)


(no connection)

8 ga.

A2

X1

TB4

T

U

P2

T

U

J2

AN16ga

2.5A

ALT. ENCODER

2.5A

2.5A

TRANSPONDER

AUDIO PANEL

COM2

10A

GPS

5A

CD CHANGER

2.5A

COM1

10A

STEREO ICS

2.5A

EFN-97


G12132-10-05

AN16ga

AN16ga

AVIONICS MASTER

1

2

3

4

5

6

G12132-5-11

MS24659-23D

OP-1 b b


15A

P2 J2



AN16ga

PP9

EFN-48

G12132-5-10

G12132-5-12

G12132-5-13

AN16ga

AN16ga

G12132-16-01 AN16ga

G12132-16-02 AN16ga

W

V

W

V

T

U

P2

T

U

J2


G12132-16-03P2 J2

15A

1

2

3

4

5

6

G12132-5-11

MS24524-23

AN16ga

AN16ga

OP-1AVIONICS MASTER

AN16ga

AN16ga

FROM G12132-5-073368



FROM G12132-5-073368


G12132-16-04

42

AN16ga

42

FROM G12132-10-073368

G12132-8-04Q Q

42


FROM G12132-8-073368


PP6

G12132-16-073368 --


RBH 04/06/10

CLB 04/06/10

GA107 1

ref: WDM 25.80.00


1ME3E



N N

From G12132-7-073368

G12132-17-01


ref: WDM 25.80.00

J2P2

EFN-48

RELEASE

2.5A

G12132-7-04

PP5

3

2

1

G12132-17-073368 --


RBH 04/06/10

CLB 04/06/10

GA107 1


**

P*

MS24523-23

**

J*



(Installer Defined)CARGO HOOK47

G12132-17-03

G12132-17-02


28

A connector is not required in this position. The airframe wires may be connected directly to the switch. If a connector is used for this circuit, the installer shall record the connector's identification number and the contact positions used.

28

There is no standard switch assigned to the CARGO HOOK function in the -073368 version of the console. If a CARGO HOOK circuit is required, implement it using an available optional switch, or using a switch mounted in an installer-defined location outside the console. The wire numbers shown are only an example. If an internal switch is used, the wire numbers should be updated to match the internal console wiring for that switch. if an external switch is used, the installer may use these numbers, or assign unique wire numbers as appropriate.

47


G12132-18-02



29

From G12132-7-073368

2.5A300lb

CAPACITY

ref: WDM 25.63.00

450lb 7.5ARATING29 J2

F

P2

F

EFN-57

HOIST

G12132-7-09

PP9

RELEASE


ref: WDM 25.63.00

N

J2P2

N

EFN-48

2.5A

G12132-7-04

PP5

G12132-18-06

G12132-18-073368 --


RBH 04/06/10

CLB 04/06/10

GA107 1

G12132-18-04

G12132-18-03



1ME36E

**

***

*


G12132-18-05


G12132-18-01P*

*

J*

*

1

2

3

4

5

6

MS24524-23

HOIST(Installer Defined)

48ref: WDM 25.00.00ref: WDM 25.63.00ref: AEC DWG 350A63-5017ref: AEC DWG 350A63-5016ref: AEC DWG 350A63-6159

30


30

There is no standard switch assigned to the HOIST function in the -073368 version of the console. If a HOIST circuit is required, implement it using an available optional switch, or using a switch mounted in an installer-defined location outside the console. The wire numbers shown are only an example. If an internal switch is used, the wire numbers should be updated to match the internal console wiring for that switch. if an external switch is used, the installer may use these numbers, or assign unique wire numbers as appropriate.

48

Effectivity: AS350B3 embodying Mod 350A07-3476 (B3e)

G12132-2-19

DIRECT BATTERY

EMER BUS BAR, Middle Right AftG12135-2


EMERGENCY-IDL / FLT SEL

IDL / FLT SEL

1A

EFN-71E D5:A

G12132-2-08

D5:C

1A

PP9

EMER BUS BAR

2.5A

EFN-57

EFN-72K

EMER BUS BAR

G12132-2-10 AN16ga

G12132-2-14

D4:A

D2:A

G12132-2-12

D2:C

D4:C

1

2

3

4

5

6

MS24659-23D

MASTER CUTOFF


ref: WDM 24-30-00

P1 J1

G12132-2-07

ESN-6

G12132-2-18

D7:C

D6:C

3PE28E


1PG6NE

1PG1NE

1PG3NE

1PG2NE

zz

X

Y Y

X

W

S

R R

S

W

D7:A

D6:A

G12132-2-20

G12132-2-06

G12132-2-05

G12132-2-04

G12132-2-02

G12132-2-03

1

2

3

4

5

6

MS24659-23D

BAT-EXT PWR

G12132-2-01

ESN-1

MS24523-23

G12132-2-073476 --


GA 02/05/13

CLB 02/05/13

GA107 1

P2J2G12132-2-15

F F 3EU3F

3EU18E

G12132-2-13

G12132-2-17

Z Z

G12132-2-09 T T

J1 P1

1KK115E



3PW52E



3

2

1

OP-2


ref: WDM 63-41-00ref: WDM 77-00-04ref: WDM 80-11-04

ref: WDM 24-60-02

3EU88EG12132-2-11 f f


ref: WDM 63-41-00

1EW93NE

1EW37E

1EW38E

1EW39E

n

m m

n

k

jP1

k

jJ1

1

2

3

4

5

6

G12132-3-15

G12132-3-14

MS24524-23

WARNING HORNESN-12

G12132-3-08

G12132-3-07

G12132-3-06

G12132-3-02


PP1KK53E

1PA1E

1PA2E

N

M

N

M

1KK55E

1PA4E

P1 J1

U

V

U

V

ref: WDM 80-11-04ref: WDM 24-30-00

G12132-3-01


3 6

3

2

1

MS24523-26

G12132-3-05

ESN-5CRANK

PP6

GENERATOR ON / RESETESN-3

1

2

4

5


G12132-3-073476 --


GA 02/05/13

CLB 02/05/13

GA107 1


CRANK

2.5A

EFN-63


ref: WDM 24-30-00

1DH6E

G12132-3-22

d d

1WW1E E

P2

E

J2

b

c

P1

ee

1

2

3

4

5

6

G12132-3-18

G12132-3-19

G12132-3-20b

c


WARN / FIRE TEST

G12132-3-21

G12132-3-04

J1

ee

ESN-7

WARN PANEL 1

GND for OVERLAYS

2.5A

EFN-37

PP5

G12132-23-09

1PE4NE or GND

1WW38E

1WW2NE

1WW82E



This 3-position switch performs the FIRE TEST function in the aft positionref: WDM 31-61-00

ref: WDM 26-11-00


ref: WDM 29-11-00

MS24658-23D

ESN-11HYD TEST

HYDRAULICSPP5

7.5A

EFN-36

P1 J1G12132-3-101DH1E

and 1DH112E

G12132-3-09

u

ref: WDM 29-11-00

The toggle of this switch must be marked with the color YELLOW.

u

G12132-3-16

G12132-3-17

G12132-3-033

2

1


ref: WDM 63-41-00

1EW93NE

1EW37E

1EW38E

1EW39E

n

m m

n

k

jP1

k

jJ1

1

2

3

4

5

6

G12132-3-15

G12132-3-14

MS24524-23

WARNING HORNESN-12

G12132-3-08

G12132-3-07

G12132-3-06

G12132-3-02


PP1KK53E

1PA1E

1PA2E

N

M

N

M

1KK55E

1PA4E

P1 J1

U

V

U

V

ref: WDM 80-11-04ref: WDM 24-30-00

G12132-3-01


3 6

3

2

1

MS24523-26

G12132-3-05

ESN-5CRANK

PP6

GENERATOR ON / RESETESN-3

1

2

4

5


G12132-3-073476 B


GA 02/05/13

CLB 02/05/13

GA107 1


CRANK

2.5A

EFN-63


ref: WDM 24-30-00

1DH6E

G12132-3-22

d d

1WW1E E

P2

E

J2

b

c

P1

ee

1

2

3

4

5

6

G12132-3-18

G12132-3-19

G12132-3-20b

c


WARN / FIRE TEST

G12132-3-21

G12132-3-04

J1

ee

ESN-7

WARN PANEL 1

GND for OVERLAYS

2.5A

EFN-37

PP5

G12132-23-09

1PE4NE or GND

1WW38E

1WW2NE

1WW82E




ref: WDM 26-11-00


ref: WDM 29-11-00

MS24658-26F

ESN-11HYD TEST

HYDRAULICSPP5

7.5A

EFN-36

P1 J1G12132-3-101DH1E

and 1DH112E

G12132-3-09

u

ref: WDM 29-11-00


u

G12132-3-16

G12132-3-17

G12132-3-033

2

1

CHANGED ESN-11 SWITCH TYPEA 04/12/17 GA

ACCU TST or

ADDED ACCU TST OPTIONB 10/20/17 GA


G12132-4-073476 --


GA 02/05/13

CLB 02/05/13

GA107 1


MS24524-21



1LX10E or 1LX31E H

P2

L

ref: WDM 33-41-00

STROBE LIGHT

7.5A G12132-4-19

EFN-45 G12132-4-20

PP9

G12132-4-18H

L

J2

ref: WDM 33-42-00

ANTI-COL LT

EFN-83

G12132-4-17

7.5A

1

2

3

4

5

6

(Center off)

G12132-4-21ALL / TAIL

ESN-9PP6

1

2

3

4

5

6

MS24524-23

POSITION LIGHTS

1LJ1E

ref: WDM 33-41-00

POSITION LTS

EFN-87

PP6

G12132-4-13

G12132-4-14

B

J2

B

P2

7.5A

ESN-10

EFN-95

LANDING LIGHT

20A

118L

1LM7E

AN16ga.1LM6E

1LM6E-1 ZY

P2G12132-4-01

G12132-4-04AN16ga.

ZY

J2PP9




ref: WDM 33-43-01


1

2

3

4

5

67.5A

G12132-4-123LK675E

1LK671E

D D

C C

G12132-23-02G12132-4-07

1

2

3

4

5

6

MS24524-23

MS24524-23INSTRUMENT LIGHTS 2

ESN-15

EFN-43

P2 J2


PP5

G12132-23-01

INST. LTS-1

G12132-4-08

(Double pole switches used for current rating.)

G12301:2 DIMMER CONTROL (SEE G12132-23-073476)

G12301:1 DIMMER CONTROL(SEE G12132-23-073476)


PP15PP15

EFN-75

INST. LTS-2INST. LTS-2

EFN-75

7.5AG12132-4-11

ref: WDM 33-10-00

N/A-6

LAND CTL

2.5A1LM8E pP1

G12132-4-01pJ1

PP6

A2

A1

EFN-79

TAXI LIGHT

7.5A

273L

1LM2E1LM9E

G

P2G12132-4-15G

J2PP6

NOTE: If a TAXI LIGHT indicatorlight is required, the installer shall provide a suitable light and install it within clear view of the pilot, with an appropriate label.

ref: WDM 33-43-02N/A-5

TAXI CTL

2.5A1LM1802EP1

G12132-4-16J1

PP6

A2A1

q q


SEE G12132-16-073476 FOR SAMPLE OPTIONAL CIRCUITSThe OP-x switches and wiring are optional. If they are installed, they must be labeled to show their function.

Installer Defined

Installer Defined

Installer Defined

Installer Defined

U U

G12132-5-13 AN16ga.

G12132-5-12 AN16ga.

W

V

W

V

AVIONICS MASTER

1

2

3

4

5

6

MS24524-23

G12132-5-11AN16ga

G12132-5-10

T

P2

T

J2

AN16ga

OP-1

NOTE: If a FUEL PUMP indicator light is required, the installer shall provide a suitable light and install it within clear view of the pilot, with an appropriate label.

ref: WDM 30-31-00

(ref: 21Q) 1QN1E

PP5

1FN1E

G12132-5-033

2

1

J2

MS24523-23

A

P2

A

G12132-5-04

PITOT HEATESN-13

ref: WDM 28-00-00

1QW1G

7.5A

EFN-39

PITOT HEAT

DD

P1

DD

J1

G12132-5-02

G12132-5-013

2

1

MS24523-23

FUEL PUMPESN-2

EFN-67

7.5A

FUEL PUMPPP6

G12132-5-091KS2E yy

G12132-5-073476 --


GA 02/05/13

CLB 02/05/13

GA107 1

ref: WDM 71-61-10



1

2

3

4

5

6

MS24524-23

G12132-5-08

SAND FILTER

Installer Defined

Installer Defined

1KS3E

G12132-5-21

P1 J1

HH

GG

G12132-5-22

P1

x

HH

GG

J1

x

ESN-21SAND FILTER

G12132-5-07

EFN-66

7.5A

PP6

EFN-91

ref: WDM 30-42-00

1MK1E Blue

1MK1E Red

G12132-5-173

2

1

G12132-5-14

G12132-5-18

P

M

P2

P

M

J2

MS24523-23

W/S WIPERESN-24

PP9

7.5A

W/S WIPER


1LK639E

1FW2E


MS24523-26

ref: WDM 29-11-00

G12132-3-26

G12132-3-25

G12132-3-243

2

1

OP-3SERVO TEST

BB

FF

CC

P1

1DH74E

1DH14E

1DH70NE BB

FF

CC

J1


NR/NF PP5

PITOT HEAT


3EU3E

PP5

7.5A

EFN-39

G12132-6-03P1

A A

J1

EFN-38

2.5A

HYDRAULICS

WARNING PANEL 1 PP5

EFN-37

2.5A

PP5

7.5A

EFN-36

G12132-6-073476 --


GA 02/05/13

CLB 02/05/13

GA107 1

EFN-43

INST. LTS-1

7.5A

EFN-42

1KK46E Red v

P1

GOV A


v

PP5

G12132-6-05J1

PP5

EFN-41

2.5A

1WW72E

P1

D

ASU1-3

G12132-6-04J1

D

PP5


7.5A7.5A


ref: WDM 63-41-00

ref: WDM 31-41-00

ref: WDM 80-11-04




Installer Defined

ATTITUDE GYRO

RELEASE

Installer Defined

G12132-7-05u

P1

u

J1


G12132-7-04 AN16ga.

PP5

2.5A

EFN-49

N N

PP5

EFN-48

P2 J2

2.5A

STROBE LIGHT

1EW116E


EFN-46

G12132-7-03P1

s

J1

s

PP5VEMD-1

7.5A

PP9

EFN-45

7.5A

2.5A

G12132-7-073476 --


GA 02/05/13

CLB 02/05/13

GA107 1

G12132-7-01

EXT. LOAD

1ME87E

EFN-58

P1

w

J1

w

2.5A

PP9

EFN-57


G12132-7-08

G12132-7-06

IDL / FLT SEL

1WW31E

PP9

E

P1

E

J1

WARNING PANEL 2 PP6

EFN-56

2.5A

VEMD-2

1EW119E

EFN-55

P1

K K

J1

7.5A

PP6


ref: WDM 31-61-00

ref: WDM 25-00-00

ref: WDM 34-25-30

ref: WDM 25-91-00


ref: WDM 24-30-00

ref: WDM 31-61-00

ref: WDM 25-63-10ref: WDM 25-63-11ref: WDM 25-92-00ref: G12132-17-073476

ref: WDM 25-91-10

ref: G12132-18-073476


ref: WDM 77-00-04

1KW56E G12132-8-03

EFN-61

2.5A

P1

r

J1

r

ref: WDM 80-11-04

J1P1

G12132-8-02

G12132-8-01

FADEC TEST

1QW1E C

P1

PP6

C

J1

FUEL GAUGE

EFN-60

2.5A

1KW182E B

PP6

B

ENG CTL

7.5A

EFN-59

PP6

G12132-8-073476 --


GA 02/05/13

CLB 02/05/13

GA107 1

EFN-65

7.5A

EFN-66


P1

i


PP6

G12132-8-06J1

i

EFN-63

2.5A

7.5A

EFN-64

1KK138E Red

P1

L

GOV B

CRANK

G12132-8-05

PP6

J1

L

PP6

PP6


ref: WDM 28-00-00 ref: WDM 80-11-04


ref: WDM 77-30-007.5A

1KW64E Red

EDR


2.5A

EMERGENCY NR INDICATOR

EMERGENCY IDL / FLT SEL


1DT5E

EFN-72K

1A

EFN-71E

1A

EMER BUS BAR

EMER BUS BAR

H H

P1

EFN-70

J1G12132-9-02

1WW34E

J1P1

PP9HOUR METER

AA AAG12132-9-01

PP6

EFN-68

2.5A

ASU1-2

PP6FUEL PUMP

EFN-67

7.5A

PP6

G12132-9-073476 --


GA 02/05/13

CLB 02/05/13

GA107 1

PP6POSITION LTS

7.5A

EFN-87

PP6ANTI-COL LT

7.5A

EFN-83

TAXI LIGHT

7.5A

EFN-79


G12132-9-031LE1E J

P1

J

J1

CABIN LIGHTS

2.5A

EFN-76

PP6

INST. LTS-2

EFN-75

PP15

7.5A



ref: WDM 31-31-00

ref: WDM 31-41-00

Detailed on G12132-5-073476Detailed on G12132-4-073476

ref: WDM 33-12-00





Detailed on G12132-4-073476LANDING LIGHT

ref: WDM 80-11-04

1KW4E

1MH1E

20A

EFN-95

G12132-10-03 AN16ga.

G12132-10-04 AN16ga.

EFN-94

PP9

P2

X

J2

X

PP9

10A

START

a

P2

a

J2

Detailed on G12132-5-073476W/S WIPER

CARGO HOOK

POWER OUTLET

ref: WDM 24-60-01

ref: WDM 25-92-00

1ME1E G12132-10-02 AN16ga.cc

PP9

15A

EFN-93

10A

EFN-92

P2 J2

PP9

EFN-91

7.5A

G12132-10-01

Wire directly to the Directional gyro, or through a relay or an On/Off switch; or, this function may be moved to a breaker that is supplied from a switched bus.

G12132-10-073476 --


GA 02/05/13

CLB 02/05/13

GA107 1

G12132-10-09

G12132-10-08


3PW53E and 3PW55E g

P1

g

J1

3PW54E and 3PW54F

ref: WDM 24-60-02

ref: WDM 24-60-02

EFN-N/A-4

D-BAT CONTROL

P1

h

PP15

3A

h

J1

a

DIRECT BATTERY

EFN-N/A-3

(1FF210F)

PP6

2.5A

a


G12132-10-06

G12132-10-05 AN16ga.

ref: WDM 34-21-03

G G

EFN-N/A-2

P1

DIR. GYRO

2.5A

J1

PP6

EFN-N/A-1

P1 J1

PP9

ref: WDM 24-22-00

P2

b

AC INVERTER

EFN-97

1XU1E b

J2

15A

PP9

2.5A

HYD MAINref: WDM 29-11-00

1DH78F


ref: WDM 25-26-06

61

Source directly from wire 1MY41E, or through an available power terminal post. See G12132-36 for examples.

61









BUS BAR, Top Left



1PP9E

3PP23E

TB6

TB5AN8ga G12132-11-14

AN8ga G12132-11-04

AN8ga G12132-11-15

1PP6E

1PP5E

TB3

TB2

TB1AN8ga G12132-11-01

AN8ga G12132-11-02

AN8ga G12132-11-03


G12132-11-073476 --


GA 02/05/13

CLB 02/05/13

GA107 1


G12135-10

G12135-12

G12135-9

G12135-2


ESN-6

MS24659-23D

1

2

3

4

5

6

MASTER CUTOFF

G12135-2

G12135-10

G12135-8

G12135-9

AN16ga G12132-2-10

ref: G12132-2-073476



MS24524-23

INST. LTS-1

2.5A, PP5, EFN-38

NR

/NF

2.5A, PP6, EFN-68

WAR

N PN

L 2

FWD

G12132-13-073476 --


GA107 1

GA 02/05/13

GA 02/05/13

GA 02/05/13

CLB 02/05/13

7.5A, PP6, EFN-59

2.5A, PP6, EFN-60

FUEL G

AUG

EEN

G C

TL

Effectivity: AS350B3 Embodying Mod 350A07-3476 (B3e)

7.5A, PP6, EFN-64

7.5A, PP6, EFN-83

ANTI-C

OL LT

EM-N

R IN

D

DIR

. GYR

O2.5A, PP6, EFN

-N/A-2

7.5A, PP6, EFN-87

POSITIO

N LT

1A, EMER

BUS, EFN

-72K

EM-ID

L/FLT

1A, EMER

BUS, EFN

-71E

7.5A, PP6, EFN-65

EDR

GO

V B

2.5A, PP6, EFN-76

CABIN

LTS

7.5A, PP6, EFN-79

TAXI LIGH

T

DIR

ECT BATT

2.5A, PP6, EFN-N

/A-3ASU

1-2

2.5A, PP6, EFN-61

FADEC

TEST

2.5A, PP6, EFN-63

CR

ANK

TAXI LIGH

T

10A, PP9, EFN-94

IDL/FLT SEL

START

LAND

ING

LIGH

TM

S24523-23

ANTI-C

OL LT

POSITIO

N LTS

INST. LTS-2M

S24524-23

MS24524-21

INST. LTS-1

RELEASE

ATTITUD

E

2.5A, PP9, EFN-57

2.5A, PP5, EFN-49

2.5A, PP5, EFN-48

VEMD

-17.5A, PP5, EFN

-46

2.5A, PP5, EFN-41

7.5A, PP5, EFN-39

PITOT H

EAT

7.5A, PP5, EFN-42

GO

V A

ASU1-3

MS24524-23

MS24524-23

7.5A, PP6, EFN-55

VEMD

-2

2.5A, PP6, EFN-56

7.5A, PP6, EFN-66

7.5A, PP6, EFN-67

FUEL PU

MP

SAND

FILTERH

YDR

AULIC

S

WAR

N PN

L 1

7.5A, PP5, EFN-36

2.5A, PP5, EFN-37

MS24524-23

WAR

NIN

G H

OR

N

G12132-4-073476, ESN

-18

G12132-4-073476, ESN

-17

G12132-4-073476, ESN

-15

G12132-4-073476, ESN

-9

G12132-4-073476, ESN

-10

G12132-4-073476, ESN

-14

G12132-3-073476, ESN

-12

G12132-3-073476, 29-11-00

G12132-3-073476, 24-30-00

G12132-6-073476, 63-41-00

G12132-6-073476, 31-41-00

G12132-6-073476, 80-11-04

G12132-5-073476, 30-31-00

G12132-7-073476, 31-61-00

G12132-7-073476, 25-00-00

G12132-4-073476, 33-10-00

G12132-7-073476, 34-25-30

G12132-2-073476, 80-11-04

G12132-10-073476, 80-11-04

G12132-7-073476, 31-61-00

G12132-7-073476, 24-30-00

G12132-8-073476, 28-00-00

G12132-8-073476, 77-00-04

G12132-8-073476, 80-11-04

G12132-8-073476, 80-11-04

G12132-3-073476, 80-11-04

G12132-8-073476, 77-30-00

G12132-2-073476, 80-11-04

G12132-2-073476, 63-41-00

G12132-5-073476, 71-61-10

G12132-5-073476, 28-00-00

G12132-9-073476, 31-41-00

G12132-10-073476, 24-60-02

G12132-9-073476, 33-12-00

G12132-4-073476, 33-42-00

G12132-4-073476, 33-43-02

G12132-4-073476, 33-41-00

G12132-10-073476, 34-21-03

7.5A, PP5, EFN-43


G12132-13-073476-P122 --


GA107 1

GA 02/05/13

GA 02/05/13

GA 02/05/13

CLB 02/05/13

Effectivity: AS350B3 EmbodyingMod 350A07-3476 (B3e)

G12132-10-073476

G12132-4-073476

34-21-03

33-41-00

7.5A, PP6, EFN-87

POSITION LTS

DIR. GYRO2.5A, PP6, EFN-N/A-2

G12132-8-07347677-30-00

G12132-3-073476

G12132-8-073476

2.5A, PP6, EFN-63


CRANK

EDR7.5A, PP6, EFN-65

80-11-04

80-11-04

G12132-9-073476

G12132-4-073476

G12132-4-073476

33-42-00

33-43-02

33-12-00



G12132-10-073476

G12132-9-073476

24-60-02

31-41-00

ASU1-22.5A, PP6, EFN-68

DIR BATT2.5A, PP6, EFN-N/A-3

2.5A, PP6, EFN-76

CABIN LTSG12132-8-073476

G12132-8-073476

G12132-8-073476

2.5A, PP6, EFN-60

FUEL GAUGE

FADEC TEST2.5A, PP6, EFN-61

80-11-04

28-00-00

80-11-04

G12132-7-073476

G12132-7-073476

2.5A, PP6, EFN-56


WARN PNL-2


24-30-00

31-61-00

G12132-5-073476

G12132-5-073476

28-00-00

71-61-10



G12132-2-073476

G12132-2-073476EM-NR IND1A, EMER, EFN-71E

EM-IDL/FLT1A, EMER, EFN-72K

63-41-00

80-11-04

FWD

G12132-7-073476

2.5A, PP5, EFN-48

2.5A, PP5, EFN-49

G12132-7-07347634-25-30

ATTITUDE

G12132-7-07347625-00-00

31-61-00

RELEASE

INST. LTS-1

7.5A, PP5, EFN-42

7.5A, PP5, EFN-46

G12132-4-07347633-10-00

VEMD-1

G12132-6-07347680-11-04

7.5A, PP5, EFN-43

GOV A

G12132-6-073476

7.5A, PP5, EFN-39

2.5A, PP5, EFN-41

PITOT HEAT

G12132-6-07347631-41-00

ASU1-3

G12132-5-07347630-31-00

63-41-00

7.5A, PP5, EFN-36

2.5A, PP5, EFN-37

2.5A, PP5, EFN-38

WARN PNL-1

HYDRAULICS

G12132-3-07347624-30-00

NR/NF

G12132-3-07347629-11-00

G12132-10-073476

IDL/FLT SEL2.5A, PP9, EFN-57

80-11-04

10A, PP9, EFN-94

START

G12132-2-07347680-11-04


G12132-14-073476 --


GA107 1

GA 02/05/13

GA 02/05/13

GA 02/05/13

CLB 02/05/13

15A,

PP9

, EFN

-92

W/S

WIP

ERG

1213

2-5-

0734

76, 3

0-42

-00

CAR

GO

HO

OK

FWD

7.5A

, PP9

, EFN

-91

HO

UR

MET

ERH

YD M

AIN


AC IN

VER

TER

15A,

PP9

, EFN

-97

STR

OBE

LT

7.5A

, PP9

, EFN

-45

G12

132-

10-0

7347

6, 2

4-60

-01

G12

132-

10-0

7347

6, 2

5-92

-00

PWR

OU

TLET

15A,

PP9

, EFN

-93

G12

132-

4-07

3476

, 33-

41-0

0LA

ND

ING

LT

G12

132-

4-07

3476

, 33-

43-0

1

20A,

PP9

, EFN

-95

G12

132-

9-07

3476

, 31-

31-0

0

2.5A

, PP9

, EFN

-70

G12

132-

7-07

3476

, 25-

91-0

0

EXT.

LO

AD

2.5A

, PP9

, EFN

-58

G12

132-

10-0

7347

6, 2

4-22

-00

2.5A

, PP9

, EFN

-N/A

-1G

1213

2-10

-073

476,

29-

11-0

0

G12

132-

2-07

3476

, ESN

-1

MS2

4659

-23D

BAT-

EXT

PWR

G12

132-

5-07

3476

, ESN

-21

SAN

D F

ILTE

R

MS2

4524

-23

G12

132-

3-07

3476

, OP-

3

G12

132-

5-07

3476

, ESN

-24

W/S

WIP

ER

G12

132-

5-07

3476

, ESN

-2

FUEL

PU

MP

MS2

4523

-23

MS2

4523

-23

G12

132-

2-07

3476

, OP-

2

DIR

ECT

BATT

MS2

4523

-23

G12

132-

5-07

3476

, OP-

1

AVIO

NIC

S

MS2

4524

-23

7.5A

, PP1

5, E

FN-7

5IN

ST.L

TS-2

G12

132-

4-07

3476

, 33-

10-0

0?A

, PP1

5, L

MB-

9O

ptio

nal

G12

132-

12-0

7327

3?A

, PP1

5, L

MB-

8O

ptio

nal

G12

132-

12-0

7327

3?A

, PP1

5, L

MB-

7O

ptio

nal

G12

132-

12-0

7327

3?A

, PP1

5, L

MB-

6O

ptio

nal

G12

132-

12-0

7327

3?A

, PP1

5, L

MB-

5O

ptio

nal

G12

132-

12-0

7327

3?A

, PP1

5, L

MB-

4O

ptio

nal

G12

132-

12-0

7327

3?A

, PP1

5, L

MB-

3O

ptio

nal

G12

132-

12-0

7327

3?A

, PP1

5, L

MB-

2O

ptio

nal

G12

132-

12-0

7327

33A

, PP1

5, E

FN-N

/A-4

D-B

AT C

TRL

G12

132-

12-0

7327

3

Opt

iona

l

?A, ?

bus,

LTB

-1

G12

132-

12-0

7327

3

Opt

iona

l

?A, ?

bus,

LTB

-2

G12

132-

12-0

7327

3

Opt

iona

l

?A, ?

bus,

LTB

-3

G12

132-

12-0

7327

3

Opt

iona

l

?A, ?

bus,

LTB

-4

G12

132-

12-0

7327

3

Opt

iona

l

?A, ?

bus,

LTB

-5

G12

132-

12-0

7327

3

Opt

iona

l

?A, ?

bus,

LTB

-6

G12

132-

12-0

7327

3

Opt

iona

l

?A, ?

bus,

LTB

-7

G12

132-

12-0

7327

3

Opt

iona

l

?A, ?

bus,

LTB

-8

G12

132-

12-0

7327

3

Opt

iona

l

?A, ?

bus,

LTB

-9

G12

132-

12-0

7327

3

Opt

iona

l

?A, ?

bus,

LTB

-10

G12

132-

12-0

7327

3

Opt

iona

l

?A, ?

bus,

LTB

-11

G12

132-

12-0

7327

3

Opt

iona

l

?A, ?

bus,

LTB

-12

SER

VO T

EST

MS2

4523

-23

G12

132-

10-0

7347

6, 2

4-60

-02


CARGO HOOK

PWR OUTLET

15A, PP9, EFN-92

15A, PP9, EFN-93

W/S WIPER7.5A, PP9, EFN-91

STROBE LT

AC INVERTER

20A, PP9, EFN-95

LANDING LT

15A, PP9, EFN-97

EXT. LOAD

G12132-10-073476

2.5A, PP9, EFN-58

HOUR METER


HYD MAIN

G12132-7-073476

G12132-10-073476

G12132-4-073476

G12132-10-073476

G12132-10-073476

G12132-5-07347630-42-00

25-92-00

24-60-01

33-43-01

24-22-00

25-91-00

FWD Effectivity: AS350B3 EmbodyingMod 350A07-3476 (B3e)

OptionalG12132-12-073273

2.5A, PP9, EFN-70

G12132-9-07347631-31-00

7.5A, PP9, EFN-45

G12132-4-07347633-41-00

G12132-14-073476-P122 --


GA107 1

GA 02/05/13

GA 02/05/13

GA 02/05/13

CLB 02/05/13

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

?A, ?bus, LTB-12 7.5A, PP15, EFN-75









?A, ?bus, LTB-3 3A, PP15, EFN-N/A-4

?A, ?bus, LTB-2

?A, ?bus, LTB-1

24-60-02

D-BAT CTRLG12132-10-073476

G12132-4-07347633-10-00

INST LTS 2

29-11-00


WIPER

G12132-5-073476, ESN-24

G12132-5-073476, ESN-21

DIRECT BATT

SAND FILTER

G12132-2-073476, OP-2

G12132-5-073476, OP-1

MS24524-23

MS24523-23

AVIONICSMASTER

AVIONICS

BATTERYDIRECT

MS24524-23

MS24523-23

W/S WIPER

SANDFILTER


G12132-2-073476, ESN-1

G12132-5-073476, ESN-2

BAT-EXT PWR

FUEL PUMP

G12132-3-073476, OP-3

WINDSHIELD

MS24659-23D

MS24523-23 PUMPFUEL

POWERBAT-EXT

G12

132-

5-07

3476

, ES

N-1

3

G12

132-

2-07

3476

, ES

N-6

G12

132-

3-07

3476

, ES

N-7

G12

132-

3-07

3476

, ES

N-5

G12

132-

3-07

3476

, ES

N-1

1

G12

132-

3-07

3476

, ES

N-3

PITO

T H

EAT

MS

2465

9-23

D

MS

2452

3-23

MA

STE

R C

UTO

FF

MS

2452

3-26

MS

2740

7-3

WA

RN

/ FI

RE

TE

ST

CR

AN

K E

NG

INE

MS

2465

8-23

D

MS

2452

4-31

GE

NE

RA

TOR

ON

HY

D T

EST

TESTWARN/FIRE

ON / RESETGENERATOR

TESTHYD

CUTOFFMASTER

ENGINECRANK PITOT

HEAT

LIGHTS

G12132-4-073476, ESN-10

G12132-4-073476, ESN-9

G12132-4-073476, ESN-17

G12132-4-073476, ESN-18

POSITION LTS

ANTI-COL LT

TAXI LIGHT

LANDING LT

LANDINGLIGHT

TAXILIGHT

MS24523-23

MS24524-23


MS24524-23

G12132-4-073476, ESN-15

G12132-4-073476, ESN-14

G12132-3-073476, ESN-12

INST. LTS-2

INST. LTS-1

WARNING HORN

LIGHTS 2INSTRUMENT

POSITION

MS24524-23

LIGHTS 1INSTRUMENT

WARNINGHORN

MS24524-23

MS24524-23

G12132-15-073476 --


GA107 1

GA 02/05/13

GA 02/05/13

GA 02/05/13

CLB 02/05/13

SERVO TEST

SERVOTESTMS24523-23


A See Revision Block on G12132-1-073476

WIPER

G12132-5-073476, ESN-24

G12132-5-073476, ESN-21

DIRECT BATT

SAND FILTER

G12132-2-073476, OP-2

G12132-5-073476, OP-1

MS24524-23

MS24523-23

AVIONICSMASTER

AVIONICS

BATTERYDIRECT

MS24524-23

MS24523-23

W/S WIPER

SANDFILTER


G12132-2-073476, ESN-1

G12132-5-073476, ESN-2

BAT-EXT PWR

FUEL PUMP

G12132-3-073476, OP-3

WINDSHIELD

MS24659-23D

MS24523-23 PUMPFUEL

POWERBAT-EXT

G12

132-

5-07

3476

, ES

N-1

3

G12

132-

2-07

3476

, ES

N-6

G12

132-

3-07

3476

, ES

N-7

G12

132-

3-07

3476

, ES

N-5

G12

132-

3-07

3476

, ES

N-1

1

G12

132-

3-07

3476

, ES

N-3

PIT

OT

HE

AT

MS2

4659

-23D

MS2

4523

-23

MAS

TER

CU

TOFF

MS2

4523

-26

MS2

7407

-3

WAR

N /

FIR

E T

EST

CR

AN

K E

NG

INE

MS2

4658

-26F

MS2

4524

-31

GE

NE

RA

TOR

ON

HY

D T

EST

TESTWARN/FIRE

ON / RESETGENERATOR

TESTHYD

CUTOFFMASTER

ENGINECRANK PITOT

HEAT

LIGHTS

G12132-4-073476, ESN-10

G12132-4-073476, ESN-9

G12132-4-073476, ESN-17

G12132-4-073476, ESN-18

POSITION LTS

ANTI-COL LT

TAXI LIGHT

LANDING LT

LANDINGLIGHT

TAXILIGHT

MS24523-23

MS24524-23


MS24524-23

G12132-4-073476, ESN-15

G12132-4-073476, ESN-14

G12132-3-073476, ESN-12

INST. LTS-2

INST. LTS-1

WARNING HORN

LIGHTS 2INSTRUMENT

POSITION

MS24524-23

LIGHTS 1INSTRUMENT

WARNINGHORN

MS24524-23

MS24524-23

G12132-15-073476 B


GA107 1

GA 02/05/13

GA 02/05/13

GA 02/05/13

CLB 02/05/13

SERVO TEST

SERVOTESTMS24523-23


A Changed EFN-11 switch type 04/12/17 GA


B Added ACCU TST note 10/20/17 GA

G12132-3-073476ESN-5, MS24523-26

P122 CONSOLE LAYOUT

G12132-5-073476

G12132-4-073476ESN-17, MS24524-23

ESN-13, MS24523-23

ESN-15, MS24524-23G12132-4-073476

G12132-5-073476OP-1, MS24524-23

G12132-4-073476

AVIONICSMASTER

ESN-14, MS24524-23


ESN-10, MS24524-23G12132-4-073476 G12132-4-073476

ESN-9, MS24524-21

PANELDIMMER

SERVOTEST

GENERATORON / RESET

G12132-3-073476ESN-3, MS24524-31

INSTRUMENTLIGHTS 2

G12132-5-073476OP-3, MS24523-26

G12132-5-073476

INSTRUMENTLIGHTS 1

ESN-2, MS24523-23

FUELPUMP

ESN-1, MS24659-23DG12132-2-073476

BAT-EXTPOWER

G12132-3-073476ESN-11, MS24658-23D

ESN-21, MS24524-23G12132-5-073476

POSITIONLIGHTS

SANDFILTER

ANTI-COLALL / TAIL

ESN-24, MS24523-23G12132-5-073476

WINDSHIELDWIPER

G12132-3-073476ESN-7, MS27407-3

HYDRAULICTEST

WARN / FIRETEST

DIRECT BATTERY

ESN-18, MS24523-23G12132-4-073476

OP-2, MS24523-23G12132-2-073476

WARNINGHORN

G12132-2-073476ESN-6, MS24659-23D

LANDINGLIGHT

ESN-12, MS24524-23G12132-3-073476

TAXILIGHT

PITOTHEAT

MASTERCUTOFF

CRANKENGINE

G12132-15-073476-P122 --


GA107 1

GA 02/05/13

GA 02/05/13

GA 02/05/13

CLB 02/05/13


G12132-3-073476ESN-5, MS24523-26

P122 CONSOLE LAYOUT

G12132-5-073476

G12132-4-073476ESN-17, MS24524-23

ESN-13, MS24523-23

ESN-15, MS24524-23G12132-4-073476

G12132-5-073476OP-1, MS24524-23

G12132-4-073476

AVIONICSMASTER

ESN-14, MS24524-23


ESN-10, MS24524-23G12132-4-073476 G12132-4-073476

ESN-9, MS24524-21

PANELDIMMER

SERVOTEST

GENERATORON / RESET

G12132-3-073476ESN-3, MS24524-31

INSTRUMENTLIGHTS 2

G12132-5-073476OP-3, MS24523-26

G12132-5-073476

INSTRUMENTLIGHTS 1

ESN-2, MS24523-23

FUELPUMP

ESN-1, MS24659-23DG12132-2-073476

BAT-EXTPOWER

G12132-3-073476ESN-11, MS24658-26F

ESN-21, MS24524-23G12132-5-073476

POSITIONLIGHTS

SANDFILTER

ANTI-COLALL / TAIL

ESN-24, MS24523-23G12132-5-073476

WINDSHIELDWIPER

G12132-3-073476ESN-7, MS27407-3

HYDTEST

WARN / FIRETEST

DIRECT BATTERY

ESN-18, MS24523-23G12132-4-073476

OP-2, MS24523-23G12132-2-073476

WARNINGHORN

G12132-2-073476ESN-6, MS24659-23D

LANDINGLIGHT

ESN-12, MS24524-23G12132-3-073476

TAXILIGHT

PITOTHEAT

MASTERCUTOFF

CRANKENGINE

G12132-15-073476-P122 C


GA107 1

GA 02/05/13

GA 02/05/13

GA 02/05/13

CLB 02/05/13


A Changed EFN-11 switch type 04/12/17 GA


B Added ACCU TST note 10/20/17 GA

C Changed ESN-11 switch image to locking switch. 11/08/17 GA

FROM G12132-5-073476

AN16ga

G12132-5-12

G12132-5-13


G12132-5-10

AVIONICS-2 BUS

AVIONICS-1 BUS

RELAYAVIONICS

EXTERNAL TO CONSOLE

PP128 ga.50A

AVIONICSA1

(Airframe GND)

X2

W

V

W

V

(no connection)


(no connection)

8 ga.

A2

X1

TB4

T

U

P2

T

U

J2

AN16ga



ALT. ENCODER

2.5A

TRANSPONDER

2.5A

2.5A

AUDIO PANEL

COM2

10A

GPS

5A

CD CHANGER

2.5A

COM1

10A

STEREO ICS

2.5A

G12132-10-05


EFN-97


G12132-16-073476 --


GA 02/05/13

CLB 02/05/13

GA107 1

AN16ga

AN16ga

AVIONICS MASTER

1

2

3

4

5

6

MS24524-23

G12132-5-11

OP-1 AN16ga

45

G12132-16-04b b


45 15A

P2 J2


FROM G12132-10-073476

FROM G12132-5-073476


AN16ga

PP9

G12132-7-04

AN16ga

G12132-5-13

G12132-5-12

G12132-5-10


EFN-48

NNAN16ga

G12132-16-02 AN16ga

G12132-16-01 AN16gaW

V

W

V

T

U

P2

T

U

J2


45

G12132-16-03P2 J2

15A

FROM G12132-7-073476

1

2

3

4

5

6

MS24524-23

G12132-5-11

AN16ga

AN16ga

AVIONICS MASTEROP-1

AN16ga


AN16ga

PP5



Effectivity: AS350B3 embodying mod 350A07-3476 (B3e)

1ME3E


N N

From G12132-7-073476

G12132-17-01

More samples on G12132-18SAMPLE OPTIONAL CIRCUITSMore samples on G12132-18-073476

ref: WDM 25-00-00ref: WDM 25-92-00

J2P2

EFN-48

RELEASE

2.5A

G12132-7-04

PP5

3

2

1

G12132-17-073476 --


GA 02/05/13

CLB 02/05/13

GA107 1


MS24523-23



(Installer Defined)CARGO HOOK

G12132-17-02

G12132-17-03

ref: WDM 25-92-0046

ref: WDM 25-00-00

28


28

There is no standard switch assigned to the CARGO HOOK function in the -073476 version of the console. If a CARGO HOOK circuit is required, implement it using an available optional switch, or using a switch mounted in an installer-defined location outside the console. The wire numbers shown are only an example. If an internal switch is used, the wire numbers should be updated to match the internal console wiring for that switch. If an external switch is used, the installer may use these numbers, or assign unique wire numbers as appropriate.

46

**

P*

**

J*


Effectivity: AS350B3 embodying mod 350A07-3476 (B3e)


G12132-18-02


23

24 Installer

HOIST23

G12132-18-07

CAPACITYInstaller

450lb300lb 2.5A

7.5ARATING24


From G12132-7-073476

ref: WDM 25-63-10ref: WDM 25-63-11

J2

N

P2

N

EFN-48

2.5A

G12132-7-04

RELEASE PP5

G12132-18-06

G12132-18-073476 --


GA 02/05/13

CLB 02/05/13

GA107 1


G12132-18-03

G12132-18-04300lb UNIT: 1ME33E

450lb UNIT: 1ME101E1ME36E


From G12132-5


G12132-18-05

G12132-18-01

1

2

3

4

5

6

MS24524-23

HOIST

**

***

*

P*

*

J*

*

(Installer Defined)48

ref: WDM 25-00-00ref: WDM 25-63-11

30


30

There is no standard switch assigned to the HOIST function in the -073368 version of the console. If a HOIST circuit is required, implement it using an available optional switch, or using a switch mounted in an installer-defined location outside the console. The wire numbers shown are only an example. If an internal switch is used, the wire numbers should be updated to match the internal console wiring for that switch. If an external switch is used, the installer may use these numbers, or assign unique wire numbers as appropriate.

48

Defined

DefinedSource

P* J*

* *


ref: WDM 25-63-10

ref: WDM 25-00-00

DIRECT BATTERY

EM-IDL / FLT

IDL / FLT SEL

1A

PP9

2.5A

EFN-57

EFN-72K

EMER

G12132-2-15

D4:A

D2:A

G12132-2-16

D4:C

1

2

3

4

5

6

MS24659-23D

MASTER CUTOFF


ref: WDM 24-30-00

P1 J1

ESN-6

3PE53E


1PG6NE

1PG1NE

1PG2NE

1PG3NE

zz

X

Y Y

X

W

S

R R

S

W

G12132-2-13

G12132-2-10

G12132-2-09

G12132-2-06

G12132-2-05

G12132-2-02

1

2

3

4

5

6

MS24659-23D

BAT-EXT PWR

G12132-2-07

ESN-1

MS24524-23

G12132-2-18

G12132-2-17

Z Z

G12132-2-11 T TJ1 P1

3KK115E


NOTICE:The circuitry related to the BAT-EXT PWR switch and the MASTER ELECTRICAL CUTOFF switch has been changed from the Eurocopter original circuitry. Install using this wiring, and use this drawing for future electrical troubleshooting.

OP-2

G12132-2-074280 E


GA 12/05/12

CLB 12/05/12


ref: WDM 80-11-04ref: WDM 24-60-02

P2J2EM-NR IND

1A

EFN-71E D5:A

G12132-2-19

D5:C

EMER

G12132-2-20F F 3EU3F

D2:C

3PE40E F F G12132-2-04

D1:A

G12132-2-03

D1:C

D3:C D3:A

G12132-2-08

A Added Effectivity note. 2/04/13

Effectivity: AS350B3 embodying Mod 350A07-4280

GA

B PP49 switching separated from PP50 Changed Direct Battery Indicator Wiring

4/08/13 GA

G12132-2-30 AN 18ga.

The EMER emergency bus MUST be rewired to match this diagram. The 5A circuit breaker is not present in the factory configuration and must be provided by the installer. The cable length between the battery and the 5A breaker must be kept as short as possible.

EMER BUS BARG12132-2-21 AN16ga

1

2

3

4

5

6

G12132-2-01

G12132-2-14

NOTE: If the DIRECT BATTERY indicator light is desired, the installer shall provide a suitable light and install it within clear view of the pilot, with an appropriate label. Recommended maximum current 12mA.

3LK296E


ref: G12132-11-074280

G12132-2-12

C Minor text changes. 6/19/13 GA

D Changed Effectivity note. Added WDM ref for EM-IDL/FLT. Minor text changes. 8/14/13 GA

ref: WDM 63-41-00

NOTE: Cap and Stow 1PE1E

E Added note for 1PE1E. Changed name of airframe wire from P1:T. Changed PP46 to EMER bus. Added note about 5A EMER bus breaker.

12/05/14 GA

The added aircraft-side wire listed here as G12132-2-30 must be labelled, but at the installer's discretion the label format may vary from the format used here provided it uniquely identifies each wire.

21P BATTERY(Right Hold)

5AAN 8ga.

EMERBUS

(Right Hold)

ref: WDM 63-41-00

1EW93NE

1EW37E

1EW38E

1EW39E

n

m m

n

k

jP1

k

jJ1

G12132-3-161

2

3

4

5

6

G12132-3-15

G12132-3-14

MS24524-23

G12132-3-17

WARNING HORNESN-12

G12132-3-08

G12132-3-07

G12132-3-06

G12132-3-02

The Generator switch has a center off position. The forward position provides the normal GENERATOR ON function. The momentary aft position provides the GENERATOR RESET function.GENERATOR RESET receives power from CRANK breaker. GEN RST breaker is not installed.

PP1KK53E

1PA1E

1PA2E

N

M

N

M

1KK55E

1PA4E

P1 J1

U

V

U

V

ref: WDM 80-11-04ref: WDM 24-30-00

G12132-3-01


3 6

3

2

1

MS24523-26

G12132-3-05

ESN-5CRANK ENGINE

PP6

GENERATOR ON/RESET

G12132-3-03ESN-3

1

2

4

5


G12132-3-074280 G


GA 12/05/12

CLB 12/05/12

GA107 1


CRANK

2.5A

EFN-63

G12132-3-223WW1E E

P2

E

J2

b

c

P1

e

1

2

3

4

5

6

G12132-3-19

G12132-3-20b

c


WARN/FIRE TST

G12132-3-21

G12132-3-04

J1 ESN-7

WARN PNL-1

GND for OVERLAYS

3A

EFN-37

PP15

G12132-23-09

1PE95NE or GND

1WW38E


NOTE: If PP15 Bus is mounted outside the console, it is the installers responsibility to provide ESN-7 pin 5 with power from the WARN PNL-1 breaker.


ref: WDM 26-11-10


MS24658-26F

ESN-11HYD TST

1WW84E

HYDRAULICSPP5

7.5A

EFN-36P1 J1

G12132-3-101DH131E u

e

ref: WDM 29-10-00


u

A Changed circuitry to support SB AS350-01.00.66. Changed ESN-7 switch type. Added Effectivity note.

3

2

1

G12132-3-09

2/04/13

Effectivity: AS350B3 embodying Mod 350A07-4280GA


d1DH130E d

B Changed WARN/FIRE TEST wiring. 4/08/13 GA

G12132-3-18

C Changed WARN/FIRE TEST wiring. 6/19/13 GA

D Changed Effectivity note. Changed WARN/FIRE TEST external connection. 8/14/13 GA

ref: WDM 24-30-00

G12132-3-231DH67E t t

E Changed Note for GEN RESET Circuit. Changed Hydraulic wiring. 12/05/14 GA

ref: WDM 29-11-00

3WW98EPre-MOD 074677

Post-MOD 074677

F Wire connection option for WARN PNL-1 Changed ESN-11 switch type. 9/27/16 GA

(Cap & Stow 3WW89E)

ACCU TST or

G Added ACCU TST Option. Changed TEST to TST. 10/20/17 GA

G12132-4-074280 D


GA 12/05/12

CLB 12/05/12

GA107 1


MS24524-21

ANTI-COL


1LX54F H

P2

L

ref: WDM 33-41-00STROBE LT

7.5A G12132-4-19

EFN-45 G12132-4-20

PP9

G12132-4-18H

L

J2

ref: WDM 33-42-00

ANTI-COL LT

EFN-83

G12132-4-17

7.5A

1

2

3

4

5

6

(Center off)

G12132-4-21ALL / TAIL

ESN-9PP6

The STROBE LIGHT switch circuit is optional and is usually used for additional strobe lights. If no additional strobe light is installed, wires G12132-4-19, G12132-4-20 and G12132-4-21 may be deleted.

ref: WDM 33-43-01


PP6TAXI LIGHT

7.5A

EFN-79

1LM9E G G

P2 J2G12132-4-04

LANDING LT

20A

EFN-95

PP9

G12132-4-05G12132-4-03 1LM1802E g

P1

g

J1

EFN-N/A-4

TAXI CTL

P1

h

PP6

2.5A

h

J1

LAND CTL

EFN-N/A-3

PP6

2.5A

1LM6EG12132-4-01 AN16ga.

P2

Y

J2

YG12132-4-02 AN16ga.

Z Z

1LM8E

G12132-4-033

2

1

MS24523-23

LANDING LIGHTESN-18

G12132-4-06P1

h h

J1

1LM1E

At the installer's discretion the Landing Light switch may relocated from the Pilot's collective lever to the console, bypassing the collective switch as shown.

G12132-4-053

2

1

MS24523-23

TAXI LIGHTESN-17

G12132-4-07P1

g g

J1

1LM2008E

ref: WDM 33-43-01

ref: WDM 33-43-02

ref: WDM 33-43-02

At the installer's discretion the Taxi Light switch may relocated from the Pilot's collective lever to the console, bypassing the collective switch as shown.

Splice two AN16ga. wires from P2 pins Y and Z to 1LM6E. Wires should be kept as short as possible.

(1LJ5E or 1LJ48E or Installer Defined)


A Added Effectivity note. 2/04/13 GAB Added optional Position Light switch 4/08/13 GA

G12132-9-04 AN16ga.

MS24524-23


G12132-4-08 AN16ga.P1

d d

J1

1LJ3E

At the installer's discretion an optional POSITION LIGHT switch may be added to the console. This switch can turn off position lights when the [OFF/DAY/NIGHT] selector on the instrument panel is in DAY and NIGHT positions but does not turn on the position lights when the selector is in the OFF position.

EFN-87

POSITION LTS PP6

7.5A

1

2

3

4

5

6

(Double Pole switch used for current rating)

C Changed Effectivity note. Fixed POSITION LTS and ANTI-COL circuit wording and references. 8/14/13 GA

ref: WDM 33-41-00

D Changed Anti-Col external wire number. 10/20/17 GA

Disconnect 1LX54F and 1LX31E from the 245L relay and splice together.


Installer Defined

Installer Defined

Installer Defined

Installer Defined

U U

G12132-5-16 AN16ga.

G12132-5-15 AN16ga.

W

V

W

V

AVIONICS MASTER

1

2

3

4

5

6

MS24524-23

G12132-5-14AN16ga

G12132-5-13

T

P2

T

J2

AN16ga

OP-1

NOTE: If a FUEL PUMP indicator light is desired, the installer shall provide a suitable light and install it within clear view of the pilot, with an appropriate label.

ref: WDM 30-31-00

PP5

1FN35E

G12132-5-033

2

1

J2

MS24523-23

A

P2

A

G12132-5-04

PITOT HEATESN-13

ref: WDM 28-00-00

7.5A

EFN-39

PITOT HEAT

DD

P1

DD

J1

G12132-5-02

G12132-5-013

2

1

MS24523-23

FUEL PUMPESN-2

EFN-67

7.5A

FUEL PUMPPP6

G12132-5-091KS2E yy

G12132-5-074280 E


GA 12/05/12

CLB 12/05/12

GA107 1

ref: WDM 71-61-10



1

2

3

4

5

6

MS24524-23

G12132-5-10

SAND FILTER

Installer Defined

Installer Defined

1KS3E

P1 J1

HH

GG

P1

x

HH

GG

J1

x

ESN-21SAND FILTER

G12132-5-08

EFN-66

7.5A

PP6

OP-3

MS24523-26

EFN-91

1MK27E

1MK28E

G12132-5-173

2

1

G12132-5-19P

M

P2

P

M

J2

MS24523-23

WINDSHIELD WIPERESN-24

PP9

7.5A

W/S WIPER-1

NOTE: If a PITOT indicator light is desired, the installer shall provide a suitable light and install it within clear view of the pilot, with an appropriate label. Recommended maximum current 12mA.The Installer must install a relay of a suitable rating to drive the lamp, wired as shown.

1FW20E

1FW21E


G12132-5-18

G12132-5-11

G12132-5-12

SERVO TST

3

2

1

BB

FF

CC

P1

1DH74E

1DH14E

1DH70NE BB

FF

CC

P1

ref: WDM 29-11-00

ref: WDM 30-42-00

G12132-5-06

G12132-5-05

G12132-5-07

A Changed circuitry to support SB AS350-01.00.66. Added Effectivity note. 2/04/13


GA

B Changed Indicator light wiring 4/08/13 GA

1QN3E

215720

2321

141174

185

163619

42Q

1QN1E

1QW81NE 1QN26EBA

DE

M5

224L

FM1

133L4Remove existing wire between224L M5-A and 224L M12-D

The original FUEL PUMP circuit MUST be rewired to match this diagram.

A3A1A2

X1

Y1

PITOT K1

1FN33E

1FN34NE

C Minor text changes. 6/19/13 GA

D Changed Effectivity note. 8/14/13 GA

E Changed SERVO TEST to SERVO TST. 10/20/17 GA


NR / NF

ref: WDM 63-41-00PP5

PITOT HEAT


3EU3E

PP5

7.5A

EFN-39

G12132-6-03P1

A A

J1

EFN-38

3A

HYDRAULICS

WARN PNL-1


PP15

EFN-37

3A

PP5

7.5A

EFN-36

G12132-6-074280 C


GA 12/05/12

CLB 12/05/12

GA107 1

5A

EFN-43

INST. LTS-1

5A

EFN-42

ref: WDM 80-11-04

ref: WDM 33-10-00

1KK46E Red v

P1

GOV A


v

PP5

G12132-6-05J1

PP5

EFN-41

3A

ref: WDM 31-41-00

1WW72E

P1

D

ASU1-3

G12132-6-04J1

D

PP5


G12132-6-02P1

EE EE

J1

1LK738E

G12301:1 DIMMER CONTROL(SEE G12132-23-074280)

G12132-23-01

At the installer's discretion, the entire PP15 bus, Including the WARN PNL-1 and RELEASE breaker functions may be moved to an installer defined location outside the console.


A Added Effectivity note. 2/04/13 GAB Changed Effectivity note. 8/14/13 GAC Changed EFN-43 rating. 4/22/15 GA


Installer Defined

ATTITUDE

RELEASE

ref: WDM 25-00-00

ref: WDM 34-25-30

Installer Defined

G12132-7-05f

P1

f

J1

G12132-7-04 AN16ga.

PP5

3A

EFN-49

N N

EFN-48

P2 J2

3A

STROBE LT


1EW116E

ref: WDM 31-61-00

EFN-46

G12132-7-03P1

s

J1

s

PP5VEMD-1

7.5A

PP9

EFN-45

7.5A

2.5A

G12132-7-074280 C


GA 12/05/12

CLB 12/05/12

GA107 1

G12132-7-01

EXT LOAD

1ME87E or Installer Defined

EFN-58

P1

w

J1

w

2.5A

PP9

EFN-57


G12132-7-08

G12132-7-06

ref: WDM 24-30-00

Detailed on G12132-2-074280IDL/FLT SEL PP9

E

P1

E

J1

WARN PNL-2 PP6

EFN-56

2.5A

ref: WDM 31-61-00VEMD-2

1EW119E

EFN-55

P1

K K

J1

7.5A

PP6

ref: WDM 25-63-10PP15

ref: WDM 25-91-00



A Added Effectivity note. 2/04/13 GA

B Changed Effectivity note. Changed EXT LOAD WDM Reference. Minor text changes. 8/14/13 GA

1WW31E1WW97E

Pre-MOD 074677Post-MOD 074677

C Wire connection option for WARN PNL-2 9/27/16 GA


ref: WDM 77-00-04

1KW56E G12132-8-03

EFN-61

2.5A

P1

r

J1

r

ref: WDM 28-00-00

ref: WDM 80-11-04

J1P1

G12132-8-02

G12132-8-01

FADEC TEST

1QW1E C

P1

PP6

C

J1

FUEL GAUGE

EFN-60

2.5A

1KW182E B

PP6

B

ENG CTL

7.5A

EFN-59

PP6

ref: WDM 77-30-00

G12132-8-074280 B


GA 12/05/12

CLB 12/05/12

GA107 1

EFN-65

7.5A

7.5A

EFN-66


1KW64E Red

P1

i


PP6

G12132-8-06J1

i

EFN-63

2.5A

7.5A

EFN-64

ref: WDM 80-11-04

1KK138E Red

EDR

P1

L

GOV B


G12132-8-05

PP6

J1

L

PP6

PP6


A Added Effectivity note. 2/04/13 GAB Changed Effectivity note. 8/14/13 GA


2.5A


Detailed on G12132-2-074280EM-NR IND

EM-IDL/FLT

1DT5E

EFN-72K

1A

EFN-71E

1A

EMER

EMER

H H

P1

EFN-70

J1G12132-9-02


1WW34E

ref: WDM 31-41-00

ref: WDM 31-31-00

J1P1

PP9HOUR METER

AA AAG12132-9-01

PP6

EFN-68

2.5A

ASU1-2

PP6FUEL PUMP

EFN-67

7.5A

PP6

G12132-9-074280 C


GA 12/05/12

CLB 12/05/12

GA107 1

PP6POSITION LTS

7.5A

EFN-87

ref: WDM 33-41-00

PP6ANTI-COL LT

7.5A

EFN-83

TAXI LIGHT

7.5A

EFN-79


G12132-9-031LE1E J

P1

J

J1

CABIN LTS

2.5A

EFN-76

PP6

1LJ3E d d

P1 J1G12132-9-04

CAM

EFN-75

PP5

2.5A

ref: WDM 33-12-00



1BG6E Red g

P2

g

J2G12132-9-05 AN16ga.



GAB Changed Effectivity note. Added CAM breaker. 8/14/13 GA

ref: WDM 25-10-40

C Changed PP46 to EMER. 12/05/14 GA


LANDING LT

ref: WDM 80-11-04

1KW4E

1MH20E and/or 1MH22E (if installed)

20A

EFN-95

G12132-10-03 AN16ga.

G12132-10-04 AN16ga.

EFN-94

PP9

P2

X

J2

X

PP9

10A

START

a

P2

a

J2

Detailed on G12132-5-074280W/S WIPER-1

SWING

PWR OUTLET


15A

EFN-93

10A

EFN-92

PP9

EFN-91

7.5A

G12132-10-01


G12132-10-074280 E


GA 12/05/12

CLB 12/05/12

GA107 1

EFN-N/A-4

TAXI CTL PP6

2.5A

a

LAND CTL

EFN-N/A-3

1FF239E or Installer Defined

PP6

2.5A

a


G12132-10-05 AN16ga.

ref: WDM 34-21-00

EFN-N/A-2

P1

GYRO

5A

J1

EFN-N/A-1

PP9

P2

b

EFN-97

b

J2

2.5A

HYD MAIN

1DH78F

ref: WDM 25-26-06

Installer Defined G12132-10-02 AN16ga.cc

P2 J2

ref: WDM 25-91-00 Source directly from wire 1MY41E, or through an available power terminal post. See G12132-11-074280.

61

61




1MH1E


G12132-10-06G G

P1 J1

ref: WDM 29-11-00

ref: WDM 24-22-00


GAB Minor text changes. 6/19/13 GA

C Changed Effectivity note. Renamed CARGO HOOK to SWING to match EC documentation. Changed GYRO to match EC documentation.

8/14/13 GA

62

63

62 63

ref: WDM 28-00-00

D Changed EFN-97 based on MOD level. 9/27/16 GA

MOD LABEL RATING WIRE #

Pre-MOD 074629 AC INVERTER 10A 1XU1E

Post-MOD 074629 FUEL LOW 3A 1QW86E

64 BUS

PP9

PP5

64

65 BUS

PP5

PP9

MOD

Pre-MOD 074629

Post-MOD 074629

65

Changed EFN-97 and EFN-N/A-2 bus assignments based on MOD level.

E 10/20/17 GA







RMSTR BUS BAR, Top Left


AN8ga G12132-11-13TB4To output of Radio Master relay

1PP9E

3PP23E

TB6

TB5AN8ga G12132-11-14

AN8ga G12132-11-04

AN8ga G12132-11-15

1PP6E

1PP5E

TB3

TB2

TB1 AN8ga G12132-11-01

AN8ga G12132-11-02

AN8ga G12132-11-03


G12132-11-074280 E


GA 12/05/12

CLB 12/05/12

GA107 1


G12135-10

G12135-12

G12135-8

G12135-2


G12135-10

G12135-8

G12135-9



AN10ga G12132-11-05SWING

10A

EFN-92

Detailed on G12132-10-0742801MY41E

EMER BUS BAR, Middle Right AftAN16ga G12132-2-21G12135-2

The PP46 bus has been rewired to contain the EM-IDL/FLT (EFN-72K) and EM-NR IND (EFN-71E) breakers ONLY. This new bus is designated EMER. Any other breakers previously assigned to the PP46 bus must be relocated to the PP50 bus or to an installer-defined bus.



GA

1

2

3

4

5

6

MS24659-23D

ESN-6

ref: G12132-2-074280

B Changed PP46 power source. 4/08/13 GA

MASTER CUTOFF

C Removed second PP46 Bus Bar. 6/19/13 GA

D Changed Effectivity note. Renamed CARGO HOOK to SWING to match EC documentation. 8/14/13 GA

E Changed PP46 to EMER bus. 12/05/14 GA

AIR

CR

AFT

FW

D




LEFT MIDDLE BUS BAR

Optional RMSTR BUS

?A

LTB-1

G12132-12-19

G12132-12-20

LTB-4

RMSTR BUS

RMSTR BUS

Optional

LTB-2

?A

LTB-3

?A

Optional

G12132-12-18

G12132-12-17

RMSTR BUS

RMSTR BUSLTB-5

?A

Optional

LTB-6

?A

Optional

G12132-12-16

G12132-12-15

G12132-12-14

Installer defined

Installer definedVU

VU

Installer defined

Installer definedT T

S S

Installer defined

Installer defined

Installer definedR R

Q

P

Q

P

RMSTR BUSOptional

G12132-12-09

RMSTR BUS

RMSTR BUS

?A

?A

LTB-7Optional

LTB-8

?A

Optional

G12132-12-12

G12132-12-13

G12132-12-10

G12132-12-11

RMSTR BUS

RMSTR BUS

?A

LTB-9Optional

?A

LTB-10Optional

G12132-12-07

G12132-12-08

G12132-12-05

G12132-12-06

RMSTR BUS

RMSTR BUS

?A

LTB-11

Optional

?A

LTB-12

Optional

G12132-12-04

G12132-12-03

G12132-12-01

G12132-12-02


Installer defined

Installer defined

Installer defined

Installer defined

Installer defined

L L

N

M

N

M

KJ

KJ

Installer defined

Installer defined

Installer defined

Installer definedHG

HG

FE

FE


Installer defined

Installer defined

Installer defined

Installer defined

CD

CD

AB

J3

AB

P3LEFT TOP BUS BAR

G12132-12-074280 C


GA 12/05/12

CLB 12/05/12

GA107 1

Installer definedG12132-12-30if installed.

Installer defined f f

G12132-12-29

G12132-12-28

G12132-12-27

G12132-12-26

?A

LMB-2

?A

LMB-3Optional PP15

LMB-5

LMB-4

Optional

Optional

Optional

PP15

PP15

?A

PP15

?A

e

d

Installer definede

Installer definedd

c

b

Installer definedc

Installer definedb


Installer definedG12132-12-21

PP15

G12132-12-25

G12132-12-24

G12132-12-23

G12132-12-22

LMB-8

LMB-7

LMB-6

?A

Optional

Optional

PP15

?A

PP15


LMB-9

?A

Optional

Optional

PP15

Y Y

a

Z

Installer defineda

Installer definedZ

X

W

Installer definedX

Installer defined

W

(p/n: G12135-12)

(p/n: G12135-10)

G12132-11-13RMSTR BUS

J3

PP15 BUS

P3

G12132-11-14AN8ga.


3PP23ETB5


ref: WDM 24-60-02ref: G12132-11-074280ref: G12132-16-074280

?A



GAB Removed PP46 bus. 6/19/13 GAC Changed Effectivity note. 8/14/13 GA

MS24524-21

ANTI-COL ALL / TAIL

G12132-4-074280, ESN

-93A, PP5, EFN

-38

NR

/NF

G12132-6-074280, 63-41-00

G12132-7-074280, 24-30-00

2.5A, PP6, EFN-68

G12132-5-074280, 28-00-00

WAR

N PN

L-2

FWD

G12132-13-074280 D

CONSOLE BREAKER LAYOUTP132 RIGHT SIDE VIEW

GA107 1

GA 12/05/12

GA 12/05/12

GA 12/05/12

CLB 12/05/12

7.5A, PP6, EFN-59

2.5A, PP6, EFN-60

FUEL G

AUG

EEN

G C

TL

G12132-8-074280, 80-11-04

G12132-4-074280, 33-43-02


G12132-3-074280, 80-11-04

7.5A, PP6, EFN-64

7.5A, PP6, EFN-83

ANTI-C

OL LT

G12132-4-074280, 33-42-00

START

G12132-10-074280, 80-11-04

TAXI CTL

2.5A, PP6, EFN-N

/A-4G

12132-9-074280, 33-41-007.5A, PP6, EFN

-87

POSITIO

N LTS

2.5A, PP9, EFN-57

G12132-8-074280, 77-30-00

IDL/FLT SEL

10A, PP9, EFN-94

G12132-2-074280, 80-11-04

G12132-8-074280, 80-11-04

7.5A, PP6, EFN-65

EDR

GO

V B

2.5A, PP6, EFN-76

CABIN

LTS

7.5A, PP6, EFN-79

TAXI LIGH

T

G12132-4-074280, 33-43-02

G12132-9-074280, 33-12-00

G12132-4-074280, 33-43-01

LAND

CTL

2.5A, PP6, EFN-N

/A-3G

12132-9-074280, 31-41-00

ASU1-2

G12132-8-074280, 28-00-00

2.5A, PP6, EFN-61

G12132-8-074280, 77-00-04

FADEC

TEST

2.5A, PP6, EFN-63

CR

ANK

SPARE

G12132-5-074280, ESN

-17

1A, EMER

, EFN-71E

EM-ID

L/FLT

G12132-2-074280, 80-11-04

EM-N

R IN

D

G12132-2-074280, 63-41-00

G12132-5-074280, ESN

-18

SPARE

MS24524-23

SPARE

G12132-5-074280, ESN

-10

SPARE

G12132-5-074280, ESN

-15

SPARE

G12132-5-074280, ESN

-14

MS24524-23

MS24524-23

G12132-6-074280, 33-10-00

INST. LTS-1

G12132-10-074280, 34-21-00

GYR

O

ATTITUD

E

G12132-7-074280, 34-25-30

1A, EMER

, EFN-72K

3A, PP5, EFN-49

G12132-7-074280, 31-61-00

5A, PP5, EFN-N

/A-2VEM

D-1

7.5A, PP5, EFN-46

3A, PP5, EFN-41

7.5A, PP5, EFN-39

PITOT H

EAT

G12132-5-074280, 30-31-00

5A, PP5, EFN-42

GO

V AG

12132-6-074280, 80-11-04

ASU1-3

G12132-6-074280, 31-41-00

MS24524-23

MS24524-23

7.5A, PP6, EFN-55

VEMD

-2

G12132-7-074280, 31-61-00

2.5A, PP6, EFN-56

7.5A, PP6, EFN-66

G12132-5-074280, 71-61-10

7.5A, PP6, EFN-67

FUEL PU

MP

SAND

FILTERH

YDR

AULIC

S

G12132-3-074280, 29-11-00

CAM

G12132-9-074280, 25-10-40

7.5A, PP5, EFN-36

2.5A, PP5, EFN-75

MS24524-23

WAR

NIN

G H

OR

N

G12132-3-074280, ESN

-12

5A, PP5, EFN-43



B Changed Effectivity note. Added CAM breaker. Updated GYRO to match WDM. 8/14/13 GA

C Changed PP46 to EMER. 12/05/14 GAD Changed EFN-43 rating. 4/22/15 GA

G12132-13-074280-P122 C


GA107 1

GA 02/04/13

GA 02/04/13

GA 02/04/13

CLB 02/04/13

Effectivity: AS350B3 embodyingMod 350A07-4280

G12132-4-074280

G12132-9-074280

33-43-02

33-41-00

7.5A, PP6, EFN-87

POSITION LTS

TAXI CTL2.5A, PP6, EFN-N/A-4

G12132-8-07428077-30-00

G12132-3-074280

G12132-8-074280

2.5A, PP6, EFN-63


CRANK


80-11-04

80-11-04

G12132-9-074280

G12132-4-074280

G12132-4-074280

33-42-00

33-43-02

33-12-00



G12132-4-074280

G12132-9-074280

33-43-01

31-41-00

ASU1-22.5A, PP6, EFN-68

LAND CTL2.5A, PP6, EFN-N/A-3

2.5A, PP6, EFN-76

CABIN LTSG12132-8-074280

G12132-8-074280

G12132-8-074280

2.5A, PP6, EFN-60

FUEL GAUGE


77-00-04

28-00-00

80-11-04

G12132-7-074280

G12132-7-074280

2.5A, PP6, EFN-56


WARN PNL-2


24-30-00

31-61-00

G12132-5-074280

G12132-5-074280

28-00-00

71-61-10



G12132-2-074280



63-41-00

80-11-04

FWD

G12132-7-074280

5A, PP5, EFN-N/A-2

3A, PP5, EFN-49

G12132-7-07428034-25-30

ATTITUDE

G12132-10-07428034-21-00

31-61-00

GYRO

INST. LTS-1

5A, PP5, EFN-42

7.5A, PP5, EFN-46

G12132-6-07428033-10-00

VEMD-1

G12132-6-07428080-11-04

5A, PP5, EFN-43

GOV A

G12132-6-074280

7.5A, PP5, EFN-39

3A, PP5, EFN-41

PITOT HEAT

G12132-6-07428031-41-00

ASU1-3

G12132-5-07428030-31-00

63-41-00

7.5A, PP5, EFN-36

2.5A, PP5, EFN-75

3A, PP5, EFN-38

CAM

HYDRAULICS

G12132-9-074280

NR/NF

G12132-3-07428029-11-00

G12132-10-074280


80-11-04

10A, PP9, EFN-94

START

G12132-2-07428080-11-04


25-10-40

A Added CAM breaker. 8/14/13 GAB Changed PP46 to EMER. 12/05/14 GAC 4/22/15 GA Changed EFN-43 rating.

MS24524-21

ANTI-COL ALL / TAIL

G12132-4-074280, ESN

-93A, PP5, EFN

-38

NR

/NF

G12132-6-074280, 63-41-00

G12132-7-074280, 24-30-00

2.5A, PP6, EFN-68

G12132-5-074280, 28-00-00

WAR

N PN

L-2

FWD

G12132-13-074629 --


GA107 1

GA 10/20/17

GA 10/20/17

GA 10/20/17

GA 10/20/17

7.5A, PP6, EFN-59

2.5A, PP6, EFN-60

FUEL G

AUG

EEN

G C

TL

G12132-8-074280, 80-11-04

G12132-4-074280, 33-43-02


G12132-3-074280, 80-11-04

7.5A, PP6, EFN-64

7.5A, PP6, EFN-83

ANTI-C

OL LT

G12132-4-074280, 33-42-00

START

G12132-10-074280, 80-11-04

TAXI CTL

2.5A, PP6, EFN-N

/A-4G

12132-9-074280, 33-41-007.5A, PP6, EFN

-87

POSITIO

N LTS

2.5A, PP9, EFN-57

G12132-8-074280, 77-30-00

IDL/FLT SEL

10A, PP9, EFN-94

G12132-2-074280, 80-11-04

G12132-8-074280, 80-11-04

7.5A, PP6, EFN-65

EDR

GO

V B

2.5A, PP6, EFN-76

CABIN

LTS

7.5A, PP6, EFN-79

TAXI LIGH

T

G12132-4-074280, 33-43-02

G12132-9-074280, 33-12-00

G12132-4-074280, 33-43-01

LAND

CTL

2.5A, PP6, EFN-N

/A-3G

12132-9-074280, 31-41-00

ASU1-2

G12132-8-074280, 28-00-00

2.5A, PP6, EFN-61

G12132-8-074280, 77-00-04

FADEC

TEST

2.5A, PP6, EFN-63

CR

ANK

SPARE

G12132-5-074280, ESN

-17

1A, EMER

, EFN-71E

EM-ID

L/FLT

G12132-2-074280, 80-11-04

EM-N

R IN

D

G12132-2-074280, 63-41-00

G12132-5-074280, ESN

-18

SPARE

MS24524-23

SPARE

G12132-5-074280, ESN

-10

SPARE

G12132-5-074280, ESN

-15

SPARE

G12132-5-074280, ESN

-14

MS24524-23

MS24524-23

G12132-6-074280, 33-10-00

INST. LTS-1

G12132-10-074280, 28-00-00

FUEL LO

W

ATTITUD

E

G12132-7-074280, 34-25-30

1A, EMER

, EFN-72K

3A, PP5, EFN-49

G12132-7-074280, 31-61-00

3A, PP5, EFN-97

VEMD

-17.5A, PP5, EFN

-46

3A, PP5, EFN-41

7.5A, PP5, EFN-39

PITOT H

EAT

G12132-5-074280, 30-31-00

5A, PP5, EFN-42

GO

V AG

12132-6-074280, 80-11-04

ASU1-3

G12132-6-074280, 31-41-00

MS24524-23

MS24524-23

7.5A, PP6, EFN-55

VEMD

-2

G12132-7-074280, 31-61-00

2.5A, PP6, EFN-56

7.5A, PP6, EFN-66

G12132-5-074280, 71-61-10

7.5A, PP6, EFN-67

FUEL PU

MP

SAND

FILTERH

YDR

AULIC

S

G12132-3-074280, 29-11-00

CAM

G12132-9-074280, 25-10-40

7.5A, PP5, EFN-36

2.5A, PP5, EFN-75

MS24524-23

WAR

NIN

G H

OR

N

G12132-3-074280, ESN

-12

5A, PP5, EFN-43


G12132-13-074629-P122 --


GA107 1

GA 10/20/17

GA 10/20/17

GA 10/20/17

GA 10/20/17


G12132-4-074280

G12132-9-074280

33-43-02

33-41-00

7.5A, PP6, EFN-87

POSITION LTS


G12132-8-07428077-30-00

G12132-3-074280

G12132-8-074280

2.5A, PP6, EFN-63


CRANK


80-11-04

80-11-04

G12132-9-074280

G12132-4-074280

G12132-4-074280

33-42-00

33-43-02

33-12-00



G12132-4-074280

G12132-9-074280

33-43-01

31-41-00

ASU1-22.5A, PP6, EFN-68


2.5A, PP6, EFN-76

CABIN LTSG12132-8-074280

G12132-8-074280

G12132-8-074280

2.5A, PP6, EFN-60

FUEL GAUGE


77-00-04

28-00-00

80-11-04

G12132-7-074280

G12132-7-074280

2.5A, PP6, EFN-56


WARN PNL-2


24-30-00

31-61-00

G12132-5-074280

G12132-5-074280

28-00-00

71-61-10



G12132-2-074280



63-41-00

80-11-04

FWD

G12132-7-074280

3A, PP5 EFN-97

3A, PP5, EFN-49

G12132-7-07428034-25-30

ATTITUDE

G12132-10-07428028-00-00

31-61-00

FUEL LOW

INST. LTS-1

5A, PP5, EFN-42

7.5A, PP5, EFN-46

G12132-6-07428033-10-00

VEMD-1

G12132-6-07428080-11-04

5A, PP5, EFN-43

GOV A

G12132-6-074280

7.5A, PP5, EFN-39

3A, PP5, EFN-41

PITOT HEAT

G12132-6-07428031-41-00

ASU1-3

G12132-5-07428030-31-00

63-41-00

7.5A, PP5, EFN-36

2.5A, PP5, EFN-75

3A, PP5, EFN-38

CAM

HYDRAULICS

G12132-9-074280

NR/NF

G12132-3-07428029-11-00

G12132-10-074280


80-11-04

10A, PP9, EFN-94

START

G12132-2-07428080-11-04


25-10-40

G12132-14-074280 D

CONSOLE BREAKER LAYOUTP132 LEFT SIDE VIEW

GA107 1

GA 12/05/12

GA 12/05/12

GA 12/05/12

CLB 12/05/12

3A, P

P15,

EFN

-37

WAR

N P

NL-

1G

1213

2-3-

0742

80, 2

6-11

-10

?A, P

P15,

LM

B-7

?A, P

P15,

LM

B-8

15A,

PP9

, EFN

-93

W/S

WIP

ER-1

PWR

OU

TLET

FWD

7.5A

, PP9

, EFN

-91

HYD

MAI

N


EXT

LOAD

2.5A

, PP9

, EFN

-58

LAN

DIN

G L

T

20A,

PP9

, EFN

-95

STR

OBE

LT

7.5A

, PP9

, EFN

-45

AC IN

VER

TER

15A,

PP9

, EFN

-97

?A, P

P15,

LM

B-6

2.5A

, PP9

, EFN

-N/A

-1

HO

UR

MET

ER

2.5A

, PP9

, EFN

-70

?A, P

P15,

LM

B-5

??, R

MST

R b

us, L

TB-1

1

??, R

MST

R b

us, L

TB-1

2

MS2

4659

-23D

BAT-

EXT

PWR

SAN

D F

ILTE

R

MS2

4524

-23

W/S

WIP

ER

??, R

MST

R b

us, L

TB-7

??, R

MST

R b

us, L

TB-8

??, R

MST

R b

us, L

TB-1

0

??, R

MST

R b

us, L

TB-9

??, R

MST

R b

us, L

TB-6

??, R

MST

R b

us, L

TB-5

??, R

MST

R b

us, L

TB-3

??, R

MST

R b

us, L

TB-4

FUEL

PU

MP

MS2

4523

-23

MS2

4523

-26

SER

VO T

ST

MS2

4523

-23

??, R

MST

R b

us, L

TB-2

??, R

MST

R b

us, L

TB-1

DIR

ECT

BATT

MS2

4524

-23

AV M

ASTE

R

MS2

4524

-23

Opt

iona

lG

1213

2-12

-074

280

Opt

iona

lG

1213

2-12

-074

280

Opt

iona

lG

1213

2-12

-074

280

Opt

iona

lG

1213

2-12

-074

280

Opt

iona

lG

1213

2-12

-074

280

Opt

iona

lG

1213

2-12

-074

280

Opt

iona

lG

1213

2-12

-074

280

Opt

iona

lG

1213

2-12

-074

280

Opt

iona

lG

1213

2-12

-074

280

Opt

iona

lG

1213

2-12

-074

280

Opt

iona

lG

1213

2-12

-074

280

Opt

iona

lG

1213

2-12

-074

280

Opt

iona

lG

1213

2-12

-074

280

Opt

iona

lG

1213

2-12

-074

280

Opt

iona

lG

1213

2-12

-074

280

Opt

iona

lG

1213

2-12

-074

280

G12

132-

5-07

4280

, 30-

42-0

0G

1213

2-10

-074

280,

24-

60-0

1

G12

132-

4-07

4280

, 33-

41-0

0

G12

132-

4-07

4280

, 33-

43-0

1G

1213

2-10

-074

280,

24-

22-0

0

G12

132-

7-07

4280

, 25-

91-0

0

G12

132-

9-07

4280

, 31-

31-0

0G

1213

2-10

-074

280,

29-

11-0

0

G12

132-

5-07

4280

, OP-

1

G12

132-

2-07

4280

, OP-

2

G12

132-

5-07

4280

, ESN

-21

G12

132-

5-07

4280

, ESN

-24

G12

132-

5-07

4280

, OP-

3

G12

132-

5-07

4280

, ESN

-2

G12

132-

2-07

4280

, ESN

-1


REL

EASE

3A, P

P15,

EFN

-48

G12

132-

7-07

4280

, 25-

00-0

0

10A,

OP1

bus

, EFN

-92

G12

132-

10-0

7428

0, 2

5-91

-00

SWIN

G

?A, P

P15,

LM

B-9

Opt

iona

lG

1213

2-12

-074

280

?A, P

P15,

LM

B-4

Opt

iona

lG

1213

2-12

-074

280

?A, P

P15,

LM

B-2

Opt

iona

lG

1213

2-12

-074

280


?A, P

P15,

LM

B-3

Opt

iona

lG

1213

2-12

-074

280

B Removed PP46 bus. Changed OP-2 switch type. 6/19/13 GA

C Changed Effectivity note. Renamed CARGO HOOK to SWING to match EC documentation. 8/14/13 GA

D Changed SERVO TEST to SERVO TST. 10/20/17 GA

SWING

PWR OUTLET

10A, OP1, EFN-92

15A, PP9, EFN-93

W/S WIPER-17.5A, PP9, EFN-91

STROBE LT

AC INVERTER

20A, PP9, EFN-95

LANDING LT

15A, PP9, EFN-97

EXT. LOAD

G12132-10-074280

2.5A, PP9, EFN-58

HOUR METER


HYD MAIN

G12132-7-074280

G12132-10-074280

G12132-4-074280

G12132-10-074280

G12132-10-074280

G12132-5-07428030-42-00

25-91-00

24-60-01

33-43-01

24-22-00

25-91-00

FWD Effectivity: AS350B3 embodyingMod 350A07-4280

2.5A, PP9, EFN-70

G12132-9-07428031-31-00

7.5A, PP9, EFN-45

G12132-4-07428033-41-00

G12132-14-074280-P122 A


GA107 1

GA 02/04/13

GA 02/04/13

GA 02/04/13

CLB 02/04/13

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-7-073273RELEASE

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

?A, RMSTR, LTB-12 3A, PP15, EFN-37

?A, PP15, LMB-9?A, RMSTR, LTB-11

?A, RMSTR, LTB-10 ?A, PP15, LMB-8





?A, RMSTR, LTB-5

3A, PP15, EFN-48

?A, RMSTR, LTB-4

?A, RMSTR, LTB-3

?A, RMSTR, LTB-2

?A, RMSTR, LTB-1

G12132-3-07428026-11-10

WARN PNL-1

29-11-00


A Removed PP46 bus. Renamed CARGO HOOK to SWING to match EC documentation. 8/14/13 GA

G12132-12-073273Optional

?A, PP15, LMB-3

G12132-12-073273Optional

?A, PP15, LMB-2

25-00-00

G12132-14-074629 A


GA107 1

GA 9/27/16

GA 9/27/16

GA 9/27/16

SJC 9/27/16

3A, P

P15,

EFN

-37

WAR

N P

NL-

1G

1213

2-3-

0742

80, 2

6-11

-10

?A, P

P15,

LM

B-7

?A, P

P15,

LM

B-8

15A,

PP9

, EFN

-93

W/S

WIP

ER-1

PWR

OU

TLET

FWD

7.5A

, PP9

, EFN

-91

HYD

MAI

N


EXT

LOAD

2.5A

, PP9

, EFN

-58

LAN

DIN

G L

T

20A,

PP9

, EFN

-95

STR

OBE

LT

7.5A

, PP9

, EFN

-45

GYR

O

5A, P

P9, E

FN-N

/A-2

?A, P

P15,

LM

B-6

2.5A

, PP9

, EFN

-N/A

-1

HO

UR

MET

ER

2.5A

, PP9

, EFN

-70

?A, P

P15,

LM

B-5

??, R

MST

R b

us, L

TB-1

1

??, R

MST

R b

us, L

TB-1

2

MS2

4659

-23D

BAT-

EXT

PWR

SAN

D F

ILTE

R

MS2

4524

-23

W/S

WIP

ER

??, R

MST

R b

us, L

TB-7

??, R

MST

R b

us, L

TB-8

??, R

MST

R b

us, L

TB-1

0

??, R

MST

R b

us, L

TB-9

??, R

MST

R b

us, L

TB-6

??, R

MST

R b

us, L

TB-5

??, R

MST

R b

us, L

TB-3

??, R

MST

R b

us, L

TB-4

FUEL

PU

MP

MS2

4523

-23

MS2

4523

-26

SER

VO T

ST

MS2

4523

-23

??, R

MST

R b

us, L

TB-2

??, R

MST

R b

us, L

TB-1

DIR

ECT

BATT

MS2

4524

-23

AV M

ASTE

R

MS2

4524

-23

Opt

iona

lG

1213

2-12

-074

280

Opt

iona

lG

1213

2-12

-074

280

Opt

iona

lG

1213

2-12

-074

280

Opt

iona

lG

1213

2-12

-074

280

Opt

iona

lG

1213

2-12

-074

280

Opt

iona

lG

1213

2-12

-074

280

Opt

iona

lG

1213

2-12

-074

280

Opt

iona

lG

1213

2-12

-074

280

Opt

iona

lG

1213

2-12

-074

280

Opt

iona

lG

1213

2-12

-074

280

Opt

iona

lG

1213

2-12

-074

280

Opt

iona

lG

1213

2-12

-074

280

Opt

iona

lG

1213

2-12

-074

280

Opt

iona

lG

1213

2-12

-074

280

Opt

iona

lG

1213

2-12

-074

280

Opt

iona

lG

1213

2-12

-074

280

G12

132-

5-07

4280

, 30-

42-0

0G

1213

2-10

-074

280,

24-

60-0

1

G12

132-

4-07

4280

, 33-

41-0

0

G12

132-

4-07

4280

, 33-

43-0

1G

1213

2-10

-074

280,

34-

21-0

0

G12

132-

7-07

4280

, 25-

91-0

0

G12

132-

9-07

4280

, 31-

31-0

0G

1213

2-10

-074

280,

29-

11-0

0

G12

132-

5-07

4280

, OP-

1

G12

132-

2-07

4280

, OP-

2

G12

132-

5-07

4280

, ESN

-21

G12

132-

5-07

4280

, ESN

-24

G12

132-

5-07

4280

, OP-

3

G12

132-

5-07

4280

, ESN

-2

G12

132-

2-07

4280

, ESN

-1


REL

EASE

3A, P

P15,

EFN

-48

G12

132-

7-07

4280

, 25-

00-0

0

10A,

OP1

bus

, EFN

-92

G12

132-

10-0

7428

0, 2

5-91

-00

SWIN

G

?A, P

P15,

LM

B-9

Opt

iona

lG

1213

2-12

-074

280

?A, P

P15,

LM

B-4

Opt

iona

lG

1213

2-12

-074

280

?A, P

P15,

LM

B-2

Opt

iona

lG

1213

2-12

-074

280

?A, P

P15,

LM

B-3

Opt

iona

lG

1213

2-12

-074

280

A Changed SERVO TEST to SERVO TST. 10/20/17 GA Swapped EFN-97 and EFN-N/A-2

SWING

PWR OUTLET

10A, OP1, EFN-92

15A, PP9, EFN-93


STROBE LT

GYRO

20A, PP9, EFN-95

LANDING LT

5A, PP9, EFN-N/A-2

EXT. LOAD

G12132-10-074280

2.5A, PP9, EFN-58

HOUR METER


HYD MAIN

G12132-7-074280

G12132-10-074280

G12132-4-074280

G12132-10-074280

G12132-10-074280

G12132-5-07428030-42-00

25-91-00

24-60-01

33-43-01

34-21-00

25-91-00

FWD Effectivity: AS350B3 embodyingMod 350A07-4629

2.5A, PP9, EFN-70

G12132-9-07428031-31-00

7.5A, PP9, EFN-45

G12132-4-07428033-41-00

G12132-14-074629-P122 A


GA107 1

GA 09/27/16

GA 09/27/16

GA 09/27/16

SJC 09/27/16

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-7-073273RELEASE

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional








?A, RMSTR, LTB-5

3A, PP15, EFN-48

?A, RMSTR, LTB-4

?A, RMSTR, LTB-3

?A, RMSTR, LTB-2

?A, RMSTR, LTB-1

G12132-3-07428026-11-10

WARN PNL-1

29-11-00


G12132-12-073273Optional

?A, PP15, LMB-3

G12132-12-073273Optional

?A, PP15, LMB-2

25-00-00

A Swapped EFN-97 and EFN-N/A-2 10/20/17 GA

G12132-15-074280 E


GA107 1

GA 12/05/12

GA 12/05/12

GA 12/05/12

CLB 12/05/12

WIPER

G12132-5-074280, ESN-21

G12132-5-074280, ESN-24

DIRECT BATT

SAND FILTER

G12132-5-074280, OP-1

G12132-2-074280, OP-2

MS24524-23

MS24524-23

AV MASTERMASTER

AVIONICS

BATTERY

MS24524-23

MS24523-23

W/S WIPER

SANDFILTER


G12132-5-074280, ESN-2

G12132-2-074280, ESN-1BAT-EXT PWR

FUEL PUMP

G12132-5-074280, OP-3

WINDSHIELD

MS24659-23D

MS24523-23 PUMPFUEL

POWERBAT-EXT

G12

132-

5-07

4280

, ES

N-1

3

G12

132-

2-07

4280

, ES

N-6

G12

132-

3-07

4280

, ES

N-5

G12

132-

3-07

4280

, ES

N-7

G12

132-

3-07

4280

, ES

N-1

1

G12

132-

3-07

4280

, ES

N-3

PIT

OT

HE

AT

MS2

4659

-23D

MS2

4523

-23

MAS

TER

CU

TOFF

MS2

4523

-26

MS2

7407

-3

WAR

N/F

IRE

TST

CR

AN

K E

NG

INE

MS2

4658

-26F

MS2

4524

-31

GE

N O

N /

RE

SE

T

AC

CU

TS

T

TSTWARN/FIRE

ON/RESETGENERATOR

TSTACCU

CUTOFFMASTER

ENGINECRANK PITOT

HEAT

SPARE

G12132-5-074280, ESN-18

G12132-5-074280, ESN-17

G12132-5-074280, ESN-10

G12132-5-074280, ESN-15SPARE

SPARE

SPARE

SPARESPARE

SPARE

MS24524-23

MS24524-23

SPARE MS24524-23

MS24524-23

G12132-5-074280, ESN-14

G12132-4-074280, ESN-9

G12132-3-074280, ESN-12

SPARE

ANTI-COL ALL / TAIL

WARNING HORN

SPARE MS24524-23

ALL / TAILANTI-COL

WARNINGHORN

MS24524-21

MS24524-23

SERVO TST

SERVOTSTMS24523-26


DIRECT

A Changed HYD TEST switch type. Changed ESN-7 switch type. Added Effectivity note.

2/04/13 GA

B Changed OP-2 switch type. 6/19/13 GA

C Changed Effectivity note. Changed WARN/FIRE TEST switch decal. 8/14/13 GA

D Changed EFN-11 switch type. 9/27/16 GA

Note: ACCU TST switch may be marked HYD TST

E Added ACCU TST Option. Changed TEST to TST. 10/20/17 GA

G12132-3-074280ESN-5, MS24523-26

P122 CONSOLE LAYOUT

G12132-5-074280

G12132-4-074280ESN-17, MS24524-23

ESN-13, MS24523-23

ESN-15, MS24524-23G12132-4-074280

G12132-5-074280OP-1, MS24524-23

G12132-4-074280

AVIONICSMASTER

ESN-14, MS24524-23


ESN-10, MS24524-23G12132-4-074280 G12132-4-074280

ESN-9, MS24524-21

PANELDIMMER

SERVOTST

GENERATORON / RESET

G12132-3-074280ESN-3, MS24524-31

SPARE

G12132-5-074280OP-3, MS24523-26

G12132-5-074280

SPARE

ESN-2, MS24523-23

FUELPUMP

ESN-1, MS24659-23DG12132-2-074280

BAT-EXTPOWER

G12132-3-074280ESN-11, MS24658-26F

ESN-21, MS24524-23G12132-5-074280

SPARE

SANDFILTER

ANTI-COLALL / TAIL

ESN-24, MS24523-23G12132-5-074280

WINDSHIELDWIPER

G12132-3-074280ESN-7, MS27407-3

ACCUTST

WARN / FIRETST

DIRECT BATTERY

ESN-18, MS24524-23G12132-4-074280

OP-2, MS24524-23G12132-2-074280

WARNINGHORN

G12132-2-074280ESN-6, MS24659-23D

SPARE

ESN-12, MS24524-23G12132-3-074280

SPARE

PITOTHEAT

MASTERCUTOFF

CRANKENGINE

G12132-15-074280-P122 D


GA107 1

GA 02/04/13

GA 02/04/13

GA 02/04/13

CLB 02/04/13


A Changed DIRECT BATTERY switch type. 8/14/13 GA

B Changed ESN-11 switch type. 9/27/16 GA

Note: ACCU TST switch may be marked HYD TST

C Added ACCU TST Option. Changed TEST to TST. 10/20/17 GA

D Changed ESN-11 switch image to locking switch. 11/08/17 GA

FROM G12132-5-074280

AN16ga

G12132-5-12

G12132-5-13


G12132-5-10

AVIONICS-2 BUS

AVIONICS-1 BUS

RELAYAVIONICS

EXTERNAL TO CONSOLE

PP128 ga.50A

AVIONICSA1

(Airframe GND)

X2

W

V

W

V

(no connection)


(no connection)

8 ga.

A2

X1

TB4

T

U

P2

T

U

J2

AN16ga



ALT. ENCODER

2.5A

TRANSPONDER

2.5A

2.5A

AUDIO PANEL

COM2

10A

GPS

5A

CD CHANGER

2.5A

COM1

10A

STEREO ICS

2.5A

G12132-10-05

existing label: SPARE

EFN-N/A-7


G12132-16-074280 B


GA 12/05/12

CLB 12/05/12

GA107 1

AN16ga

AN16ga

AVIONICS MASTER

1

2

3

4

5

6

MS24524-23

G12132-5-11

OP-1 AN16ga

45

G12132-16-04b b


45 15A

P2 J2


FROM G12132-5-074280

FROM G12132-10-074280

AN16ga

PP9

G12132-7-04

AN16ga

G12132-5-13

G12132-5-12

G12132-5-10


EFN-48

NNAN16ga

G12132-16-02 AN16ga

G12132-16-01 AN16gaW

V

W

V

T

U

P2

T

U

J2


45

G12132-16-03P2 J2

15A

FROM G12132-7-074280

1

2

3

4

5

6

MS24524-23

G12132-5-11

AN16ga

AN16ga

AVIONICS MASTEROP-1

AN16ga


AN16ga

PP15




Effectivity: AS350B2 and AS350B3 embodying Mod 350A07-4280

B Changed Effectivity note. 8/14/13 GAGA

1ME3E

Sample CARGO SWING circuit

N N

From G12132-7-074280

G12132-17-01


ref: WDM 25-00-00

J2P2

EFN-48

RELEASE

3A

G12132-7-04 AN 16ga.

PP15

G12132-17-074280 B

CARGO SWING SAMPLE CIRCUITP132 and P122 CONSOLE WIRING

GA 12/05/12

CLB 12/05/12

GA107 1

SLING ON warning light.Installer shall provide suitable light and install in clear view of pilot, with appropriate label.

MS24524-23



(Installer Defined)SLING

G12132-17-04

G12132-17-05

46

ref: WDM 25-00-00

28


28

There is no standard switch assigned to the swing function in the -074280 version of the console. If a swing circuit is required, implement it using an available optional switch, or using a switch mounted in an installer-defined location outside the console. The wire numbers shown are only an example. If an internal switch is used, the wire numbers should be updated to match the internal console wiring for that switch. If an external switch is used, the installer may use these numbers, or assign unique wire numbers as appropriate.

46

**

P*

**

J*


Effectivity: AS350B2 and AS350B3 embodying Mod 350A07-4280

ref: WDM 25-91-00

1

2

3

4

5

6

1MW4E

1MW5E

G12132-17-02

G12132-17-03**

**1MW8NE

1MW7E


B

Changed from CARGO HOOK to SWING to match EC documents. Fixed WDM references. Indicator now uses instrument panel dimmer. Added Effectivity for B2.

8/14/13 GA

GA

Effectivity: AS350B2 and AS350B3 embodying mod 350A07-4280



23

24 Installer

HOIST23

G12132-18-07

CAPACITYInstaller

450lb300lb 2.5A

7.5ARATING24


From G12132-7-074280

ref: WDM 25-63-10ref: WDM 25-63-11

J2

N

P2

N

EFN-48

2.5A

G12132-7-04

RELEASE PP5

G12132-18-06

G12132-18-074280 --


GA 8/14/13

CLB 8/14/13

GA107 1


G12132-18-03

G12132-18-04300lb UNIT: 1ME305E 450lb UNIT: 1ME285E

1ME36E


From G12132-5


G12132-18-05

G12132-18-01

1

2

3

4

5

6

MS24524-23

HOIST

**

***

*

P*

*

J*

*

(Installer Defined)48

ref: WDM 25-00-00ref: WDM 25-63-11

30


30

There is no standard switch assigned to the HOIST function in the -074280 version of the console. If a HOIST circuit is required, implement it using an available optional switch, or using a switch mounted in an installer-defined location outside the console. The wire numbers shown are only an example. If an internal switch is used, the wire numbers should be updated to match the internal console wiring for that switch. If an external switch is used, the installer may use these numbers, or assign unique wire numbers as appropriate.

48

Defined

DefinedSource

P* J*

* *


ref: WDM 25-63-10

ref: WDM 25-00-00

300lb UNIT: 1ME303E 450lb UNIT: 1ME284E

300lb UNIT: 1ME306NE 450lb UNIT: 1ME286NE

300lb UNIT: 1MW31E 450lb UNIT: 1MW12E

300lb UNIT: 1MW32E 450lb UNIT: 1MW13E

G12132-23-08 AN22ga

G12132-23-12 AN22ga

G12132-23-01

G12132-23-02

G12132-24-02 AN22ga

G12132-24-01 AN22ga

G12132-23-06 AN22ga

G12132-23-07 AN22ga

G12132-23-10 AN22ga

G12132-23-11 AN22ga

3

ref: G12132-3-074280

ESN-7WARN/FIRE TEST


4

5

6

PWR 1

PWR 2

1

2

1

G12132-23-092

3

DIMMER CONTROL

PWR OVERLAY

PWR POT

GND

G12301

4

5

1

G12132-23-074280 D

SWITCH LEGEND LIGHTINGP132 and P122 CONSOLE WIRING

RBH 12/05/12

CLB 12/05/12

GA107 1


WIRING

100 OHM



OVERLAY-RIGHT-

OVERLAY-TOP-

OVERLAY-LEFT-

M

M

M

G12132-24DIMMER POT ASSEMBLY

3

2

OVERLAY-RIGHT+

OVERLAY-TOP+

OVERLAY-LEFT+

F

F

F


5A

EFN-43

INST. LTS-1 PP5

ref: G12132-6-074280

CONSOLE LTS powerSS

P2 J2

1.5A Maximum Current

ref: G12132-37-074280

from PP50 BUS



B Changed Effectivity note. 8/14/13GAGA

C Changed Quick Diconnect Part Numbers. 12/05/14 CLBD Changed EFN-43 rating. 4/22/15 CLB

www.genevaaviation.com G12132-37-074280 C

07-4280 CONSOLE LIGHTEXTERNAL WIRING

GA 12/05/12

CLB 12/05/12

GA107 1


INST LTS 2 PP50

5A

SS

P2 J2G12132-23-02

Installer Defined AN 20ga.

3LK296E20

R2

243L RELAYU/CP FLOOR

CONSOLE BACKLIGHT POWER FROM PP50 BUS

For aircraft that embody mod 360A07-4280, the console backlight power supply pin J2:S must be connected to the PP50 bus through a circuit breaker of an appropriate current rating, 1.5A or greater.

Power may be supplied from the INST LTS. 2 breaker in the 50alpha breaker box in the R/H Baggage compartment via the 3LK296E wire at the 243L relay.

A diode must be placed between the INST LTS 2 breaker and the 234L relay to prevent voltage feedback from the lighting module.

It is the installers responsibility to confirm the total current draw from both the instrument panel and console lights does not exceed the current rating of both the circuits and breaker.

The installer must label the added wiring with unique identifying marks and update the wiring diagrams to reflect the changes made.

GENEVA ELECTRICALCONSOLE

50 ALPHA BREAKER PANELR/H BAGGAGE COMPARTMENT

ref: G12132-23-074280

ref: WDM 33-10-00



B Changed Effectivity note. 8/14/13GAGA

D6:A D6:CY

P3

G12132-23-02

ref: G12132-23-074280

INST LTS 2 PP50

5A

LMB-8Y

J3

3LK296E


G12132-12-31 G12132-12-23

PP50 BUS INSIDE CONSOLE

PP50 BUS OUTSIDE CONSOLE

Install Diode inside 50ALP.Minimum current rating 6A.

Minimum Reverse Voltage 50Vref: Diodes Incorporated p/n: 6A10-T

5

P1B

C Added diode to 3LK296E. 4/22/15 GA

DIRECT BATTERY

1

2

3

4

5

6

MS24659-23D

MASTER CUTOFF


ref: WDM 24-30-00

P1 J1

ESN-6

3PE53E


1PG6NE

1PG1NE

1PG2NE

1PG3NE

zz

X

Y Y

X

W

S

R R

S

W

G12132-2-13

G12132-2-10

G12132-2-09

G12132-2-06

G12132-2-05

G12132-2-02

1

2

3

4

5

6

MS24659-23D

BAT-EXT PWR

G12132-2-07

ESN-1

MS24524-23

G12132-2-11 T TJ1 P1


NOTICE:The circuitry related to the BAT-EXT PWR switch and the MASTER ELECTRICAL CUTOFF switch has been changed from the Eurocopter original circuitry. Install using this wiring, and use this drawing for future electrical troubleshooting.

OP-2

G12132-2-074280B2 A


GA 8/15/13

CLB 8/15/13


ref: WDM 24-60-02

3PE40E F F G12132-2-04

D1:A

G12132-2-03

D1:C

D3:C D3:A

G12132-2-08


21P BATTERY(Right Hold)

5AAN 8ga.

EMERBUS

EMER BUS BARG12132-2-21 AN16ga

1

2

3

4

5

6

G12132-2-01

G12132-2-14

NOTE: If the DIRECT BATTERY indicator light is desired, the installer shall provide a suitable light and install it within clear view of the pilot, with an appropriate label. Recommended maximum current 12mA.

3LK296E


ref: G12132-11-074280B2

G12132-2-12

NOTE: Cap and Stow 1PE1E

A Added note for 1PE1E. Changed name of airframe wire from P1:T. Added note about 5A PP46 bus breaker.

12/05/14 GA

G12132-2-30 AN 18ga.

The added aircraft-side wire listed here as G12132-2-30 must be labelled, but at the installer's discretion the label format may vary from the format used here provided it uniquely identifies each wire.

The EMER emergency bus MUST be rewired to match this diagram. The 5A circuit breaker is not present in the factory configuration and must be provided by the installer. The cable length between the battery and the 5A breaker must be kept as short as possible.

(Right Hold)

A Changed PP46 bus name to EMER. 01/14/15 GA

ref: WDM 63-41-00

1EW93NE

1EW37E

1EW38E

1EW39E

n

m

k

jP1 J1

G12132-3-161

2

3

4

5

6

G12132-3-15

G12132-3-14

MS24524-23

G12132-3-17

WARNING HORNESN-12

G12132-3-08

G12132-3-07

G12132-3-06

G12132-3-02

The Generator switch has a center off position. The forward position provides the normal GENERATOR ON function. The momentary aft position provides the GENERATOR RESET function.GENERATOR RESET receives power from CRANK breaker. GEN RST breaker is not installed.

PP1KK2E

1PA1E

1PA2E

N

M

N

M

1KK1E

1PA4E

P1 J1

U

V

U

V

ref: WDM 80-11-01ref: WDM 24-30-00

G12132-3-01


3 6

3

2

1

MS24523-26

G12132-3-05

ESN-5CRANK ENGINE

PP6

GENERATOR ON/RESET

G12132-3-03ESN-3

1

2

4

5


G12132-3-074280B2 A


GA 8/15/13

CLB 8/15/13

GA107 1


CRANK

2.5A

EFN-63

b

P1

c

1

2

3

4

5

6

G12132-3-20b


WARN/FIRE TEST

G12132-3-19

G12132-3-18

J1

ESN-7

GND for OVERLAYS

G12132-23-091WG18NE or 1PE4NE or GND



ref: WDM 33-10-00ref: WDM 26-11-10


MS24658-23D

ESN-11HYD TEST

1WW84E

HYDRAULICSPP5

7.5A

EFN-36P1 J1

G12132-3-101DH131E u

c

ref: WDM 29-10-00


u

3

2

1

G12132-3-09



d1WG4E d

G12132-3-21

n

m

k

j

A Changed Note for GEN RESET Circuit. Changed Hydraulic wiring. 12/05/14 GA

G12132-3-231DH67E t t

ref: WDM 29-11-00

G12132-4-074280B2 --


GA 8/15/13

CLB 8/15/13

GA107 1


MS24524-21

ANTI-COL


H

P2

L

ref: WDM 33-41-00STROBE LT

7.5A G12132-4-19

EFN-45 G12132-4-20

PP9

G12132-4-18H

L

J2

ref: WDM 33-42-00

ANTI-COL LT

EFN-83

G12132-4-17

7.5A

1

2

3

4

5

6

(Center off)

G12132-4-21ALL / TAIL

ESN-9PP6

The STROBE LIGHT switch circuit is optional and is usually used for additional strobe lights. If no additional strobe light is installed, wires G12132-4-19, G12132-4-20 and G12132-4-21 may be deleted.

ref: WDM 33-43-01


PP6TAXI LIGHT

7.5A

EFN-79

1LM9E G G

P2 J2G12132-4-04

LANDING LT

20A

EFN-95

PP9

G12132-4-05G12132-4-03 1LM1802E g

P1

g

J1

EFN-N/A-4

TAXI CTL

P1

h

PP6

2.5A

h

J1

LAND CTL

EFN-N/A-3

PP6

2.5A

1LM6EG12132-4-01 AN16ga.

P2

Y

J2

YG12132-4-02 AN16ga.Z Z

1LM8E

G12132-4-033

2

1

MS24523-23

LANDING LIGHTESN-18

G12132-4-06P1

h h

J1

1LM1E

At the installer's discretion the Landing Light switch may relocated from the Pilot's collective lever to the console, bypassing the collective switch as shown.

G12132-4-053

2

1

MS24523-23

TAXI LIGHTESN-17

G12132-4-07P1

g g

J1

1LM2008E

ref: WDM 33-43-01

ref: WDM 33-43-02

ref: WDM 33-43-02

At the installer's discretion the Taxi Light switch may relocated from the Pilot's collective lever to the console, bypassing the collective switch as shown.

Splice two AN16ga. wires from P2 pins Y and Z to 1LM6E. Wires should be kept as short as possible.

(1LJ5E or 1LJ48E or Installer Defined)


G12132-9-04 AN16ga.

MS24524-23


G12132-4-08 AN16ga.P1

e e

J1

1LJ3E

At the installer's discretion an optional POSITION LIGHT switch may be added to the console. This switch can turn off position lights when the [OFF/DAY/NIGHT] selector on the instrument panel is in DAY and NIGHT positions but does not turn on the position lights when the selector is in the OFF position.

EFN-87

POSITION LTS PP6

7.5A

1

2

3

4

5

6

(Double Pole switch used for current rating)

ref: WDM 33-41-00

1LX31E

SEE G12132-16-074280B2 FOR SAMPLE OPTIONAL CIRCUITS

Installer Defined

Installer Defined

Installer Defined

Installer Defined

U U

G12132-5-16 AN16ga.

G12132-5-15 AN16ga.

W

V

W

V

AVIONICS MASTER

1

2

3

4

5

6

MS24524-23

G12132-5-14AN16ga

G12132-5-13

T

P2

T

J2

AN16ga

OP-1

NOTE: If a FUEL PUMP indicator light is desired, the installer shall provide a suitable light and install it within clear view of the pilot, with an appropriate label.

ref: WDM 30-31-00

PP5

1FN35E

G12132-5-033

2

1

J2

MS24523-23

A

P2

A

G12132-5-04

PITOT HEATESN-13

ref: WDM 28-00-00

7.5A

EFN-39

PITOT HEAT

DD

P1

DD

J1

G12132-5-02

G12132-5-013

2

1

MS24523-23

FUEL PUMP-1ESN-2

EFN-67

7.5A

FUEL PUMP-1PP6

G12132-5-091KS2E yy

G12132-5-074280B2 --


GA 8/15/13

CLB 8/15/13

GA107 1



1

2

3

4

5

6

MS24524-23

G12132-5-10

Installer Defined

Installer Defined

1KS3E

P1x

J1x

ESN-21SAND FILTER

G12132-5-08

EFN-66

7.5A

PP6

EFN-91

1MK27E

1MK28E

G12132-5-173

2

1

G12132-5-19P

M

P2

P

M

J2

MS24523-23

WINDSHIELD WIPERESN-24

PP9

7.5A

W/S WIPER-1

NOTE: If a PITOT indicator light is desired, the installer shall provide a suitable light and install it within clear view of the pilot, with an appropriate label. Recommended maximum current 12mA.The Installer must install a relay of a suitable rating to drive the lamp, wired as shown.

1FW20E

1FW21E


G12132-5-18

G12132-5-11

G12132-5-12

ref: WDM 71-61-10

ref: WDM 30-42-00


1QN3E

2157

20

2321

141

174

185

163619

42Q

1QN1E

1QW81NE 1QN26EBA

DE

M5

224L

FM1

133L4Remove existing wire between224L M5-A and 224L M12-D

The original FUEL PUMP circuit MUST be rewired to match this diagram.

A3A1A2

X1

Y1

PITOT K1

1FN33E

1FN34NE

NOTE: If a FUEL PUMP 2 indicator light is desired, the installer shall provide a suitable light and install it within clear view of the pilot, with an appropriate label.

ref: WDM 28-00-00

BB

P1

BB

J1

G12132-5-06

G12132-5-053

2

1

MS24523-23

FUEL PUMP-2OP-3

EFN-68

7.5A

FUEL PUMP-2PP6

1QN9E

2157

20

2321

141

174

185

163619

44Q

1QN8E

1QN33NE 1QN29EGF

JK

M5

224L

DM1

133L4Remove existing wire between224L M5-F and 224L M12-E

The original FUEL PUMP 2 circuit MUST be rewired to match this diagram.

SAND FILTER

1KS36E

1KS32E

ref: WDM 71-61-10

NOTE: If a SAND FILTER indicator light is desired, the installer shall provide a suitable light and install it within clear view of the pilot, with an appropriate label.

HHHH

P1

GG

J1

GG


NR IND


PITOT HEAT

Detailed on G12132-5-074280B2

3EU3E

PP5

7.5A

EFN-39

G12132-6-03P1

A A

J1

EFN-38

3A

HYDRAULICS

WARN PNL-1


PP15

EFN-37

3A

PP5

7.5A

EFN-36

G12132-6-074280B2 A


GA 8/15/13

CLB 8/15/13

GA107 1

7.5A

EFN-43

INST. LTS-1

1A

EFN-42

ref: WDM 77-00-01

ref: WDM 33-10-00

3EU72E v

P1

EM-NR CONV


v

PP5

G12132-6-01J1

EMER

EFN-41

3A

ref: WDM 31-61-00

1EW103E

P1

D

VHIU-1

G12132-6-04J1

D

PP5ref: WDM 26-11-00

G12132-6-02P1

EE EE

J1

1LK738E

G12301:1 DIMMER CONTROL(SEE G12132-23-074280B2)

G12132-23-01



1WW1E and 1WW1F G12132-6-05P2

E E

J2

D2:C

D2:AEFN-40

1A

ref: WDM 77-00-01

3EU3F

P1

t

EM-NR IND

G12132-6-07J1

t

EMER

G12132-6-06

ref: WDM 24-30-00

A Changed PP46 to EMER. 12/05/14 GA



ATTITUDE

RELEASE

ref: WDM 25-00-00

ref: WDM 34-25-30

Installer Defined

G12132-7-05f

P1

f

J1

G12132-7-04 AN16ga.

PP5

3A

EFN-49

N N

EFN-48

P2 J2

3A

STROBE LT


1EW30E

ref: WDM 31-61-00

EFN-46

G12132-7-03P1

s

J1

s

PP5VEMD-1

7.5A

PP9

EFN-45

7.5A

2.5A

G12132-7-074280B2 --


GA 8/15/13

CLB 8/15/13

GA107 1

G12132-7-01

EXT LOAD

1ME87E or Installer Defined

EFN-58

P1

w

J1

w

2.5A

PP9

EFN-57


G12132-7-08

G12132-7-06

ref: WDM 24-30-00

ref: WDM 25-63-10HOIST

1WW31E

PP9

E

P1

E

J1

WARN PNL-2 PP6

EFN-56

2.5A

ref: WDM 31-61-00VEMD-2

1EW35E

EFN-55

P1

K K

J1

7.5A

PP6

ref: WDM 25-63-10PP15

ref: WDM 25-91-00



Wire directly to the Attitude Gyro or through an On/Off switch and/or the Avionics Master Relay; or, this function may be moved to a breaker supplied from a switched bus

G12132-7-091ME303E or Installer Defined Z

P1

Z

J1


ref: WDM 28-41-10

1QW38E G12132-8-03

EFN-61

2.5A

P1

r

J1

r

ref: WDM 28-00-00

ref: WDM 31-61-00

J1P1

G12132-8-02

G12132-8-01

FUEL FLOW

1QW1E C

P1

PP6

C

J1

FUEL GAUGE

EFN-60

2.5A

1EW105E B

PP6

B

VHIU-2

2.5A

EFN-59

PP6

ref: WDM 25-10-40

G12132-8-074280B2 --


GA 8/15/13

CLB 8/15/13

GA107 1

EFN-65

5A

7.5A

EFN-66

Detailed on G12132-5-074280B2SAND FILTER

Installer Defined

P1

i


PP6

G12132-8-06J1

i

EFN-63

2.5A

2.5A

EFN-64

ref: WDM 77-00-01

3EU71E

SPARE

P1

L

NR CONV

Detailed on G12132-3-074280B2CRANK

G12132-8-05

PP5

J1

L

PP6

PP6


ref: WDM 30-42-00

1MK7E G12132-8-04

EFN-62

7.5A

P2

Q

J2

Q

W/S WIPER-2 PP6


2.5A

1DT5E H H

P1

EFN-70

J1G12132-9-02



ref: WDM 31-31-00PP9HOUR METER

PP6

EFN-68

7.5A

FUEL PUMP-2

PP6FUEL PUMP-1

EFN-67

7.5A

PP6

G12132-9-074280B2 --


GA 8/15/13

CLB 8/15/13

GA107 1

PP6POSITION LTS

7.5A

EFN-87

ref: WDM 33-41-00

PP6ANTI-COL LT

7.5A

EFN-83

TAXI LIGHT

7.5A

EFN-79


G12132-9-031LE1E J

P1

J

J1

CABIN LTS

2.5A

EFN-76

PP6

1LJ3E e e

P1 J1G12132-9-04

CAM

EFN-75

PP5

2.5A

ref: WDM 33-12-00




1BG6E Red FF FF

P1 J1G12132-9-05

ref: WDM 25-10-40


LANDING LT

ref: WDM 80-11-01

1KK4E and 1KK4F

1MH20E and/or 1MH22E (if installed)

20A

EFN-95

G12132-10-03 AN16ga.

G12132-10-04 AN16ga.

EFN-94

PP9

P2

X

J2

X

PP9

10A

START

a

P2

a

J2

Detailed on G12132-5-074280B2W/S WIPER-1

SLING

PWR OUTLET


15A

EFN-93

10A

EFN-92

PP9

EFN-91

7.5A

G12132-10-01

Wire directly to the Gyro Compass, or through an On/Off switch; or, this function may be moved to a breaker that is supplied from a switched bus.

G12132-10-074280B2 --


GA 8/15/13

CLB 8/15/13

GA107 1

EFN-N/A-4

TAXI CTL PP6

2.5A

a

LAND CTL

EFN-N/A-3


PP6

2.5A

a


G12132-10-05 AN16ga.

ref: WDM 34-21-03

EFN-N/A-2

P1

GYRO

5A

J1

PP5

EFN-N/A-1

PP9

P2

b

AC INVERTER

EFN-97

1XU1E b

J2

PP9

2.5A

TURN & BANK

1FA1E or Installer Defined

ref: WDM 25-26-06

15A

Installer Defined G12132-10-02 AN16ga.cc

P2 J2

ref: WDM 25-91-00 Source directly from wire 1MY41E, or through an available power terminal post. See G12132-11-074280B2.

61

61




1MH1E

G12132-10-06G G

P1 J1

ref: WDM 34-26-03

ref: WDM 24-22-00


Wire directly to the Turn & Bank Indicator, or through an On/Off switch; or, this function may be moved to a breaker that is supplied from a switched bus.







RMSTR BUS BAR, Top Left


AN8ga G12132-11-13TB4To output of Radio Master relay

1PP9E

3PP23E

TB6

TB5AN8ga G12132-11-14

AN8ga G12132-11-04

AN8ga G12132-11-15

1PP6E

1PP5E

TB3

TB2

TB1 AN8ga G12132-11-01

AN8ga G12132-11-02

AN8ga G12132-11-03


G12132-11-074280B2 A


GA 8/15/13

CLB 8/15/13

GA107 1


G12135-10

G12135-12

G12135-8

G12135-2


G12135-10

G12135-8

G12135-9



AN10ga G12132-11-05SLING

10A

EFN-92

Detailed on G12132-10-074280B21MY41E

EMER BUS BAR, Middle Right AftAN16ga G12132-2-21G12135-2

The PP46 bus has been rewired to contain the EM-IDL/FLT (EFN-72K) and EM-NR IND (EFN-71E) breakers ONLY. This new bus is designated EMER. Any other breakers previously assigned to the PP46 bus must be relocated to the PP50 bus or to an installer-defined bus.


1

2

3

4

5

6

MS24659-23D

ESN-6

ref: G12132-2-074280B2

MASTER CUTOFF

A Changed PP46 to EMER bus. 12/05/14 GA

AIR

CR

AFT

FW

D




LEFT MIDDLE BUS BAR

Optional RMSTR BUS

?A

LTB-1

G12132-12-19

G12132-12-20

LTB-4

RMSTR BUS

RMSTR BUS

Optional

LTB-2

?A

LTB-3

?A

Optional

G12132-12-18

G12132-12-17

RMSTR BUS

RMSTR BUSLTB-5

?A

Optional

LTB-6

?A

Optional

G12132-12-16

G12132-12-15

G12132-12-14

Installer defined

Installer definedVU

VU

Installer defined

Installer definedT T

S S

Installer defined

Installer defined

Installer definedR R

Q

P

Q

P

RMSTR BUSOptional

G12132-12-09

RMSTR BUS

RMSTR BUS

?A

?A

LTB-7Optional

LTB-8

?A

Optional

G12132-12-12

G12132-12-13

G12132-12-10

G12132-12-11

RMSTR BUS

RMSTR BUS

?A

LTB-9Optional

?A

LTB-10Optional

G12132-12-07

G12132-12-08

G12132-12-05

G12132-12-06

RMSTR BUS

RMSTR BUS

?A

LTB-11

Optional

?A

LTB-12

Optional

G12132-12-04

G12132-12-03

G12132-12-01

G12132-12-02


Installer defined

Installer defined

Installer defined

Installer defined

Installer defined

L L

N

M

N

M

KJ

KJ

Installer defined

Installer defined

Installer defined

Installer definedHG

HG

FE

FE


Installer defined

Installer defined

Installer defined

Installer defined

CD

CD

AB

J3

AB

P3LEFT TOP BUS BAR

G12132-12-074280B2 --


GA 8/15/13

CLB 8/15/13

GA107 1

Installer definedG12132-12-30if installed.

Installer defined f f

G12132-12-29

G12132-12-28

G12132-12-27

G12132-12-26

?A

LMB-2

?A

LMB-3Optional PP15

LMB-5

LMB-4

Optional

Optional

Optional

PP15

PP15

?A

PP15

?A

e

d

Installer definede

Installer definedd

c

b

Installer definedc

Installer definedb


Installer definedG12132-12-21

PP15

G12132-12-25

G12132-12-24

G12132-12-23

G12132-12-22

LMB-8

LMB-7

LMB-6

?A

Optional

Optional

PP15

?A

PP15


LMB-9

?A

Optional

Optional

PP15

Y Y

a

Z

Installer defineda

Installer definedZ

X

W

Installer definedX

Installer defined

W

(p/n: G12135-12)

(p/n: G12135-10)

G12132-11-13RMSTR BUS

J3

PP15 BUS

P3

G12132-11-14AN8ga.


3PP23ETB5


ref: WDM 24-60-02ref: G12132-11-074280B2ref: G12132-16-074280B2

?A


MS24524-21

ANTI-COL ALL / TAIL

G12132-4-074280B2, ESN

-93A, PP5, EFN

-38

NR

IND

G12132-6-074280B2, 77-00-01

G12132-7-074280B2, 24-30-00

7.5A, PP6, EFN-68

G12132-5-074280B2, 28-00-00

WAR

N PN

L-2

FWD

G12132-13-074280B2 A


GA107 1

GA 8/15/13

GA 8/15/13

GA 8/15/13

CLB 8/15/13

2.5A, PP6, EFN-59

2.5A, PP6, EFN-60

FUEL G

AUG

EVH

IU-2

G12132-8-074280B2, 31-61-00

G12132-4-074280B2, 33-43-02


G12132-3-074280B2, 80-11-01

2.5A, PP6, EFN-64

7.5A, PP6, EFN-83

ANTI-C

OL LT

G12132-4-074280B2, 33-42-00

START

G12132-10-074280B2, 80-11-01

TAXI CTL

2.5A, PP6, EFN-N

/A-4G

12132-9-074280B2, 33-41-007.5A, PP6, EFN

-87

POSITIO

N LTS

2.5A, PP9, EFN-57

G12132-8-074280B2, 30-42-00

HO

IST

10A, PP9, EFN-94

G12132-7-074280B2, 25-63-10

G12132-8-074280B2, 77-00-01

7.5A, PP6, EFN-62

W/S W

IPER-2

NR

CO

NV

2.5A, PP6, EFN-76

CABIN

LTS

7.5A, PP6, EFN-79

TAXI LIGH

T

G12132-4-074280B2, 33-43-02

G12132-9-074280B2, 33-12-00

G12132-4-074280B2, 33-43-01

LAND

CTL

2.5A, PP6, EFN-N

/A-3G

12132-5-074280B2, 28-00-00

FUEL PU

MP-2

G12132-8-074280B2, 28-00-00

2.5A, PP6, EFN-61

G12132-8-074280B2, 28-41-10

FUEL FLO

W

2.5A, PP6, EFN-63

CR

ANK

SPARE

G12132-5-074280B2, ESN

-17

1A, EMER

, EFN-40

EM-N

R C

ON

V

G12132-6-074280B2, 77-00-01

EM-N

R IN

D

G12132-6-074280B2, 77-00-01

G12132-5-074280B2, ESN

-18

SPARE

MS24524-23

SPARE

G12132-5-074280B2, ESN

-10

SPARE

G12132-5-074280B2, ESN

-15

SPARE

G12132-5-074280B2, ESN

-14

MS24524-23

MS24524-23

G12132-6-074280B2, 33-10-00

INST. LTS-1

G12132-10-074280B2,24-21-03

GYR

O

ATTITUD

E

G12132-7-074280B2, 34-25-30

1A, EMER

, EFN-42

3A, PP5, EFN-49

G12132-7-074280B2, 31-61-00

5A, PP5, EFN-N

/A-2VEM

D-1

7.5A, PP5, EFN-46

3A, PP5, EFN-41

7.5A, PP5, EFN-39

PITOT H

EAT

G12132-5-074280B2, 30-31-00

5A, PP5, EFN-65

SPARE

G12132-8-074280B2

VHIU

-1G

12132-6-074280B2, 31-61-00M

S24524-23

MS24524-23

7.5A, PP6, EFN-55

VEMD

-2

G12132-7-074280B2, 31-61-00

2.5A, PP6, EFN-56

7.5A, PP6, EFN-66

G12132-5-074280B2, 71-61-10

7.5A, PP6, EFN-67

FUEL PU

MP-1

SAND

FILTERH

YDR

AULIC

S

G12132-3-074280B2, 29-11-00

CAM

G12132-9-074280B2, 25-10-40

7.5A, PP5, EFN-36

2.5A, PP5, EFN-75

MS24524-23

WAR

NIN

G H

OR

N

G12132-3-074280B2, ESN

-12

7.5A, PP5, EFN-43



G12132-13-074280B2-P122 A


GA107 1

GA 8/15/13

GA 8/15/13

GA 8/15/13

CLB 8/15/13


G12132-4-074280B2

G12132-9-074280B2

33-43-02

33-41-00

7.5A, PP6, EFN-87

POSITION LTS


G12132-8-074280B230-42-00

G12132-3-074280B2

G12132-8-074280B2

2.5A, PP6, EFN-63

NR CONV2.5A, PP6, EFN-64

CRANK


77-00-01

80-11-01

G12132-9-074280B2

G12132-4-074280B2

G12132-4-074280B2

33-42-00

33-43-02

33-12-00



G12132-4-074280B233-43-01


2.5A, PP6, EFN-76

CABIN LTSG12132-8-074280B2

G12132-8-074280B2

G12132-8-074280B2

2.5A, PP6, EFN-60

FUEL GAUGE

FUEL FLOW2.5A, PP6, EFN-61

28-41-10

28-00-00

31-61-00

G12132-7-074280B2

G12132-7-074280B2

2.5A, PP6, EFN-56


WARN PNL-2

VHIU-22.5A, PP6, EFN-59

24-30-00

31-61-00

G12132-5-074280B2

G12132-5-074280B2

28-00-00

71-61-10



G12132-6-074280B2

G12132-6-074280B2EM-NR IND1A, EMER, EFN-40

EM-NR CONV1A, EMER, EFN-42

77-00-01

77-00-01

FWD

G12132-7-074280B2

5A, PP5, EFN-N/A-2

3A, PP5, EFN-49

G12132-7-074280B234-25-30

ATTITUDE

G12132-10-074280B234-21-00

31-61-00

GYRO

INST. LTS-1

5A, PP5, EFN-65

7.5A, PP5, EFN-46

G12132-6-074280B233-10-00

VEMD-1

G12132-8-074280B2

7.5A, PP5, EFN-43

SPARE

G12132-6-074280B2

7.5A, PP5, EFN-39

3A, PP5, EFN-41

PITOT HEAT

G12132-6-074280B231-61-00

VHIU-1

G12132-5-074280B230-31-00

77-00-01

7.5A, PP5, EFN-36

2.5A, PP5, EFN-75

3A, PP5, EFN-38

CAM

HYDRAULICS

G12132-9-074280B2

NR IND

G12132-3-074280B229-11-00

G12132-10-074280B2

HOIST2.5A, PP9, EFN-57

80-11-04

10A, PP9, EFN-94

START

G12132-7-074280B225-63-10


25-10-40

G12132-5-074280B228-00-00



G12132-14-074280B2 --


GA107 1

GA 8/15/13

GA 8/15/13

GA 8/15/13

CLB 8/15/13

3A, P

P15,

EFN

-37

WAR

N P

NL-

1G

1213

2-6-

0742

80B2

, 24-

30-0

0

?A, P

P15,

LM

B-7

?A, P

P15,

LM

B-8

15A,

PP9

, EFN

-93

W/S

WIP

ER-1

PWR

OU

TLET

FWD

7.5A

, PP9

, EFN

-91

TUR

N &

BAN

K


EXT

LOAD

2.5A

, PP9

, EFN

-58

LAN

DIN

G L

T

20A,

PP9

, EFN

-95

STR

OBE

LT

7.5A

, PP9

, EFN

-45

AC IN

VER

TER

15A,

PP9

, EFN

-97

?A, P

P15,

LM

B-6

2.5A

, PP9

, EFN

-N/A

-1

HO

UR

MET

ER

2.5A

, PP9

, EFN

-70

?A, P

P15,

LM

B-5

??, R

MST

R b

us, L

TB-1

1

??, R

MST

R b

us, L

TB-1

2

MS2

4659

-23D

BAT-

EXT

PWR

SAN

D F

ILTE

R

MS2

4524

-23

W/S

WIP

ER

??, R

MST

R b

us, L

TB-7

??, R

MST

R b

us, L

TB-8

??, R

MST

R b

us, L

TB-1

0

??, R

MST

R b

us, L

TB-9

??, R

MST

R b

us, L

TB-6

??, R

MST

R b

us, L

TB-5

??, R

MST

R b

us, L

TB-3

??, R

MST

R b

us, L

TB-4

FUEL

PU

MP-

1

MS2

4523

-23

MS2

4523

-23

FUEL

PU

MP-

2

MS2

4523

-23

??, R

MST

R b

us, L

TB-2

??, R

MST

R b

us, L

TB-1

DIR

ECT

BATT

MS2

4524

-23

AV M

ASTE

R

MS2

4524

-23

Opt

iona

lG

1213

2-12

-074

280B

2

Opt

iona

lG1

2132

-12-

0742

80B2

Opt

iona

lG

1213

2-12

-074

280B

2

Opt

iona

lG

1213

2-12

-074

280B

2

Opt

iona

lG

1213

2-12

-074

280B

2

Opt

iona

lG

1213

2-12

-074

280B

2

Opt

iona

lG

1213

2-12

-074

280B

2

Opt

iona

lG

1213

2-12

-074

280B

2

Opt

iona

lG

1213

2-12

-074

280B

2

Opt

iona

lG

1213

2-12

-074

280B

2

Opt

iona

lG

1213

2-12

-074

280B

2

Opt

iona

lG

1213

2-12

-074

280B

2

Opt

iona

lG

1213

2-12

-074

280B

2

Opt

iona

lG

1213

2-12

-074

280B

2

Opt

iona

lG1

2132

-12-

0742

80B2

Opt

iona

lG

1213

2-12

-074

280B

2

G12

132-

5-07

4280

B2, 3

0-42

-00

G12

132-

10-0

7428

0B2,

24-

60-0

1

G12

132-

4-07

4280

B2, 3

3-41

-00

G12

132-

4-07

4280

B2, 3

3-43

-01

G12

132-

10-0

7428

0B2,

24-

22-0

0

G12

132-

7-07

4280

B2, 2

5-91

-01

G12

132-

9-07

4280

B2, 3

1-31

-00

G12

132-

10-0

7428

0B2,

34-

26-0

3

G12

132-

5-07

4280

B2, O

P-1

G12

132-

2-07

4280

B2, O

P-2

G12

132-

5-07

4280

B2, E

SN-2

1

G12

132-

5-07

4280

B2, E

SN-2

4

G12

132-

5-07

4280

B2, O

P-3

G12

132-

5-07

4280

B2, E

SN-2

G12

132-

2-07

4280

B2, E

SN-1


REL

EASE

3A, P

P15,

EFN

-48

G12

132-

7-07

4280

B2, 2

5-00

-00

10A,

OP1

bus

, EFN

-92

G12

132-

10-0

7428

0B2,

25-

91-0

0

SLIN

G

?A, P

P15,

LM

B-9

Opt

iona

lG

1213

2-12

-074

280B

2

?A, P

P15,

LM

B-4

Opt

iona

lG

1213

2-12

-074

280B

2

?A, P

P15,

LM

B-2

Opt

iona

lG

1213

2-12

-074

280B

2

?A, P

P15,

LM

B-3

Opt

iona

lG

1213

2-12

-074

280B

2

SLING

PWR OUTLET

10A, OP1, EFN-92

15A, PP9, EFN-93


STROBE LT

AC INVERTER

20A, PP9, EFN-95

LANDING LT

15A, PP9, EFN-97

EXT LOAD

G12132-10-074280B2

2.5A, PP9, EFN-58

HOUR METER


TURN&BANK

G12132-7-074280B2

G12132-10-074280B2

G12132-4-074280B2

G12132-10-074280B2

G12132-10-074280B2

G12132-5-074280B230-42-00

25-91-00

24-60-01

33-43-01

24-22-00

25-91-00

FWD Effectivity: AS350B2 EmbodyingMod 350A07-4280

2.5A, PP9, EFN-70

G12132-9-074280B231-31-00

7.5A, PP9, EFN-45

G12132-4-074280B233-41-00

G12132-14-074280B2-P122 --


GA107 1

GA 8/15/13

GA 8/15/13

GA 8/15/13

CLB 8/15/13

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-7-073273RELEASE

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional

G12132-12-073273Optional








?A, RMSTR, LTB-5

3A, PP15, EFN-48

?A, RMSTR, LTB-4

?A, RMSTR, LTB-3

?A, RMSTR, LTB-2

?A, RMSTR, LTB-1

G12132-6-074280B224-30-00

WARN PNL-1

34-26-03


G12132-12-073273Optional

?A, PP15, LMB-3

G12132-12-073273Optional

?A, PP15, LMB-2

25-00-00

G12132-15-074280B2 --

CONSOLE SWITCH LAYOUTP132 TOP VIEW

GA107 1

GA 8/15/13

GA 8/15/13

GA 8/15/13

CLB 8/15/13

WIPER

G12132-5-074280B2, ESN-21

G12132-5-074280B2, ESN-24

DIRECT BATT

SAND FILTER

G12132-5-074280B2, OP-1

G12132-2-074280B2, OP-2

MS24524-23

MS24524-23

AV MASTERMASTER

AVIONICS

BATTERY

MS24524-23

MS24523-23

W/S WIPER

SANDFILTER


G12132-5-074280B2, ESN-2

G12132-2-074280B2, ESN-1BAT-EXT PWR

FUEL PUMP-1

G12132-5-074280B2, OP-3

WINDSHIELD

MS24659-23D

MS24523-23 PUMP-1FUEL

POWERBAT-EXT

G12

132-

5-07

4280

B2,

ES

N-1

3

G12

132-

2-07

4280

B2,

ES

N-6

G12

132-

3-07

4280

B2,

ES

N-5

G12

132-

3-07

4280

B2,

ES

N-7

G12

132-

3-07

4280

B2,

ES

N-1

1

G12

132-

3-07

4280

B2,

ES

N-3

PITO

T H

EAT

MS

2465

9-23

D

MS

2452

3-23

MA

STE

R C

UTO

FF

MS

2452

3-26

MS

2740

7-3

WA

RN

/FIR

E T

EST

CR

AN

K E

NG

INE

MS

2465

8-23

D

MS

2452

4-31

GE

N O

N /

RE

SE

T

HY

D T

EST

TESTWARN/FIRE

ON/RESETGENERATOR

TESTHYD

CUTOFFMASTER

ENGINECRANK PITOT

HEAT

SPARE

G12132-5-074280B2, ESN-18

G12132-5-074280B2, ESN-17

G12132-5-074280B2, ESN-10

G12132-5-074280B2, ESN-15SPARE

SPARE

SPARE

SPARESPARE

SPARE

MS24524-23

MS24524-23

SPARE MS24524-23

MS24524-23

G12132-5-074280B2, ESN-14

G12132-4-074280B2, ESN-9

G12132-3-074280B2, ESN-12

SPARE

ANTI-COL ALL / TAIL

WARNING HORN

SPARE MS24524-23

ALL / TAILANTI-COL

WARNINGHORN

MS24524-21

MS24524-23

FUEL PUMP-2

FUELPUMP-2MS24523-23


DIRECT

G12132-3-074280B2ESN-5, MS24523-26

P122 CONSOLE LAYOUT

G12132-5-074280B2

G12132-4-074280B2ESN-17, MS24524-23

ESN-13, MS24523-23

ESN-15, MS24524-23G12132-4-074280B2

G12132-5-074280B2OP-1, MS24524-23

G12132-4-074280B2

AVIONICSMASTER

ESN-14, MS24524-23


ESN-10, MS24524-23G12132-4-074280B2 G12132-4-074280B2

ESN-9, MS24524-21

PANELDIMMER

FUELPUMP-2

GENERATORON / RESET

G12132-3-074280B2ESN-3, MS24524-31

SPARE

G12132-5-074280B2OP-3, MS24523-23

G12132-5-074280B2

SPARE

ESN-2, MS24523-23

FUELPUMP-1

ESN-1, MS24659-23DG12132-2-074280B2

BAT-EXTPOWER

G12132-3-074280B2ESN-11, MS24658-23D

ESN-21, MS24524-23G12132-5-074280B2

SPARE

SANDFILTER

ANTI-COLALL / TAIL

ESN-24, MS24523-23G12132-5-074280B2

WINDSHIELDWIPER

G12132-3-074280B2ESN-7, MS27407-3

HYDRAULICTEST

WARN / FIRETEST

DIRECT BATTERY

ESN-18, MS24524-23G12132-4-074280B2

OP-2, MS24524-23G12132-2-074280B2

WARNINGHORN

G12132-2-074280B2ESN-6, MS24659-23D

SPARE

ESN-12, MS24524-23G12132-3-074280B2

SPARE

PITOTHEAT

MASTERCUTOFF

CRANKENGINE

G12132-15-074280B2-P122 --


GA107 1

GA 8/15/13

GA 8/15/13

GA 8/15/13

CLB 8/15/13


G12132-23-08 AN22ga

G12132-23-12 AN22ga

G12132-23-01

G12132-23-02

G12132-24-02 AN22ga

G12132-24-01 AN22ga

G12132-23-06 AN22ga

G12132-23-07 AN22ga

G12132-23-10 AN22ga

G12132-23-11 AN22ga

3

ref: G12132-3-074280B2

ESN-7WARN/FIRE TEST


4

5

6

PWR 1

PWR 2

1

2

1

G12132-23-092

3

DIMMER CONTROL

PWR OVERLAY

PWR POT

GND

G12301

4

5

1

G12132-23-074280B2 A

SWITCH LEGEND LIGHTINGP132 and P122 CONSOLE WIRING

GA 8/15/13

CLB 8/15/13

GA107 1


WIRING

100 OHM



OVERLAY-RIGHT-

OVERLAY-TOP-

OVERLAY-LEFT-

M

M

M

G12132-24DIMMER POT ASSEMBLY

3

2

OVERLAY-RIGHT+

OVERLAY-TOP+

OVERLAY-LEFT+

F

F

F


7.5A

EFN-43

INST. LTS-1 PP5

ref: G12132-6-074280B2

CONSOLE LTS powerSS

P2 J2

1.5A Maximum Current

ref: G12132-37-074280B2

from PP50 BUS


A Changed Quick Diconnect Part Numbers 12/05/14 CLB

www.genevaaviation.com G12132-37-074280B2 --

07-4280 CONSOLE LIGHTEXTERNAL WIRING

GA 8/15/13

CLB 8/15/13

GA107 1


INST LTS 2 PP50

5A

SS

P2 J2G12132-23-02Installer Defined AN 20ga.

3LK296E20

R2

243L RELAYU/CP FLOOR

CONSOLE BACKLIGHT POWER FROM PP50 BUS

For aircraft that embody mod 360A07-4280, the console backlight power supply pin J2:S must be connected to the PP50 bus through a circuit breaker of an appropriate current rating, 1.5A or greater.

Power may be supplied from the INST LTS. 2 breaker in the 50alpha breaker box in the R/H Baggage compartment via the 3LK296E wire at the 243L relay.

It is the installers responsibility to confirm the total current draw from both the instrument panel and console lights does not exceed the current rating of both the circuits and breaker.

The installer must label the added wiring with unique identifying marks and update the wiring diagrams to reflect the changes made.


50 ALPHA BREAKER PANELR/H BAGGAGE COMPARTMENT

ref: G12132-23-074280B2

ref: WDM 33-10-00


Documents

G12132 CONSOLE WIRING DIAGRAMS REVISION U