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COMPONENT MAINTENANCE MANUAL 653AX9XXXX FIRST ISSUE : JUNE 12/2006 25-33-93 APR 10/07 F9767 GALLEY TYPE A0E13J11 NL BP PN : 653A398108 653A892108 COMPONENT MAINTENANCE MANUAL WITH ILLUSTRATED PARTS LIST

ATR-42 Galley Manual for the aircraft BHN,BHO,BHP

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Essential document for ATR-42 systems training and ATR-42 galley trouble shooting.

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  • COMPONENT MAINTENANCE MANUAL653AX9XXXX

    FIRST ISSUE : JUNE 12/2006 25-33-93APR 10/07

    F9767

    GALLEYTYPE A0E13J11 NL BP

    PN : 653A398108653A892108

    COMPONENT MAINTENANCE MANUALWITH

    ILLUSTRATED PARTS LIST

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    FIRST ISSUE : JUNE 12/2006 25-33-93APR 10/07

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    25-33-93RECORD OF REVISIONS page 1

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    R E C O R D O F R E V I S I O N S

    REVISION N REVISION DATE INSERTION DATE BY

    01 APR 10/07

    Retain this record in the front of the manual. On receipt of revisions insert revised pages inthe manual and enter revision number, revision date, date inserted and initials.

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    R E C O R D O F S E R V I C E B U L L E T I N S

    SERVICEBULLETIN

    INCORPORATIONDATE REVISION OBJECT

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    ILLUSTRATED PARTS LIST TP 1001 page 1page 2 (blank)

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    INTRODUCTION Intro page 1page 2page 3page 4

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    LIST OF VENDORS LOV page 1page 2

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    25-33-93TABLE OF CONTENTS page 1

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    T A B L E O F C O N T E N T SPAGES

    INTRODUCTION INTRO1. General2. Presentation of manual3. Updating

    DESCRIPTION AND OPERATION 11. General2. Description

    A. StructureB. AttachmentsC. Electrical feedD. Water connectionE. Main ComponentF. Overall dimensionsG. Installations

    3. OperationA. Access doors to stowage compartmentsB. Locking of built-in componentsC. Operation of built-in materialsD. Electrical installationE. ConnectionsF. Supplyong of water to the galleyG. Making the galley operationalH. Switching off the galley

    TESTING AND TROUBLESHOOTING 1011. General

    A. DoorsB. Revolving retainersC. Electrical installation

    2. TestingA. Electrical circuitsB. Hydraulic systemC. Filter cylinderD. Disinfecting the water and tank system

    3. TroubleshootingA. The W/T indicator light fails to illumateB. The W/T indicator light fails to illumateC. the pump does not operateD. The water heater fails to operate

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    PAGESE. The hot water flow is weak

    AUTOMATIC TEST REQUIREMENTS (ATLAS) NOT ALLOCATED

    DISASSEMBLY 3011. General2. Specific component disassembly instructions

    A. Dismantling the water heaterB. Dismantling of the CONTROL PANEL and RELAY PANEL C. Dismantling of the hydraulic sectionD. DoorsE. Edging profilesF. Decorative panelG. Folding tableH. BasinI. Removal of upper attachmentsJ. Removal of lower attachments

    CLEANING 4011. General2. In-flight cleaning3. On-ground cleaning

    CHECK, CONTROL 5011. General2. Specific component check procedures

    A. Stowage compartment doorsB. Sandwich panelsC. Galley attachmentsD. Electrical installationE. Checking

    REPAIRS 601I- REPAIRS OF SANDWICH PANELS

    1. General2. Necessary materials and products3. Repair procedure

    A. Determining damagesB. Preparation of the repair areaC. Use of adhesives

    4. RepairsA. Preparation of the damaged surfaceB. Preparation of productsC. Minor repairs

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    PAGESD. Major repairs

    ASSEMBLY 7011. General2. Necessary materials and products3. Specific component assembly instructions

    A. Bonded profileB. Stowage compartment door latchesC. Decorative panelD. Installation of lower attachmentE. Installation of upper attachmentF. BasinG. Folding tableH. Piping and tankI. Assembling the water heaterJ. Electrical connections

    4. Storage

    FITS AND CLEARANCES NOT ALLOCATED

    SPECIAL TOOLS AND EQUIPMENT 9011. General

    ILLUSTRATED PARTS LIST (IPL) 1001

    INTRODUCTION INTRO1. General2. Material arrangement

    A. IntroductionB. Alphanumerical IndexC. Detailed Parts List

    3. How to use the Parts ListA. When the part number is knownB. When the part number is not known

    4. List of abbreviations

    LIST OF VENDORS LOV

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    L I S T O F I L L U S T R A T I O N S

    FIGURES PAGES

    DESCRIPTION AND OPERATION1 Situation of galley 22 Installation 5

    TESTING AND TROUBLESHOOTING101 Electrical schematic 104102 Electrical schematic 105103 Electrical nomenclature 106104 Hydraulical schematic 107

    DISASSEMBLY301 Doors 301302 Decorative panel 302303 Decorative panel on door 303

    REPAIRS602 Repair instructions 606603 Repair instructions 606604 Repair instructions 606605 Repair instructions 607606 Repair instructions 607607 Repair instructions 607608 Repair instructions 608609 Repair instructions 609610 Repair instructions 609

    ASSEMBLY702 Door latches 702703 Decorative panel 703704 Decorative panel on door 703

    ILLUSTRATED PARTS LIST1 Galley unit 1001-02 Primary structure assy 1002-03 Primary structure assy 1003-04 Secondary upper structure 1004-05 Secondary lower structure 1005-06 Lower fitting assy 1006-07 Upper fitting assy 1007-08 Hydraulic installation assy 1008-0

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    FIGURES PAGES9 Wastebin door assy 1009-0

    10 Basin assy 1010-011 Folding table assy 1011-012 Electrical circuit assy 1012-013 Cap assy 1013-014 Secondary Upper Structure Assy 1014-015 Secondray Lower Structure Assy 1015-016 Hydraulic installation assy 1016-0

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    I N T R O D U C T I O N

    General

    This Component Maintenance Manual with Illustrated Parts List has been elaboratedaccording to standard ATA 100 (AIR TRANSPORT OF AMERICA). It should enable amechanic who is not familiar with this equipment to check the condition and repair thecomponents making up this equipment. This manual does not specify a work schedule forthe component.

    This galley is manufactured by:

    SIMAIR17, AVENUE ANDRE DULIN

    ZONE INDUSTRIELLE DES SOEURS17300 ROCHEFORT SUR MER

    FRANCETel. : 33.5.46.99.71.49 - FAX : 33.5.46.87.40.12

    (F9767)

    Presentation of manual

    For page numbering, a number group is used for each heading described in thisMaintenance Manual.

    1 - 99 Description and Operation101 - 199 Testing and Troubleshooting301 - 399 Disassembly401 - 499 Cleaning501 - 599 Check, Control601 - 699 Repairs701 - 799 Assembly901 - 999 Special Tools and Equipment

    1001 - 1099 Illustrated Parts List

    Updating

    Updating, inclusions and deletions carried out manually will be indicated by a black line inthe margin, only opposite the printed part of the modified contents of the document.

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    ATTENTION :

    SIMAIR assumes no liability whatsoever, whether contractural, warranty, tort or otherwise,for any unauthorized substitution of or alteration to any part contained in any ERC galley orfor any alteration not performed in accordance with SIMAIR approved procedures.

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    D E S C R I P T I O N A N D O P E R A T I O N

    1. General

    The galley intended to store hotel products is situated at the right aft section of thepassengers compartment. In function with standard aircraft, its position is given in Figure 1.

    2. Description

    A. Structure

    From the monoblock construction, formed beginning from the sandwich panelsassembled between them by the tenons and mortices then bonded, the galley is dividedinto several compartments each having a particular function. Its dimensions allow itsplacement in the aircraft in passing through the passengers door.

    B. Attachments

    The galley is permanently attached to the aircraft structure by two attachments locatedat the upper part and one attachment located at the lower part. Each attachment isaccessible and easily disassembled.

    C. Electrical feed

    The electrical energy necessary for incorporated equipments (hot jugs, ovens ...)functioning is provided by the electrical network of the aircraft from cables andindependant connections of aircraft circuit.

    D. Water connection

    The tank consists of a filling outlet and an open air exhaust outlet, both connected tothe pipe work of the aeroplane

    Two draining pipes empty the water from the tank and the water heater to the containerbin.

    E. Main components

    - One water heater.

    - One 9 liter capacity water tank installed in the upper part of galley. It is fitted with awater presence sensor.

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    - An electric pump unit including a pressure regulation system.

    - A water purification filter.

    - Two drainage cocks.

    - One piping unit and one fast action connector enabling the connection water heater tothe water systels.

    - one electric plate attached to the galley comprising :

    . 1 ruler No. 02MC3 for the connections of the electrical circuits.

    . 1 CONTROL PANEL with a WATER TANK indicator (W/T), a WATERPUMP switch (W/T), the ON indicator and the 03MC8 monophase circuitbreaker.

    . 1 RELAY PANEL with the 03MC10 water heater and 03MC11 pumpprotective circuit breakers as well the control relays14MC2 and 14MC3 for the14MC1 pump.

    . 1 power supply from the 24 Vcc.

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    SITUATION OF GALLEYFIGURE 1

    X

    21909.221033.2

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    F. Overall dimensions

    Dimensions

    Height : 1875 mm (73.81 in)Width : 822 mm (32.36 in)Depth : 985 mm (38.78 in)

    Density

    P/N Without equipments : With equipments :653A398108 77 kg ( 169.4 lb ) 318.6 kg ( 701 lb )

    G. Installation (fig. 2)

    ITEM DESIGNATION CAPACITIES Qty1 HOT-CUP 1 kg ( 2.20 lb ) 12 PROVISION FOR WATER-HEATER 9 kg ( 20 lb ) 13 WORKING AREA 14 ICE UNIT 5 kg ( 11 lb ) 15 HALF-SIZE TROLLEY 60 kg ( 132 lb ) 16 OVEN DF115 45.5 kg ( 100.1 lb ) 17 STOWAGE 12 kg ( 26.4 lb ) 18 SU 20 kg ( 44 lb ) 19 SU 20 kg ( 44 lb ) 1

    10 WASTE BIN 10 kg ( 22 lb ) 111a 10 kg ( 22 lb ) 111b WATER TANK 20 kg ( 44 lb ) 112 FOLDING TABLE 40 kg ( 88 lb ) 113 HALF-SIZE TROLLEY 60 kg ( 132 lb ) 114 BASIN None 115 SLIDING TABLE 40 kg ( 88 lb ) 1

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    3. Operation

    A. Access doors to stowage compartmentsThe doors are equipped with a pallet latch and a security latch fitted with a commandbutton having two positions : open (red dot),closed looking position (green dot). Closingand locking a door are obtained as follows :

    (1) Door closed, not locked : the bolt of the latch is completely engaged in the strike.The bolt of the security latch is retracted, the red dot on the command button isvisible. The door can be opened by operating the closing latch flap.

    (2) Door closed, locked : the bolt of the latch and that of the security latch arecompletely engaged in their strike. The green dot on the command button of thesecurity latch is visible, the red dot is hidden. The door can not be opened byoperating the latch flap.

    B. Locking of built-in components(1) Compartment hot jugs and standard unit.

    The immobilization of equipments is ensured by using two rotary latches.

    (2) Folding tableEasy functionning two-position rotary latches allow immobilizing the folding table ina folded position.

    Note :

    Any item within a storage compartment, which prevents closing a door or locking rotarylatches, must be removed. Signs installed in the galley compartments indicate itsindividual maximum capacity which must not be exceeded.

    C. Operation of built-in materialsSpecific instructions concerning the operation of material built-in the galley are notdescribed in this manual. They are generally furnished by the vendor of the materialsused.

    D. Electrical installationElectrical equipment installed in the galley must be supplied power only at the time ofusage. The installation is protected by thermal circuit-breakers whose main purpose isto protect the electrical wiring from overload. In no case should these circuit-breakersbe used as switches.

    E. Connections

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    The Galley is connected to the hydraulic system by a fast action HANSEN connectorand to the electrical circuit by the 01MC4 jack.

    F. Supplying of water of the galleyThis takes place before take-off. The galley is connected to the planes water system.

    Before filling, two factors must be taken into consideration.

    (1) When the galley is in operation (the W/P switch is in tyhe ON position). At thetime of filling of the planes water system, the galley tank (9 liters or 20 liters) andthe water heater tank wil also be filled.

    If the indicator light is not on, ensure that the filling of water has fully taken place. Ifthe light still does not illuminate, refer to the chapter Testing andTroubleshooting .

    The filling of the water heater takes place by activating the water pump switch(W/P) throughout the period of use.As a result of its regularization, the pump maintains its pressure at the water heaterinlet. It starts up and operates automatically once the hot water is extracted.

    When the galley tank is empty, the W/P indicator light turns itself off and the pumpstops.

    Put the W/P switch in the OFF position. Hot water can be drawn off until thewater heater is empty.

    (2) When the galley is not in operation (the W/P switch in in the OFF position).Only the 9 liters or 20 liters tank is full.

    G. Making the galley operationalSwitch on the circuit breakers, Nos. 03MC8, 03MC10 and 03MC11.

    H. Switching off the galleyDisarm the circuit breakers 03MC8, 03MC10, 03MC11.

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    INSTALLATIONFIGURE 2

    1

    2

    3

    4

    6 10

    12

    11a

    7

    8

    9

    513 5

    14

    13

    15

    11b

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    T E S T I N G A N D T R O U B L E S H O O T I N G

    1. General

    Design of the galley is simple and the tests are limited to checking the operation of doorsand latches.

    A. Doors

    The wear on hinges and latches can be easily observed. Refer to the assembly anddisassembly section for the eventual need of their replacement.

    B. Revolving retainers

    As with doors, the wear on revolving retainers is easily observed. Particularly on cupretainers. Refer to the assembly and disassembly section for the eventual need of theirreplacement.

    C. Electrical installation

    Testing the electrical installation is limited to checking the hot jugs supply systems.Eventual troubleshooting can be done by consulting the electrical schematic in figure101 and 102.

    2. Testing

    A. Electrical circuits

    - testing of indicator lights W/P and W/T.- Visual testing of the CONTROL PANEL No. 03MC8 circuit breaker.- Visual testing of the RELAY PANEL circuit breaker ( by removing the access panel ).- Visual control of the water heater connection.

    B. Hydraulic system

    - Checking that the drainage cocks are closed.- Checking for any possible leaks.- Checking that the fast action HANSEN water heater connector is well connected.

    C. Filter cylinder

    - Replacement of cylinder after being filled 600 times or if the flow drastically reduces ( toless then 1 gallon per minute).

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    D. Disinfecting the water and tank systems

    - Put the disinfecting product into the tank periodically, or systematically every time thegalley are removes, in the following measurements :

    Tank : 4.5 ml.- Perform a disinfecting cycle by carrying out the operation defined in the in the chapter Description and operation , paragraphe 3.F.

    3. Troubleshooting

    In this section we are only concerned with the repair of the whole unit.For the water heater and the pump, refer to the CMM for these pieces of equipement.In the event of breakdown, refer to either the electrical or hydraulic diagrams dependingon the type of fault.

    A. The W/T indicator light fails to illumate.

    W/T

    OFFON

    Is there any water in the tank ?NO

    YES

    Check the circuit breaker No.03MC8Check the indicator lightCheck the seal No. 11MC9power supply ( see diagram )

    Check againafter filling

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    B. The W/T indicator light fails to illumate when you press the switch

    Check :- The circuit breaker No. 03MC8.- The indicator light.- The power supply.

    C. The pump does not operate when the W/P switch is activated :

    -Check the water pressure ( W/T illuminated).- The pump should stop once operational pressure has been reached (23 Psig). Once the water heater tap is turned on the pressure reducesand at 15 Psig the pump should become engaged.If the pump does not start to function :

    - Check the 3A circuit breaker No. 03MC11 (remove the access panel ).- Check the tension pressure on the pump connector.- Check the relays No. 14MC2 and 14MC3.- Check the pump, refer to its CMM.

    D. The water heater fails to operate

    - Check the 15A circuit breaker No. 03MC10 (remove the accesspanel).- Check the tension at the connector terminals No. 01MC4.- Check the water heater equipment, refer to its CMM.

    E. The hot water flow is weak :

    - Check the filter on the pump.- Check and replace the filter cylinder if necessary.- if the problem persists, measure the pressure at the HANSENconnector outlet (rate 15-23 Psig). If the pressure are incorrect, refer tothe pump CMM.

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    FIGURE 101ELECTRICAL SHEMATIC

    651A2926-100

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    FIGURE 102ELECTRICAL SHEMATIC

    651A2926-100

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    11MC10 1 NSA937910EA2000 CONTACT

    122MC1 NSA936809-RG0002 SPLICE

    BACKSHELL

    02MC3 4 NSA937905 SH02

    02MC3 2 NSA937905E02MC3 3 NSA937905C10

    Qte1

    1

    2

    BARRETTE A BORNEENTRETOISE

    4

    REPERE ELEC Rep REFERENCE DESIGNATION

    01MC41 AS85049/31S16N

    1

    1

    CONTACT

    LAMPE

    204J01HV1NZ1480NNSA937910EA2000

    07MC4

    100VK01B00B00N CORPS DE VOYANT

    E0251A0S

    1CONTACT 6NSA937910EA2000

    41

    NSA936809-RG0003 SPLICE

    NSA936809-RG0003 SPLICENSA936809-RG0003 SPLICE

    1NSA936809-RG0002 SPLICE

    18MC119MC1

    21MC1

    1

    11MC1

    07MC4 1

    09MC9 A1

    09MC8 A

    1121

    8

    1

    15MC1 A1 NSA937910EA2000 CONTACT

    14MC3 A1 E0252DK1600 CONTACT

    17MC1

    204J01NAAWE TETE DE VOYANT15MC1 1 73E LAMPE15MC1 A

    15MC1

    114MC3 E0246-28A0 RELAIS 4RT-10A 114MC3 A SOCLE RELAIS

    14MC2 A1 E0252DK1600 CONTACT14MC2 A E0219ASXXX SOCLE RELAIS

    2

    E0217XXX030A RELAIS TEMPORISE (30S) 2RT411

    4

    411

    LS1750-TFC INTERRUPTEUR A FLOTTEUR11MC911MC10 NSA938993-33

    4

    TETE INDICAT. INTER.

    TETE INDICAT. INTER.

    14MC2

    SPLICE DEMONTABLE

    09MC9

    FOUR DF700

    CORPS INDICAT. INTER.

    121120VK01N0GB30S CORPS INDICAT. INTER.

    129VK01V0SR20NB

    73E

    E0512A1409MC809MC8 1

    09MC8 A1

    09MC9 A

    1

    03MC11 NSA931322-030

    CONTREPLAQUEMS3450W14-5S

    204J01NAAWE

    103MC8 NSA931320-030SHUNT

    EN3155-004M1212

    03MC10 NSA931322-15003MC9 NSA931320-075

    BROCHE

    VIS A COLONETTE02MC3 1 NSA937905F

    01MC6 A1 E0199-03-14K

    02MC3 NSA937905A1001MC6 A2

    01MC6 A EN2997SE61404AN CONNECTEUR 28VDC

    01MC1 A1 NSA938186-0301MC4 MS3106R16-1SF80

    CONNECTEUR 115VAC01MC1 A NSA938925BMP

    1

    7

    REDUCTEUR DE SERTISSAGE

    1

    5

    1

    1

    SERRE-CABLES

    FICHE WATER HEATER

    1

    1

    1

    CAPOT

    DISJONCTEUR TRIPHASE

    2

    CONNECTEUR POMPE

    1

    DISJONCTEUR UNIPOLAIRE

    DISJONCTEUR TRIPHASE

    20MC1 1NSA936809-RG0003 SPLICE

    DISJONCTEUR UNIPOLAIRE 1

    03MC12 NSA931322-150 DISJONCTEUR TRIPHASE 1

    14MC1 A E0250B0S SOCLE RELAIS14MC1 B E0252DK1600 CONTACT

    114MC1 E0245-115B0 RELAIS 2RT-10A13MC1 CA13303 PRISE HOT CUP

    111MC1 J1 A 857-0590-130 CONTACT 311MC1 J1 ACR-6-33 CONNECTEUR

    311MC1 J1 B 857-0591-130/B CONTACT

    GAINEE0389V15

    CABLE MONOFILAIREE0261CF16E0261CF14

    CABLE MONOFILAIRE

    CABLE MONOFILAIREE0261CF10

    NSA936501TA1403

    E0470A01

    3COSSE

    GAINEE0389V08

    E0432A10 GAINEE0432A06 GAINE

    NSA937201ME0400 MANCHON TMS

    NSA937201ME1000 MANCHON TMSNSA937201ME0600 MANCHON TMS

    NSA937201ME1200

    REPERE ELEC Rep REFERENCE DESIGNATION Qte

    MANCHON TMS

    COSSE

    E0261CF20

    CABLE MONOFILAIREE0260BF18

    18

    NSA936501TA1404 COSSE

    NSA936501TA1604NSA936501TA1603

    E0432A20 GAINEE0432A12 GAINE

    18NSA936501TA1003

    1210COSSE

    COSSECOSSE

    3

    ETIQUETTE AUTOCOLLANTE

    NSA936501TA1004

    E0261CF12 CABLE MONOFILAIRE

    CABLE MONOFILAIREE0261CF18CABLE MONOFILAIRE

    FIGURE 103ELECTRICAL NOMENCLATURE

    651A2926-100

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    FIGURE 104HYDRAULIC SCHEMATIC

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    D I S A S S E M B L Y

    1. General

    This section describes the disassembly methods for galley components which may needreplacing. Sandwich structure panels are bonded and cannot be removed. In case of adamaged panel refer to the "Repairs" section of this manual.

    Note 1 : Before attempting any disassembly procedures, ensure that disassembly isnecessary. Unnecessary disassembly will reduce the life of the components.

    2. Specific component disassembly instructions

    NOTA : All operations should take place once the emptying of the system has taken place.- Place the W/P switch on the OFF position.- Open the two cocks. Let all the water drain out ( The W/T indicator light should goout).- Close the two drainage cocks.

    A. Dismantling the water heater

    - Remove it from housing.- Undo the fast action HANSEN connector.- Unscrew the electrical supply connector.

    B. Dismantling of the CONTROL PANEL and RELAY PANEL

    - Disconnect them from their supports in order to reach the hydraulic section.

    C. Dismantling of the hydraulic section

    - Dismantle the access panels Nos. 4-60, 4-90, 4-70.- Remove the fliter from its supports.- Dismantel the collars Nos. 8-210 supporting the pipe Nos. 8-80 and 8-90.- Dismantle the pipes Nos. 8-80, 8-90 and 8-50.- Dismantle the units Nos. 8-340 and 8-100.- Dismantle the pipes Nos. 8-70.- remove the pipe No. 8-40 and the T-square No. 8-340.- Disconnect the water presence sensor No. 11MC10 (non-polarized).- Loosen the fixing screws and remove them.- Undo the pump collar support and remove it.

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    D. Doors (Fig. 301)(1) Unlock latches and open doors.(2) Unscrew and remove hinge (item 1) attachment screws

    (item 2) from the structure side of the galley.(3) Remove doors.(4) Unscrew and remove hinge attachment screws

    (item 3).(5) Eventually replace the hinge spring.

    Note 2 : Each door latch is removed in the samemanner.

    (6) Unscrew and remove the two attachment screws(item 4) from one latch back plate (item 5, 6) on theinside of the door. Remove the back plate (item 7).

    (7) Retract the latch bolt, remove the latch (item 5, 6).Note 3 : Do not disassemble latches.

    E. Edging profiles

    Edges of the sandwich panels are protected by appropriate profiles and are bonded orscrewed, according to their, status to panel fields. To bond profiles, a structural adhesi-ve, softened by hot air, is used. The removal of bonded profiles is extremely delicateand should only be done if absolutely necessary.

    (1) Bonded profile(a) Heat the bonding length of the profile's exterior surface evenly with a hot air

    blower taking care to avoid the adjacent surfaces of the sandwich panel.(b) Remove the profile from the panel field at the first sign of the bonding melting.

    Use pliers with protected bits in order to avoid damaging the parts. Continueheating, little by little, and follow with the removal of the profile.

    CAUTION : THE TEMPERATURE SHOULD NOT EXCEED 105C (221F) DURINGTHE OPERATION OF A PROFILE'S REMOVAL.

    (2) Screwed profileRemoval of screwed profiles does not pose any particular problem. The profilesattaching rivet screws will be replaced systematically, after four removals, the rivetscrews having a diameter immediately superior.

    6 5 2

    1

    4

    7

    3

    Figure 301

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    F. Decorative panel (Fig. 302)The galley is equipped with removabledecorative panels. The panels are kept on theircontact surface by grooves found on the edgingprofiles.

    (1) Remove the decorative panel from the backpartition (item 1)

    (a) Remove the baseboard (item 2) from theback partition.

    (b) Using common sense, lift the back of thedecorative panel, slide it in such a waythat it loosens from the profile's grooves(item 3, 4). Remove the panel.

    (2) Remove the decorative panel from the door (Fig. 303).(a) Open the stowage compartment door.(b) Remove the door latches (item 1,2) as well

    as the profile (item 3).(c) Slide the decorative panel (item 4) until its

    upper edge is loosened from the profile'sgroove (item 5, 6 and 7).

    (d) Using common sense, lift the panel in itsmiddle using an appropriate tool (made ofwood or a plastic material) in order torelease it from its contact surface on thedoor's sandwich panel in such a way toloosen the panel's edge from the profile'sgroove. Remove the panel.

    G. Folding table

    (1) Remove the slides by pulling out the screw and the spacers.(2) Unscrew and remove hinge attachment screws from the structure side of the galley.(3) Remove the folding table.

    4

    3

    1

    2 Figure 302

    2 1 3

    6

    7

    5 4

    Figure 303

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    H. Basin ( Galley optionally fitted with basin )(1) Removal of hose

    (a) Remove the clamp by withdrawing screw, washer and nut.(b) Separate hose from couplings.

    (2) removal of basin(a) Remove lever by withdrawing screw(b) If necessary, remove equipped bung by withdrawing syphon.(c) Remove basin by withdrawing screw and washer.

    See IPL for details.

    I. Removal of upper attachments

    Note 4 : Since the principle of disassembly for different attachments is identical, thefollowing paragraphs shall only describe the disassembly of one assembly.

    (1) Remove screw and nut.(2) Remove equipped rod.(3) If necessary, remove fitting by withdrawing screw and nut.

    J. Removal of lower attachments

    Note 5 : Since the principle of disassembly for the different attachments is identical, thefollowing paragraphs shall only describe the disassembly of one assembly.

    (1) Remove screw and washer.(2) Remove the galley.(3) If necessary, remove fitting by withdrawing screw and nut.

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    C L E A N I N G

    1. GeneralThis section describes the cleaning procedures for the galley to be carried out during its usein-flight, or during scheduled on-ground maintenance. Periodic cleaning is recommended,and its interval and level is up to the operator. The cleaning products recommended areindicated in table 401.

    TABLE 401

    ITEM SPECIFICATION SOURCE

    Cleaning agent Turco Interior Cleaner TURCO-FRANCE SA3, Imp. du quai de lindustrie91200 ATHIS-MONS - FRANCEor local purchase

    Liquid disinfectant LYSOL or LYSOL SPRAY Commercially available

    Note :

    Equivalent substitutes can be used for the items listed.

    2. In-flight cleaning

    Immediately clean all spilled liquids. Wipe dry with a soft clean cloth.

    3. On-ground cleaning

    A. Ensure that all galley compartments are empty of perishable items. Vaccuum the rub-bish.

    B. Clean all interior surfaces of the galley with sponge dampened with a cleaning productaccording to manufacturers instructions. Wipe dry all cleaned surfaces with a clean softcloth.

    C. Apply the liquid disinfectant, or equivalent, as indicated in table 401, following manufac-turers instructions, on all cleaned food-handling surfaces.

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    C H E C K , C O N T R O L

    1. General

    The basic construction of the galley is simple and checks are reduced to a visual inspectionof components. An appropriate light, mirror, and magnifying glass are sufficiant for thisprocedure. It is obvious that before beginning these checks all elements must be cleaned.Any dismantled component thought to be defective will be replaced.

    2. Specific component check procedures

    A. Stowage compartment doors

    (1) Check that all doors can be opened and closed without any problem.(a) Absence of any point of resistance(b) Wear is acceptable to parts as long as it doesn't defect their function.

    (2) Check that all bolt latches engage properly in their strikes, particularly in securitylatches, ensuring their locking (green dot) and unlocking (red dot) functions.

    (3) Check the tightness of door hinge attachment screws as well as the backplates oflatch attachments.

    (4) Check the condition and function of all door hinge return springs. To repair asandwich panel refer to the "Repairs" section.

    (5) Check the condition of edging profiles and sandwich panels of doors. To repair asandwich panel see the section "Repairs". To replace an profile see the sections"Assembly" and "Disassembly".

    B. Sandwich panels

    The possible deterioration of sandwich panels are not always visible to the naked eye,in particular the deterioration of the internal structure of the panels. A simple andefficient method called the "coin test" consists of tapping different areas of the panel'ssurface with a coin. The tone heard should be clear, any different tone is a sign ofinternal deterioration or the loosening of the surface from the panel's skin. If, whenpressing moderately on the panel, the surface is soft, it is certain that an interior core ofthe panel is damaged.

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    C. Galley attachments

    The lower and upper attachments are components vital to the security of the galleyinstalled in the aircraft. No allowances will be permitted. In particular, verify the following :

    (1) The tightness of fitting attachment screws on the galley's structure.(2) The absence of cracks or traces of corrosion on fittings.(3) The wear condition on anchoring fittings of lower attachments.(4) The condition of upper attachment fitting link rods of the galley with the aircraft's

    structure.

    D. Electrical installation

    Check the condition of the isolation conduit, in particular the stops of the conduit to thecable's extremities, the efficiency of the attachment cable's binding and clamps, and theabsence of any cutting on the isolation conduit. Also check the locking system ofconnectors, the presence of electrical items and the state of bulk connectors.Refer to page 101 for testing the electrical installation.

    E. Checking

    Refer to paragraphs 2A.2B in the TESTING AND TROUBLESHOOTING.( The use of water heater is specified on its front side ). In the event of a fault, firstdetermine whether the fault is an electrical or a hydraulic one and refer to chapter 3 ofthe section DESCRIPTION AND OPERATION.

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    R E P A I R S

    I- REPAIRS OF SANDWICH PANELS

    1. GeneralRepairs described in this section concern only the repairs of sandwich panels. Theserepairs must be carried out by qualified personnel having a good knowledge of compositematerials. In particular, the environmental conditions for employing the used products mustbe respected. Good ventilation in the work area is necessary.

    CAUTION DANGER :

    Avoid inhalation of dust particles during the repairs of composite materials. Do not smoke.Wear gloves, masks and protective glasses when using these products.

    2. Necessary materials and products

    Table 601 (following page) defines the materials and products necessary for carrying outrepairs.

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    TABLE 601

    MATERIALS SPECIFICATION SOURCE VENDORCODE

    Dry fabric (1) BROCHIER 20769thickness 0.25 mm

    BROCHIER SA FRANCE14, rue Beffroy92200 NEUILLY - FRANCE

    F2991

    Resin and hardener (2) REDUX 501 CIBA-GEIGY SABP 30892506 RUEIL MALMAISONCEDEX - FRANCE

    F2605

    Honeycomb (3) NOMEX, Cell size3/16, 2 LB, CUFT

    BROCHIER SA FRANCE14, rue Beffroy92200 NEUILLY - FRANCE

    F2991

    Structural adhesive (4) REDUX 408 CIBA-GEIGY SABP 30892506 RUEIL MALMAISONCEDEX - FRANCE

    F2605

    Resin and hardener(for filling) (5)

    REDUX 255 CIBA-GEIGY SABP 30892506 RUEIL MALMAISONCEDEX - FRANCE

    F2605

    Resin and hardener(for filling) (6)

    REDUX 252 CIBA-GEIGY SABP 30892506 RUEIL MALMAISONCEDEX - FRANCE

    F2605

    Resin and hardener(for bonding) (7)

    EC2216BEC2216A

    3M FRANCEBoulevard de l'Oise95006 GERCY-PONTOISEFRANCE

    F0347

    Sandpaper (8) Medium grade General useCleaning agent (9) Ethylacetate General use

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    3. Repair procedure

    It is very important that the repair area be treated with caution. A good bonding of materialsdepends essentially on a good preparation surface. A damp test will be done on the surfaceto be bonded before application of the adhesive layer.

    A. Determining damages

    Before any reparations are done, it is necessary to locate the area to repair in order toknow if it is accessible or not, and to identify the damage characteristics (type anddimensions) for determining the degree of intervention. The damages may be allowableor repairable.

    (1) Allowable damages :No reparation - The damaged area will be checked periodically.

    (2) Repairable damages :Classed into three categories according to their importance.

    (a) Little damage :1 Surface defect (scratches, chipping) concerning the first or second layer.2 Perforated laminate.3 Separation of the sandwich structure skin.4 Non-perforated recession of the sandwich structure skin.5 Perforation of the sandwich structure having a less than 15 mm.

    (b) Extended damage :Major delamination of the panel structure.

    (c) Deterioration of honeycomb or perforation of the sandwich structure having adiameter more than 15 mm.

    Note 1 : When damage extends to the honeycomb and the damaged area is large (2500 mm

    2 ) or when the volume of filling resin is major, it will be necessary to

    replace the honeycomb.

    Note 2 : For all other noted damages, consult the vendor.

    (3) Types of repairs following damages :(a) minor repairs for small damages(b) major repairs for extended damages, the deterioration of honeycomb or the

    perforation of the sandwich structure having a diameter more than 15 mm.

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    B. Preparation of the repair area

    (1) Elimination of the surface protection :The surface protection situated in the repair area will be eliminated.CAUTION : USE ONLY MECHANICAL MEANS FOR CARRYING OUT THE

    ABOVE OPERATION. ANY OTHER MEAN IS FORBIDDEN.

    (2) Drying of the sandwich structure :All repair work will be done on a sandwich structure that is completely dry. Humiditycan be eliminated by using a hot air generator. If humidity is not completelyeliminated the honeycomb will be replaced.

    CAUTION : DO NOT EXCEED 80C (176F) DURING THE DRYING OPERA TIONOF HONEYCOMB STRUCTURE.

    (3) Damp test :This test must be carried out after each sanding or degreasing of a repair area, aswell as on a reinforcement plate that is to be placed :(a) Apply an even layer of demineralized water on the sanded or degreased area,

    or on the reinforcement plate that is to be placed.(b) Inspect the humidified area and verify that the water forms a continuous film

    without any rippling or breaking.(c) Dry with a clean cotton cloth.

    (4) Cleaning and degreasing the damaged surface :Proceed to clean and degrease the sandwich structure's damaged surface using awhite, clean, dry, lintfree cotton cloth using ethylacetate (Table 601, item 9). Use aclean portion of the cloth for each going over, before the solvent evaporates. Thecleaning is completed when the cloth remains clean.

    C. Use of adhesives

    Adhesives used for repairs of galley panels and the impregnation of dry fabrics beforebonding are composed of a base and hardener (Table 601). When prepared, themixture must be used quickly. The polymerization time depends on the environmentaltemperature and the type of resin used. The conservation time and the method ofstoring adhesives is normally indicated on their packageing.

    Note 3 : Adhesives must be stored in their original packaging in an ambiantenvironment between 5C and 10C.

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    4. Repairs

    A. Preparation of the damaged surface

    (1) Locate the damaged surface on the side of a panel and degrease it with a cottonrag dampened with ethylacetate (see paragraph 3-B-4).

    (2) Sand down the damaged surface with a medium grade abrasive paper taking carenot to cut into the adjacent structure.

    (3) Vaccuum dust particles, clean and degrease as previously indicated.B. Preparation of products

    (1) Preparation of structural adhesive Mix 100 weighed parts of REDUX 408 resin(Table 601, item 4) with 7.5 weighed parts of REDUX 408 hardener in a clean, drycontainer using a wooden or plastic spatula, until a homogeneous mixture isobtained. The pot life of the mixture is 30 min. at 25C.

    Note 4 : REDUX 408 resin can be replaced by resin EC2216 (Table 601, item 7).In such a case, mix 50 weighed parts of the base product EC2216B with 70weighed parts of accelerator EC2216A (pot life of mixture = 90 min. at24C).

    (2) Preparation of the impregnation resinMix 100 weighed parts of REDUX 501 resin (Table 601, item 2) with 15 weighedparts of REDUX 501 accelerator, in a clean, dry container using a wooden orplastic spatula, until a homogeneous mixture is obtained.

    Note 5 : The spatula that was used for mixing should not be used for spreading theproduct on the fabric.

    (3) Preparation of filling materialMix 100 weighed parts of REDUX 252 resin (Table 601, item 6) with 140 weighedparts of REDUX 252 hardener in a clean, dry container using a wooden or plasticspatula, until a homogeneous mixture is obtained. The life-time of the mixture is 20min. at 24C.

    Note 6 : REDUX 252 resin can be replaced by REDUX 255 resin (Table 601, item5). In such a case, mix 30 weighed parts of REDUX 255 with 30 weighedparts of REDUX 255 hardener.

    Note 7 : Subsequent to the work carried out, always use different spatulas, example:

    One spatula for the base resin One spatula for the hardener One spatula for the mixture One spatula for the application

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    C. Minor repairs

    (1) Surface defect concerning the first or second layer (Fig. 602)

    (a) Prepare a sufficient quantity of REDUX 255resin (see operation B-3, note 6).

    (b) Fill the surface defect cavity with the prepa-red mixture as show in Fig. 602. Flatten,let polymerize.

    (2) Perforated delaminating (Fig. 603)(a) Prepare a sufficient quantity of REDUX

    408 resin (see operation B-1)(b) Inject the prepared mixture until it dis-

    charges from the hole. Flatten, let po-lymerize.

    (3) Separation of skin from the sandwich structure (Fig. 604)

    (a) Drill holes 3 mm on the damaged area.(b) Prepare a sufficient quantity of

    REDUX 408 resin (see operation B-1).(c) inject the prepared mixture into the

    holes 3 mm until it discharges andcompletely fills the cavity as shown inFig. 604. Remove the excess mixture,flatten, let polymerize.

    5

    FIGURE 602

    4

    FIGURE 603

    4

    FIGURE 604

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    (4) Non-perforated recession of sandwichstructure skin (Fig. 605)(a) Prepare a sufficient quantity of REDUX

    255 resin (see operation B-3, note 6).(b) Spread the prepared mixture in such a

    way that it completely fills the recessedarea until it is level with the surface ad-jacent to the damaged area, as shownin Fig. 605. Let polymerize.

    (5) Perforation of sandwich structurehaving less than 15 mm (Fig. 606).(a) Prepare a sufficient quantity of

    REDUX 408 resin (see operation B-1) added with Aerosyl.

    (b) Fill the cavity with the prepared mix-ture until it is level with the surfaceadjacent to the damaged area, asshown in Fig. 606. Let polymerize.

    D. Major repairs(1) Extended delamination of the panel

    (Fig. 607)(a) Remove the damaged part of the

    sandwich structure with an excessof about 25 mm around its edge, asshown in Fig. 607.

    (b) In the fabric, prepare (Table 601,item 1) the necessary quantity ofreinforcements. Cut to the size ofthe surface that is to be repaired onthe panel.

    (c) Place the fabric reinforcements on aVac-Pac type separator film. Placeon a non-agressive surface.

    (d) Prepare a sufficient quantity of REDUX 501 resin (see operation B-2). Calculatethe weight of the resin following the formula below.

    Resin weight = Fabric weight1 - impregnation ratio

    5

    FIGURE 605

    4

    FIGURE 606

    1 2 4 25 mm

    FIGURE 607

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    (e) Impregnate the fabric of each reinforcement, with the prepared mixture, using anotched spatula. Cover the reinforcements with a second separator film correc-tly applied. Drive the air from the fabric's center towards it's exterior.

    (f) Cut the reinforcements with a template and cutter Mark on the upper separatorthe guide to give to use for the first reinforcement in order to place it on thearea to repair.

    (g) Prepare a sufficient quantity of REDUX 408 resin (see operation B-1) andspread it on the panel area to repair.

    (h) Pull out the separator film from below the first reinforcement to be placed, posi-tion the reinforcement on the repair area respecting the guide. Press lightly andpull out the separator film from above.

    (i) Place the other reinforcements as indicated above Polymerize.CAUTION : ACCOUNT FOR THE NUMBER OF SEPARATOR FILMS WHEN

    PLACING THE REINFORCEMENTS. IF A SEPARATOR FILM ISFORGOTTEN THE REPAIR IS NOT VALID.

    (2) Replacement of a honeycomb (Fig. 608)(a) Cut out the damaged part of the

    honeycomb from the panel using atrepan milling cutter. Vacuum theshavings and clean the bared surfa-ces.

    (b) Measure the depth and the of thepanels's routed part.

    (c) Prepare an insert in a honeycomb pa-nel having the same characteristicsas the damaged panel (table 601,item 3).

    Note 8 : The insert must have a morethan 10% from the measured inoperation B and a thickness more than 1 mm to the depth measured inoperation B.

    (d) Prepare a sufficient quantity of REDUX 408 resin or EC2216 resin (see opera-tion B-l) and coat the insert linings.

    (e) Prepare a sufficient quantity of REDUX 408 resin or REDUX 501 resin (seeoperation B-l) and coat the walls of the panel's cavity.

    (f) Set the insert in the panel's cavity and place it in such a way so that its honey-comb is positioned like that of the panel.

    (g) Finish off the filling between the insert and the panel using the rest of theREDUX 408 or REDUX 501 resin. Flatten and polymerize using a hot air gene-rator.

    54

    3FIGURE 608

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    Note 9 : If after polymerization the insert is not level with the surface neighboringthe repair on the panel, wear the nap off by sanding or make-up the dif-ference with REDUX 255 resin.

    (3) Perforation of the sandwich structure having a more than 15 mm (Fig. 608,609).Remove the damaged part of the sandwich structure and proceed to replace thehoneycomb as well as place the fabric reinforcements as indicated in operations 1and 2. Follow the said case, the repair will be done as shown in Fig. 609 or 610.

    1 2 4 25 mm

    3

    1

    3

    2 4

    3

    1 2 4

    FIGURE 609 FIGURE 610

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    A S S E M B L Y

    1. General

    The assembly of the galley's mechanical elements does not produce any particularproblems. The Illustrated Parts List shows the details of attachments and the stacking ofparts. The goal of the following section is to provide recommendations for the assembly ofbonded profiles, latches for doors and decorative panels, and to give storage instructionsfor the galley. The necessary tools are those normally used in workshops. Table 701 gives alist of the products used.

    2. Necessary materials and products

    TABLE 701

    ITEM SPECIFICATION SOURCE VENDORCODE

    Structural adhesive EC2216 B/A 3M MBHGeorg.-Wilh. Str. 183-1852102 Hamburg 93 Germany

    D0551

    Silicone sealant(transparent)

    RTV - 108 General Electric TechnicalServiceGroep Stroombaan 4, 1181 VXAmstelveen, Netherlands

    H6274

    Cleaning agent Ethylacetate Commercially available

    Tape 3M 9485 3M MBHGeorg. -Wilh. Str. 183-1852102 Hamburg 93 Germany

    D0551

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    3. Specific component assembly instructions

    A. Bonded profile

    (1) To ensure that the profile surfaces to be bonded and those opposite of the galleypanel are well cleaned, degrease with a clean, lint-free cloth using Trichloroethane.

    (2) Prepare the structural adhesive as indicated in the "Repairs" section.(3) Spread a thin coat of adhesive on the surfaces of the profile and the panels that are

    to be bonded, using a spatula or suitable brush.(4) Assemble the profile on the panel so that it is well aligned with the field that is to be

    covered with the panel.

    Note 1 : For decorative panel support profiles ensure that the groove existing on oneside of the profile is situated on the face side of the galley panel raising thedecorative panel.

    B. Stowage compartment door latches (Fig. 702)Note 2 : Placing latches on stowage compartment doors should be done as shown in

    Fig. 702.

    Note 3 : Since the principle of various latch installations is identical, the followingparagraph shall describe only the installation of one door.

    (1) Mount latch (item 1) on the door's upper side.(2) Mount security latch (item 2) on the door's lower side.

    2 1

    FIGURE 702

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    C. Decorative panel

    (1) Back partition decorative panel (Fig.703).

    (a) Slide the decorative panel (item 1)under the profile grooves (item2,3)

    (b) Replace the baseboard (item 4).(2) Upper stowage compartment door

    decorative panel (Fig. 704).Note 4 : Since the principle of installation

    for the various door decorativepanels is identical, the followingparagraphs shall describe onlythe installation of one doorpanel.

    (a) Remove the latches (item 1, 2) (Seesection "Disassembly")

    (b) Remove the profile (item 3) from the loweredge of the door.

    (c) Slide the decorative panel (item 4) underthe profile grooves (items 5,6,7 and 8).

    (d) Replace the profile (item 3) and thelatches (item 1, 2) on the door. (Seeparagraph 3.B.)

    3

    2

    1

    4 FIGURE 703

    2 1 3

    5

    8

    7 4

    6

    FIGURE 704

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    D. Installation of lower attachment

    Note 5 : Since the principle of assembly of the different attachments is identical, thefollowing paragraphs shall describe only one assembly.

    (1) If necessary, install and secure fitting using screw and nut.(2) Secure fitting using screw and washer.

    E. Installation of upper attachment

    Note 6 : Since the principle of assembly of the different attachments is identical, thefollowing paragraphs shall describe only one assembly.

    (1) If necessary, secure fitting using screw and nut.(2) Installed equipped rod and secure using screw and nut.

    F. Basin

    (1) Secure basin using screw and washer.(2) Install and secure lever using screw tightening yoke.(3) Install hose on coupling.(4) Secure hose using clamp, screw, washer and nut.

    G. Folding table

    (1) Install hinge attachment screws.(2) Install slides using spacers and screw.(3) Verify that the table functions well.

    H. Piping and tank

    - Fit the reduction adaptors No. 8-360 to the pump.- Place the pump in its collar.- Place the tank in its housing.- Fit the reduction adaptors Nos. 8-300 onto the filter.- Insert the pipe No. 8-40 and fix it onto the T-square No. 8-340.- Fit the pipe No. 8-110 between the T-square and the adaptor at the pump inlet.- Fit the reduction adaptor No. 8-350 onto the pipe No. 8-100.- Attach the pipe No. 8-70 onto the T-square.- Prepare units Nos. 8-60, 8-340 and 8-100.- Place the collar No. 8-180 onto the pipe No. 8-60.- Position and fix units Nos. 8-360, 8-340, 8-100 and 8-180.- Position the filter with the help of its collar.- Place the collar No. 8-210 onto the pipes No. 8-80 and 8-90.

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    - Fix the pipes No. 8-80 and 8-90.- Attach the cocks No. 8-370 onto the pipe No. 8-80 and 8-90.- Pass the water heater connector and the cable wich extends as far as the seal in the

    notch behind the pump.- Attach the pipe No. 8-60 onto the reduction adaptor.- Attach the pipe No. 8-40 onto the tank.- Tighten the filter collar.- Check the fixing.

    I. Assembling the water heater

    - Place the water heater in its housing.- Connect the water inlet and the electrical convector.- Fasten the water heater in position.

    J. Electrical connections

    - Attach the transformer No. 10MC1 on top of the galley.- Attach the control panel.- Attach the relay panel.

    Replace the acces panels.

    4. Storage

    Clean the galley as indicated in the "Cleaning" section.

    Place the galley in a container. Enclose silicagel sachets to absorb moisture and preventcorrosion.

    Store the container upright in a clean, dry place. Periodically check the condition of thesilicagel sachets.

    Shelf life : No shelf life limits.

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    S P E C I A L T O O L S A N D E Q U I P M E N T

    1. General

    No special tools, fixtures or equipment are required for the maintenance or overhaul that isto be done on the galley unit. Standard tools are sufficient for these operations.

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    I L L U S T R A T E D P A R T S L I S T

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    I N T R O D U C T I O N

    1. General

    The illustrated Parts List (IPL) intends to show the details of the equipment and permitseasy provisioning of the spares necessary for the maintenance of this galley unit.

    2. Material arrangement

    This IPL include the following sections.

    A. Introduction

    The introduction contains all explanatory information for the individiual sections as isnecessary for use of this IPL. The introduction further contains a list of abbreviationsused in the detailed parts list as well as a list of manufacturer names and addresses.

    B. Alphanumerical Index

    This section contains a listing of part numbers of all items listed in the detailed parts listin alphanumerical sequence with cross reference to respective fig/item numbers as wellas quantity per assy.

    The order of precedence in beginning the part number arrangement at the extreme lefthand (first) position is as follows: letters A through Z numerals 0 through 9

    For subsequent rows, the order is:

    a dash letters A through Z numerals 0 through 9

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    C. Detailed Parts List

    (1) Column FIG/ITEMThe first number in the first line of a page indicates the number of the figureillustrating the part, the second number indicates the item number by which the partis identifiable on the illustration. A dash placed before the item number indicatesthat the part number is not illustrated.

    (2) The Part Number column contains the original manufacturer part number. Whenstandard parts are used, the standard part number is listed in this column.

    (3) Column AIRLINE PART NUMBERThis column is left blank for airline internal use.

    (4) Column NOMENCLATURE(a) Identure system

    The identure system shows the relationship of parts and assemblies to nexthigher assemblies of installation as follows :

    1234567Installation Detail parts for installation.Assembly.Attaching parts for assembly XXX..Detail parts for assembly..Sub-assembly..Attaching parts for sub-assembly XXX...Detail parts for sub-assembly...Sub-sub-assembly...Attaching parts for sub-sub-assembly XXX Detail parts for sub-sub-assembly etc.

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    b) Attaching partsAttaching parts shall be listed immediately below the assembly which theyattach and preceding any detail parts of said assembly. They shall be listed inthe same column as the assembly which they attach and shall be captioned"ATTACHING PARTS". The XXX symbol shall follow the last item of theattaching parts as shown above.

    (c) Vendor CodeParts manufactured by companies other than COMPOSITES AQUITAINE areidentified by an appropriate vendor code shown at the end of the line.

    (d) Effectivity CodeThe applicability of main assemblies to the various sub-assemblies to mainassemblies is indicated by a code letter in the EFF. CODE column.

    3. How to use the Parts List

    A. When the part number is known :

    (1) Turn to the numerical index and locate the part number.(2) Figure and item number on the illustration where the part appears are listed in the

    column to the right of the part number.

    (3) The corresponding item number in the accompanying parts list will give partnumber, description, assembly relationship and quantity required for that particularapplication.

    B. When the part number is not known

    (1) Look through the illustrations and find the assembly of which the component ispart, or look through the illustrations and identify the part by appearance. Note theitem number in the accompanying parts list to find part number, description andquantity required for that application.

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    4. List of abbreviations

    The following abbreviations have been used in this IPL :

    AR As required

    ASSY Assembly

    DET. Detail

    FIG. Figure

    IPL Illustrated Parts List

    NHA Next Higher Assembly

    NP Not Procurable

    RF Reference

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    L I S T O F V E N D O R S

    CODE VENDOR

    D0680 CAMLOC GMBHINDUSTRIE STRASSE 6 POSTLUCH 1180 6233 KELKHEIM GERMANY

    F0022 MINILAMP ASTARA SARLZI DE LA BOURIETTE 11000 CARCASSONNE FRANCE

    F0110 AFNORTOUR EUROPE 92080 PARIS LA DEFENSE CEDEX FRANCE

    F0214 E.C.E.BP 113 75960 PARIS CEDEX 20 FRANCE

    F0409 ERCAAEROPORT VICHY-CHARMEIL 03110 CHARMEIL CEDEX 449 FRANCE

    F0564 PLASTICS OMNIUM SABP19 AVENUE JULES CARTENET 69007 LYON FRANCE

    F4492 AVDEL SA33 BIS RUE DES ARDENNES 75019 PARIS FRANCE

    F5442 AEROSPATIALE (STE NATIONALE INDUSTRIELLE) SA. "STANDARD ASN"(AEROSPATIALE NORMALISATION)12, RUE PASTEUR 92150 SURESNES - FRANCE

    F6409 TITEFLEX22 AVENUE MAURICE CHEVALIER BP7377833 OZOIR LA FERRIERE CEDEX - FRANCE

    F7885 TECNIFLEX WITZENMANNBP 94 - AERODROME DE LOGNESEMERAINVILLE - 77314 MARNE LA VALLEE CEDEX

    31746 CANNONWOOD BERRY TN U.S.A.

    32042 MICROPUMP CORP1402 NE 136TH AVE - VANCOUVER WA 98684-0818 - USA

    52607 ACTRON MFG INC.3800 E MIRA LOMA AVE. ANAHEIM CA 92806 U.S.A.

    80205 NATIONAL AEROSPACE STANDARDS COMMITTEE AEROSPACEINDUSTRIES ASSOCIATION OF AMERICA INC

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    CODE VENDOR1250 EYE ST NW WASHIGTON DC 20005 U.S.A.

    80477 ADAMS-RITE MFG CO540 W CHEVY CHASE DR GLENDALE - CA 91204 - USA -

    86735 B/E AEROSPACEGALLEY PRODUCT GROUP11710 CENTRAL PARKWAYJACKSONVILLE, FLORIDA 32224-7626

    88044 (A.N.) AERONAUTICAL STANDARDS GROUP-DPT OF NAVY AND AIRFORCESILVER SPRINGS MD - U.S.A.

    96906 MILITARY STANDARDS PROMULGATED BY MILITARY DEPARTMENTSUNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL4120 3-M - DIRECTOR OF LOGISTIC SERVICES - U.S.A.

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    A L P H A N U M E R I C A L I N D E X

    PART NUMBER AIRLINEPART NO

    FIG. ITEM TTLREQ

    A20001-1-15 9 250 1A20019-13 9 220 1A22124-01 10 240 1A35520-1R 3 400 4

    4 208 414 230 114 260 114 320 215 530 2

    A35522-1R 3 401 1A35567-3 3 403 1

    5 145 115 430 1

    A35568-1 3 402 15 144 115 420 1

    AC-2-1DAL 16 190 1AL-21SG 16 -195 1ASNA0078A503 2 -110 ARASNA2135-020 8 140 3

    16 480 4ASNA2136-020 8 390 2

    10 230 116 460 3

    ASNA2313-16 15 590 2ASNA2313-16B 4 195 2

    14 200 1ASNA2397-10L 2 -270 4

    2 -300 23 460 194 223 345 141 237 -250 38 -30 68 -170 18 -200 28 -240 28 -290 410 -270 212 163 5713 -90 413 -140 AR14 -40 214 -300 214 -350 615 130 14

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    PART NUMBER AIRLINEPART NO

    FIG. ITEM TTLREQ

    15 410 415 510 216 -160 2

    ASNA2397-416L 3 461 537 -110 4

    ASNA2397-516L 6 -150 67 -70 2

    ASNA2397-6L 12 157 7ASNA2397-8L 4 221 2

    10 -340 616 -150 2

    ASNA3288-1158 16 230 ARASNA3597-3616 13 -160 ARASNA3623-6308 9 -95 AR

    13 -170 ARBF01-0516C 2 -90 AR

    2 -150 AR9 -210 310 -310 AR

    E0512A12 12 150 1FLEX MH2D 13 05-73 16 490 1FLEX MH6 13 107-127 8 380 1LL5N 10 -40 3MP2-AX 8 -260 1MS1916-6-4 8 350 2MS20426AD3-4 9 -50 3MS21042-3 12 165 2MS35650-302 8 -230 2

    10 -120 116 -400 2

    NAS1096-2-15 4 216 2NAS1096-2-6 16 -140 2NAS1096-3-12 7 240 3

    12 160 22NAS1096-3-13 10 -110 1NAS1096-3-14 4 219 2

    8 -160 114 -30 216 -410 3

    NAS1096-3-15 15 570 1NAS1096-3-16 16 -170 2NAS1096-3-19 12 161 1NAS1096-3-23 12 162 1NAS1096-3-4 2 -280 4

    2 -310 23 430 54 224 325 151 48 -20 68 -190 2

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    PART NUMBER AIRLINEPART NO

    FIG. ITEM TTLREQ

    8 -280 412 173 613 -150 AR14 -310 214 -360 615 400 416 -390 29

    NAS1096-3-5 3 431 145 140 2310 -260 212 155 2213 -80 415 120 1415 150 316 -420 2

    NAS1096-3-7 8 -220 213 -110 116 -380 2

    NAS1096-3-8 12 158 20NAS1096-3-9 12 159 2NAS1102-06-3 9 -160 8NAS1102-06-4 2 -190 AR

    2 -220 AR9 -40 39 -170 811 30 9

    NAS1102-06-5 3 420 3NAS1102-06-6 11 40 9NAS1102-06-7 9 -240 2

    9 -270 212 152 4

    NAS1102-3-10 3 425 25 148 615 20 215 280 4

    NAS1102-3-12 4 227 214 -220 1

    NAS1102-3-13 5 150 412 186 215 30 2

    NAS1102-3-14 4 220 3NAS1102-3-4 4 210 8

    4 218 35 149 614 -60 315 50 615 170 315 370 315 470 1215 600 2

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    PART NUMBER AIRLINEPART NO

    FIG. ITEM TTLREQ

    16 -430 20NAS1102-3-5 3 421 18NAS1102-3-6 1 -170 3

    3 422 35 146 911 80 415 260 315 340 6

    NAS1102-3-7 3 423 14 213 34 217 35 147 414 -80 315 240 315 300 1

    NAS1102-3-8 3 424 8NAS1102-4-14 7 220 ARNAS1102-4-16 3 428 6

    5 142 615 190 6

    NAS1102-4-18 7 30 AR7 -160 AR7 190 AR

    NAS1102-4-20 6 30 76 -70 106 -110 15

    NAS1102-4-22 5 153 215 320 2

    NAS1102-4-5 3 426 40NAS1102-4-6 7 140 6NAS1149D0332H 1 -200 10

    13 -20 313 -50 4

    NAS1303-1 10 -30 3NAS1304-12 5 155 2

    7 -100 415 500 2

    NAS1304-14 3 433 4NAS1305-12 7 -60 2NAS1612-6 8 -310 2NAS600-5 12 151 2NAS601-10P 12 184 2NAS601-15P 12 156 5NAS602-10 3 434 5

    4 222 314 -330 215 540 2

    NAS602-4P 10 -330 6NAS603-4 1 -190 10NAS603-6 13 -30 3

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    PART NUMBER AIRLINEPART NO

    FIG. ITEM TTLREQ

    13 -60 4NAS6604-6 3 432 1NAS6605-4 6 140 6NAS679A06 12 183 1NSA5050-3 6 -40 7

    6 -80 106 -120 1512 185 2

    NSA5050-4 3 450 75 143 87 -40 AR7 -120 47 -170 AR7 -200 AR7 -26015 200 615 520 2

    NSA5050-5 7 -80 2NSA5319-06-010 10 -80 1NSA55132-020 4 225 12

    14 -380 3NSA55144-101 4 226 12

    14 -390 3NSA55148-008 16 330 6NSA55150-001 16 -340 6NSA5516-06N 8 180 2NSA5516-10N 8 210 2

    16 -370 3NSA5516-30ND 10 250 2NSA5527-03-02 12 171 2NSA5527-03-05 12 170 11NSA855163-4C 8 340 2NSA935504-01 12 172 9NSA935807-06 12 166 7NSA935807-10 12 167 8NSA935807-12 12 168 14NSA935807-20 12 169 7NSA935808-01 12 164 32PFA-T6-062 16 200 ARS-4-RS-2V 16 -220 1SS-43GS6 16 240 1SS-600-1-4 16 300 1SS-600-1-4RS 16 210 1SS-600-2-6ST 16 260 1SS-600-3 16 250 2SS-600-5-6ST 16 270 1SS-600-9 16 280 4SS-600-A-6ANF 16 290 2SS-601-PC 16 350 112S1-9-1BB 12 154 3

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    PART NUMBER AIRLINEPART NO

    FIG. ITEM TTLREQ

    2-KL16 8 330 12-KL16 16 310 125525500625 8 370 225525500625 16 320 25S3-2 12 153 3651A0010207-201 5 112 1651A0010207-201 15 110 1651A0010208-201 5 118 1

    15 220 1651A0010209-200 3 236 1

    5 129 115 390 1

    651A0010209-201 5 128 115 380 1

    651A0011205-005 5 103 115 10 1

    651A0011208-201 5 105 1651A0011208-203 15 60 1651A0011216-200 5 106 2

    15 70 1651A0011228-001 5 114 1

    15 160 1651A0011228-002 5 127 1

    15 360 1651A00A0-002 1 40A 1

    5 -1 RF651A00A0-003 1 40B 1

    15 -1 RF651A00A003-200 5 110 1

    15 80 1651A00A003-201 15 90 1651A00A009-000 5 104 1651A00A009-014 15 40 1651A00A014-000 15 450 1651A00A022-200 15 610 1651A00A100-000 15 560 1651A00D0240-000 12 10 1651A0110216-201 4 161 1

    14 110 1651A0200237-200 4 130 1

    8 150 115 580 116 360 3

    651A0200239-200 4 131 114 -240 1

    651A0200239-201 14 -270 1651A0210205-200 3 220 1

    5 116 115 180 1

    651A0210210-200 10 280 1

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    PART NUMBER AIRLINEPART NO

    FIG. ITEM TTLREQ

    651A0210211-200 5 120 115 250 1

    651A0210212-200 10 290 1651A0300205-000 4 105 1651A0300216-200 4 116 2651A0300224-000 4 124 12

    14 340 3651A0300226-200 4 126 2

    15 460 316 110 3

    651A0300227-200 4 127 114 290 1

    651A0300253-200 4 153 1651A0300254-200 4 154 1

    14 130 1651A0300256-200 4 156 1

    14 120 1651A0300257-200 4 157 1651A0300258-200 4 158 1651A0300259-200 4 159 2651A0300260-200 4 160 1651A0300262-200 4 162 1651A0300263-200 4 163 2651A0300264-200 4 164 1651A0300265-200 4 165 2

    14 150 2651A0300267-200 4 167 1651A0513220-200 5 124 2

    15 330 2651A0600213-201 5 123 2

    15 310 2651A0600213-204 3 258 2651A0600214-200 5 121 2

    15 270 2651A0600230-000 16 90 6651A0610218-200 4 169 1

    14 180 1651A0700205-200 12 11 1651A0700206-200 12 15 1651A0700207-200 12 14 1651A0700208-200 12 12 2651A0700209-200 12 13 1651A0700210-200 12 9 1651A0700211-200 12 16 4651A0700212-200 4 119 2

    14 100 2651A0D00-000 1 30A 1

    4 -1 RF651A0D00-001 1 30B 1

    14 -1 RF

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    PART NUMBER AIRLINEPART NO

    FIG. ITEM TTLREQ

    651A0D00250-200 4 155 114 140 1

    651A0D00251-200 4 166 114 160 1

    651A1000207-001 9 -100 1651A1000212-200 2 -180 1651A1000212-201 2 210 1651A1000220-200 11 110 2651A1000221-200 11 150 1651A1000224-200 11 50 1651A1000227-200 9 120 1651A1000227-201 9 80 1651A1000229-200 9 110 1651A1000230-200 9 130 1651A1000232-000 2 30 1651A1000233-200 2 20 1651A1000237-200 4 168 1

    14 170 1651A1000246-200 2 170 1651A1000246-201 2 200 1651A1000247-200 9 10 1651A1000248-200 2 70 2651A1000249-200 9 70 1651A1000251-001 4 129 2

    14 20 2651A1000252-200 9 230 1

    9 260 1651A1000255-000 13 100 5651A1000256-200 13 70 1651A1000257-000 13 120 1651A1000258-200 7 10 1651A1000262-200 11 10 1651A1000263-200 9 20 1651A1000264-200 9 140 1651A1000268-000 11 130 1651A1000270-000 9 90 1651A1000274-200 2 140 2651A1000274-201 10 300 1651A1000276-200 9 200 1651A1000277-200 11 180 1651A1000277-201 11 60 1651A1000282-200 11 200 2651A1000283-200 11 210 2651A1000286-200 2 230 1651A1000291-000 2 260 2651A1000292-000 2 290 1651A1000293-202 1 160 1651A1000294-200 2 100 1651A1000298-200 2 -80 2651A1000300-200 11 70 2

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    PART NUMBER AIRLINEPART NO

    FIG. ITEM TTLREQ

    651A1000301-200 11 220 2651A1000302-200 11 190 2651A1000304-200 11 140 1651A1000305-200 11 160 1651A1000305-201 11 100 1651A13022-000 11 120 1651A1900253-204 4 111 1651A1900253-211 14 10 1651A1900254-011 13 10 1651A1900257-000 13 130 1651A1902-016 1 10A 1

    2 -1A RF651A1902-022 1 10B 1

    2 -1B RF651A2000205-200 12 6 1651A2001202-001 12 7 1651A2912201-200 12 4 1651A2920200-200 12 8 1651A2926-000 1 110 1

    12 -1 RF651A2926-100 12 100 1651A2926200-200 12 5 1651A2926201-200 12 3 1651A3000202-200 10 200 1651A3000207-200 10 90 1651A3000208-200 10 60 1651A3000221-200 10 210 1651A3000222-200 10 220 1651A3000250-200 10 160 1651A3000251-200 10 100 1651A3000252-200 10 140 1651A3000256-200 10 70 1651A3000257-202 10 10A 1651A3000257-203 10 10B 1651A3000258-200 10 20 3651A3003-001 1 90A 1

    10 -1A RF651A3003-006 1 90B 1

    10 -1B RF651A3003100-200 10 320 1651A4000209-200 4 128 2651A4000210-200 8 130 1651A4000224-200 8 300 2651A4000225-200 8 320 1651A4000229-200 8 360 2651A4001-001 1 70A 1

    8 -1 RF651A4001201-001 8 10 1651A4001202-000 8 40 1651A4001203-000 8 50 1

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    PART NUMBER AIRLINEPART NO

    FIG. ITEM TTLREQ

    651A4001204-000 8 60 1651A4001205-000 8 70 1651A4001206-000 8 80 1651A4001207-000 8 90 1651A4001211-000 8 100 1651A4001212-000 8 110 1651A4001213-000 8 120 1651A4002-000 1 70B 1

    16 -1 RF651A4002201-001 16 10 1651A4002201-200 16 20 1651A4002201-201 16 30 1651A4002202-201 16 40 2651A4002203-000 16 -60 1651A4002204-000 16 -80 1651A4002205-200 16 100 1651A4002206-000 16 50 1651A4002207-000 16 70 1651A4002209-000 16 440 2651A4002210-000 16 450 2651A4002211-000 16 -470 1651A4002212-200 16 130 1651A4002213-000 16 120 1651A4002214-200 16 25 1651A5101NP000A 1 80 1

    9 -1 RF651A5102-001 9 -5 1651A5110-000 9 -60 1651A5115-000 4 108 1

    14 370 1651A5116-000 4 104 1651A5117-000 4 107 1651A5118-000 4 109 1651A5121-202 6 90 3651A5122-202 6 60 2

    6 100 3651A5122-203 6 20 1651A5123-202 7 20 1651A5127-200 6 50 2651A5127-201 6 10 1651A6003-000 1 100 1

    11 1 RF651AD100201-200 3 256 1651AD100207-201 7 150651AD506-201 7 180 1651AE292002-000 12 1 1651AE292003-200 12 2 1651AJ110202-060 1 130 1651AJ110203-200 3 255 1651AJ200210-200 3 232 2

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    PART NUMBER AIRLINEPART NO

    FIG. ITEM TTLREQ

    651AJ200210-201 3 233 1651AJ200212-200 3 234 1651AJ200214-200 5 126 1

    15 490 1651AJ200216-200 3 214 4651AJ501-011 13 -1 RF651AJ501-060 1 120 1651AJ503-000 1 60 1

    7 -1 RF651AJ508-000 1 50 1

    6 -1 RF651D0110204-200 3 230 1651D0110204-201 3 231 1651D0110208-200 3 213 2651D0111207-000 3 250 2651D1000232-200 2 130 1

    3 254 1651D1000236-200 2 120 2

    3 212 44 117 214 90 215 550 10

    651D1000238-200 3 253 15 122 115 290 1

    651E1000307-200 4 125 214 -210 1

    651J1000220-200 3 200 1651J1000228-200 3 206 1651J1000241-200 3 201 1651J1100212-060 1 140 1651J1100225-200 3 204 1651J1100226-200 3 202 1651J1100227-200 3 203 1651J1100230-200 3 235 1

    5 111 215 100 1

    651J1100231-200 3 208 1651J1100239-200 3 238 1651J1100239-202 3 257 1651J1100240-200 3 237 1651J1100256-200 3 215 2651J1100258-200 3 216 2

    5 117 215 210 2

    651J1100261-000 1 180 1651J1100263-200 5 119 1

    15 230 1651J1100266-200 7 210 1651J1100270-201 5 113 1

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    PART NUMBER AIRLINEPART NO

    FIG. ITEM TTLREQ

    15 140 1651J1100280-200 3 210 1651J19009-000 1 20 1

    3 -1 RF651J19051-011 13 40 1651J19056-060 1 150 1651J19057-200 1 210 1651J19109-000 3 121 1651J19111-000 3 120 1651J19113-200 3 205 1651J19114-200 3 207 1651J19202-200 7 130 1651J19203-200 7 230 1651P0100-201 2 40 AR

    15 480 AR651P0100-202 2 50 AR651P0100-204 2 60 AR651P0400202-200 9 -150 2

    11 -20 2651P0500201-000 7 90 2651P0500208-000 7 50 1651P0800202-200 3 300 2

    4 180 214 190 1

    651P0800203-200 3 302 1651P0800208-200 3 301 1651P0800220-200 9 190 1651P0800222-200 2 320 1651P0800250-200 2 240 1651P0800255-200 4 181 1

    9 180 1651P0800263-200 11 170 1

    15 440 1651P0800265-200 5 125 1651P0800265-200 15 350 1651P1000206-200 2 160 11

    3 242 34651P1200-001 6 130 6651P1400200-200 4 122 1

    14 50 1651P1400201-200 4 123 1

    14 70 1651P1400205-203 3 211 4651P1400212-200 4 121 1651P1400213-200 4 120 1651SP0001 2 -250 AR651SP0009 11 90 2651SP0010 3 440 60651SP0012 10 50 1651SP0015 10 150 1

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    PART NUMBER AIRLINEPART NO

    FIG. ITEM TTLREQ

    651SP0016 10 190 1651SP0018 10 170 1651SP0019 10 -130 1651SP0027 3 251 2651SP0043 8 400 AR651SP0049 10 180 1651SP0050 4 211 1651SP0051 4 212 1

    14 -250 114 -280 1

    651Y0005-200 9 -30 1651Y0012-200 9 -25 1651Y0013-000 1 -240 1653A398108 1 -1A RF653A892108 1 -1B RF82773 8 250 18700 MDL 668-400-2 8 -270 18700 MDL 668-400-2 16 180 1

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    10

    30

    40

    60

    70

    80

    90

    110

    120

    130

    210

    100

    140

    20

    150160

    180

    210

    GALLEY UNITFIGURE 1

    50

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    FIG.ITEM PART NUMBER

    AIRLINEPART N0

    NOMENCLATURE1234567

    EFF.CODE

    UNITSPER

    ASSY

    1-1A 653A398108 GALLEY UNIT RF-1B 653A892108 GALLEY UNIT RF10A 651A1902-016 PRIMARY STRUCTURE

    ASSYNP A 1

    (SEE FIG.2 FOR DET.)10B 651A1902-022 PRIMARY STRUCTURE

    ASSYNP B 1

    (SEE FIG.2 FOR DET.)20 651J19009-001 PRIMARY STRUCTURE

    ASSYNP 1

    (SEE FIG. 3 FOR DET.)30A 651A0D00-000 SECONDARY UPPER

    STRUCTURE ASSYNP A 1

    (SEE FIG. 4 FOR DET.)30B 651A0D00-001 SECONDARY UPPER

    STRUCTURE ASSYNP B 1

    (SEE FIG. 14 FOR DET.)40A 651A00A0-002 SECONDARY LOWER

    STRUCTURE ASSYNP A 1

    (SEE FIG. 5 FOR DET.)40B 651A00A0-003 SECONDARY LOWER

    STRUCTURE ASSYNP B 1

    (SEE FIG. 15 FOR DET.)50 651AJ508-000 LOWER FITTING ASSY NP 1

    (SEE FIG. 6 FOR DET.)60 651AJ503-000 UPPER ATTACHMENT

    FITTING ASSYNP 1

    (SEE FIG. 7 FOR DET.)70A 651A4001-001 HYDRAULIC

    INSTALLATION ASSYNP A 1

    (SEE FIG. 8 FOR DET.)70B 651A4002-000 HYDRAULIC

    INSTALLATION ASSYNP B 1

    (SEE FIG. 16 FOR DET.)80 651A5101NP000A WASTEBIN DOOR ASSY NP 1

    (SEE FIG. 9 FOR DET.)

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    FIG.ITEM PART NUMBER

    AIRLINEPART N0

    NOMENCLATURE1234567

    EFF.CODE

    UNITSPER

    ASSY

    190A 651A3003-001 BASIN ASSY NP A 1

    (SEE FIG. 10 FOR DET.)90B 651A3003-006 BASIN ASSY NP B 1

    (SEE FIG. 10 FOR DET.)100 651A6003-000 FOLDING TABLE ASSY NP 1

    (SEE FIG. 11 FOR DET.)110 651A2926-000 ELECTRICAL

    INSTALLATION ASSYNP 1

    (SEE FIG. 12 FOR DET.)120 651AJ501-060 CAP ASSY 1

    (SEE FIG. 13 FOR DET.)130 651AJ110202-060 PANEL, DECORATIVE 1140 651J1100212-060 PANEL, DECORATIVE 1150 651J19056-060 PANEL, DECORATIVE 1160 651A1000293-202 SLIDE 1

    ATTACHING PARTS-170 NAS1102-3-6 SCREW 80205 3

    ***

    180 651J1100261-000 BASEBOARDATTACHING PARTS

    -190 NAS603-4 SCREW 80205 10-200 NAS1149D0332H WASHER 80205 10

    ***

    210 651J19057-200 BASEBOARD 1-240 651Y0013-000 WASTEBIN 1

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    40

    50

    60

    TYPE OF PROFILES

    PRIMARY STRUCTURE ASSYFIGURE 2

    160

    100

    230

    30

    170

    20

    70

    240

    140

    200

    210

    130

    120

    260

    290

    320

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    FIG.ITEM PART NUMBER

    AIRLINEPART N0

    NOMENCLATURE1234567

    EFF.CODE

    UNITSPER

    ASSY

    2

    1A 651A1902-016 PRIMARY STRUCTUREASSY

    (SEE FIG.1 FOR NHA)

    NP RF

    -1B 651A1902-022 PRIMARY STRUCTUREASSY

    (SEE FIG.1 FOR NHA)

    NP RF

    20 651A1000233-200 PROFILE 130 651A1000232-000 PROFILE 140 651P0100-201 PROFILE AR50 651P0100-202 PROFILE AR60 651P0100-204 PROFILE AR70 651A1000248-200 SHEET METAL 2

    ATTACHING PARTS

    80 651A1000298-200 JOINT 2

    90 BF01-0516C RIVET F4492 AR***

    100 651A1000294-200 ANGLE 1ATTACHING PARTS

    110 ASNA0078A503 RIVET F5442 AR***

    120 651D1000236-200 SLIDE 2130 651D1000232-200 SPOOL 1140 651A1000274-200 SHEET METAL 2

    ATTACHING PARTS

    150 BF01-0516C RIVET F4492 AR***

    160 651P1000206-200 SHOULDERED BUSHING 11170 651A1000246-200 SHEET METAL 1

    ATTACHING PARTS

    180 651A1000212-200 GASKET 1

    190 NAS1102-06-4 SCREW 80205 AR

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    FIG.ITEM PART NUMBER

    AIRLINEPART N0

    NOMENCLATURE1234567

    EFF.CODE

    UNITSPER

    ASSY

    2

    ***

    200 651A1000246-201 SHEET METAL 1ATTACHING PARTS

    210 651A1000212-201 GASKET 1

    220 NAS1102-06-4 SCREW 80205 AR***

    230 651A1000286-200 PROFILE 1240 651P0800250-200 INDICATOR PLATE 1

    ATTACHING PARTS

    250 651SP0001 RIVET AR***

    260 651A1000291-000 SUPPORT 2ATTACHING PARTS

    270 ASNA2397-10L WASHER F5442 4

    280 NAS1096-3-4 SCREW 80205 4***

    290 651A1000292-000 SUPPORT 1ATTACHING PARTS

    300 ASNA2397-10L WASHER F5442 2

    310 NAS1096-3-4 SCREW 80205 2***

    320 651P0800222-200 INDICATOR PLATE 1

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    FIGURE 3PRIMARY STRUCTURE

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    FIG.ITEM PART NUMBER

    AIRLINEPART N0

    NOMENCLATURE1234567

    EFF.CODE

    UNITSPER

    ASSY3

    1 651J19009-001 PRIMARY STRUCTUREASSY(SEE FIG.1 FOR NHA)

    NP RF

    120 651J19111-000 STOWAGE DOOR ASSY 1121 651J19109-000 CAP ASSY 1200 651J1000220-200 PROFILE 1201 651J1000241-200 PROFILE 1202 651J1100226-200 PROFILE 1203 651J1100227-200 PROFILE 1204 651J1100225-200 PROFILE 1205 651J19113-200 PROFILE 1206 651J1000228-200 PROFILE 1207 651J19114-200 PROFILE 1208 651J1100231-200 PROFILE 1210 651J1100280-200 SLIDE 1211 651P1400205-203 SLIDE 4212 651D1000236-200 SLIDE 4213 651D0110208-200 SLIDE 2214 651AJ200216-200 SLIDE 4215 651J1100256-200 SLIDE 2216 651J1100258-200 SLIDE 2220 651A0210205-200 TROLLEY FITTING 1230 651D0110204-200 ANGLE 1231 651D0110204-201 ANGLE 1232 651AJ200210-200 ANGLE 2233 651AJ200210-201 ANGLE 1234 651AJ200212-200 ANGLE 1235 651J1100230-200 ANGLE 1236 651A0010209-200 ANGLE 1237 651J1100240-200 SHEET METAL 1238 651J1100239-200 SHEET METAL 1242 651P1000206-200 SHOULDERED BUSHING 34250 651D0111207-000 SUPPORT 2251 651SP0027 STOP 2253 651D1000238-200 STOP 1254 651D1000232-200 SPOOL 1255 651AJ110203-200 SPACER 1256 651AD100201-200 SPACER 1257 651J1100239-202 SHEET METAL 1258 651A0600213-204 SPACER 2300 651P0800202-200 LABEL 20 Kg 2301 651P0800208-200 LABEL 2 Kg 1302 651P0800203-200 LABEL 60Kg 1400 A35520-1R LATCH 4

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    FIG.ITEM PART NUMBER

    AIRLINEPART N0

    NOMENCLATURE1234567

    EFF.CODE

    UNITSPER

    ASSY3

    401 A35522-1R LATCH 1402 A35568-1 LATCH 1403 A35567-3 LATCH 1420 NAS1102-06-5 SCREW 3421 NAS1102-3-5 SCREW 18422 NAS1102-3-6 SCREW 3423 NAS1102-3-7 SCREW 1424 NAS1102-3-8 SCREW 8425 NAS1102-3-10 SCREW 2426 NAS1102-4-5 SCREW 40428 NAS1102-4-16 SCREW 6430 NAS1096-3-4 SCREW 5431 NAS1096-3-5 SCREW 14432 NAS6604-6 SCREW 1433 NAS1304-14 SCREW 4434 NAS602-10 BLANCHE SCREW 5440 651SP0010 SCREW 60450 NSA5050-4 NUT 7460 ASNA2397-10L WASHER 19461 ASNA2397-416L WASHER 53

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    FIGURE 4SECONDARY UPPER STRUCTURE ASSY

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    FIG.ITEM PART NUMBER

    AIRLINEPART N0

    NOMENCLATURE1234567

    EFF.CODE

    UNITSPER

    ASSY04

    1 651A0D00-000 SEC. UPPER STRUCTURE(SEE FIG.1 FOR NHA)

    NP RF

    104 651A5116-000 DOOR TANK 1 105 651A0300205-000 PANEL SANDWICH 1 107 651A5117-000 DOOR PUMP 1 108 651A5115-000 DOOR BASIN 1 109 651A5118-000 DOOR FILTER 1 111 651A1900253-204 TANK 1 116 651A0300216-200 SLIDE 2 117 651D1000236-200 SLIDE 2 119 651A0700212-200 SLIDE 2 120 651P1400213-200 SLIDE 1 121 651P1400212-200 SLIDE 1 122 651P1400200-200 SLIDE 1 123 651P1400201-200 SLIDE 1 124 651A0300224-000 SUPPORT 12 125 651E1000307-200 SPACER 2 126 651A0300226-200 ANGLE 2 127 651A0300227-200 SUPPORT 1 128 651A4000209-200 SUPPORT 2 129 651A1000251-001 SUPPORT 2 130 651A0200237-200 SPACER 1 131 651A0200239-200 SPACER 1 153 651A0300253-200 SLIDE 1 154 651A0300254-200 PROFILE 1 155 651A0D00250-200 PROFILE 1 156 651A0300256-200 PROFILE 1 157 651A0300257-200 PROFILE 1 158 651A0300258-200 PROFILE 1 159 651A0300259-200 PROFILE 2 160 651A0300260-200 PROFILE 1 161 651A0110216-201 PROFILE 1 162 651A0300262-200 PROFILE 1 163 651A0300263-200 PROFILE 2 164 651A0300264-200 PROFILE 1 165 651A0300265-200 PROFILE 2 166 651A0D00251-200 PROFILE 1 167 651A0300267-200 PROFILE 1 168 651A1000237-200 PROFILE 1 169 651A0610218-200 PROFILE 1 180 651P0800202-200 LABEL 20 KG 2 181 651P0800255-200 LABEL 10 KG 1 195 ASNA2313-16-B STOP 2 208 A35520-1R LA