WELCOME TO TECHNICAL ORDER 00-105E-9, 1 FEBRUARY 2006

TO GO DIRECTLY TO THE TECHNICAL ORDER, CLICK ON THE CONTINUE BUTTON.

WELCOME TO TECHNICAL ORDER 00-105E-9, 1 FEBRUARY 2006, REVISION 11.

TO SEE THE SEGMENT INFORMATION CHANGE NOTICE, CLICK ON THE NOTICE BUTTON.

TO CONTACT THE TECHNICAL CONTENT MANAGER , CLICK ON THE CONTACT BUTTON.

CONTINUE

NOTICE

CONTACT

TO NAVIGATE

CLICK ON THEBOOKMARKS ANDCLICK ON THE (+)SYMBOLS, THEN

CLICK ON SUBJECTLINKS TO GO TOSPECIFIC VIEWS

IN THIS SEGMENT.

THIS IS SEGMENT 4 COVERING CHAPTER 6 TO THE C-12J.

TECHNICAL ORDER 00-105E-9 TECHNICAL CONTENT MANAGER

WRITTEN CORRESPONDENCE:

HQ AFCESA/CEXFATTN: Fire and Emergency Services Egress Manager139 Barnes Drive Suite 1Tyndall AFB, Florida 32403-5319

E-MAIL: [email protected]

INTERNET: HQ AFCESA Fire and Emergency Services PUBLIC WEB PAGE: http://www.afcesa.af.mil/CEX/cexf/index.asp Safety Supplements: http://www.afcesa.af.mil/CEX/cexf/_firemgt.asp

PHONE: (850) 283-6150DSN 523-6150

FAX: (850) 283-6383DSN 523-6383

For technical order improvements, correcting procedures, and other inquiries,please use the above media most convenient.

This page is provided to notifiy the user of any informational changes made to Technical Order 00-105E-9 in this Segment and the currentRevision. Informational changes will be referenced in the Adobe Reader’s Bookmark tool as a designator symbol illustrated as a <[C]> forquick reference to the right of the affected aircraft. The user shall insure the most current information contained in this TO is used for hisoperation. Retaining out of date rescue information can negatively affect the user’s operability and outcome of emergencies. If the user printsout pages his unit requires, the user shall print the affected page(s), remove and destroy the existing page(s), and insert the newly printedpage(s) in the binder provided for that purpose. A Master of this TO shall be retained in the unit’s library for reference, future printingrequirements and inspections.

CHAPTER AIRCRAFT PAGE EXPLANATION OF CHANGE 6 C-5 ALL File updated. 6 C-12C/D/F ALL File updated to this segment and incorporates Safety Supplement -8, dated 9 November 2005.

SEGMENT 4 INFORMATION CHANGE NOTICE

TO 00-105E-9

Chapter 6 Cover

NOTE

Chapter 6 contains emergency rescue andmishap response information for the following aircraft:

USAF C-5USAF C-7USAF (V)C-9A/CUSAF C-12C/D/FUSAF C-12JUSAF C-17AUSAF C-18USAF C-18DUSAF C-20USAF C-20HUSAF C-21USAF C-22BUSAF C-23AUSAF C-26USAF C-27AUSAF C-32AUSAF C-37AUSAF C-38AUSAF C-40USAF C-130USAF C-130JUSAF C-135USAF NC-135WUSAF RC-135S

USAF RC-135UUSAF RC-135V/WUSAF TC-135SUSAF TC-135WUSAF WC-135CUSAF WC-135WUSAF (V)C-137USAF C-141USAF NC-141AUSAF C-212USAF KC-10A

T.O. 00-105E-9

6-1. INTRODUCTION AND USE.

6-2. This section contains emergency rescue andmishap response information illustrations in alpha-numerical order relative to type and model of aircraft.This arrangement of illustrations is maintained fromChapter 4 throughout the remainder of the publica-tion.

6-3. GENERAL ARRANGEMENT.

6-4. Aircraft type designation has been positionedin the upper right corner of the horizontal illustrationfor rapid identification. Additional aids to rapid orien-tation are:

a. Recent technological advances in avia-tion have caused concern for the modern firefighter.Aircraft hazards, cabin configurations, airframe ma-terials, and any other information that would be help-ful in fighting fires, the locating and rescue of per-sonnel will be added as the information becomesavailable.

b. Suggested special tools/equipment arelisted in the upper left corner, on the Aircraft/Entrypage of each listed aircraft.

c. Procedural steps covering emergency/normal entrances, cut-ins, engine/APU shutdown,safetying ejection/escape systems, and aircrew ex-traction are outlined on the left side of each pagewith coordinated illustrations on the right.

d. Illustrations located on right side of pagesare coordinated with text by numerals and small let-ters depicting both paragraph and subparagraph onthe page.

e. Each illustration is consistently coloredand/or pattern keyed to highlight essential emergencyrescue information.

f. Details are pulled directly from the illus-tration to highlight an area, thus eliminating unnec-essary searching for desired information.

CHAPTER 6

U.S. AIR FORCE

CARGO/TANKER/TEST

AEROSPACE EMERGENCY RESCUEAND MISHAP RESPONSE INFORMATION

6-1

T.O

. 00-105E-9

C-5

C-5. AIRCRAFT PAINT SCHEME1

T.O

. 00-105E-9

C-5

C-5. AIRCRAFT DIMENSIONS

WING SPAN 222’ 8.5” (67.88 M)

HEIGHT 65’ 1.5”(19.85 M)

LENGTH: 247’ 10” (75.54 M)

CABINWIDTH 25.8’

2

T.O

. 00-105E-9

C-5

C-5.3 AIRCRAFT SKIN PENETRATION POINTS

AND SYSTEM ACCESS PANELS

ENGINE OIL TANK

ENGINE ACCESSORY SECTIONAFT OF FAN EXIT BELOW ENGINECENTERLINE (RIGHT SIDE)

LEFT ENGINESPENETRATION POINTS

RIGHT ENGINESPENETRATION POINTS

CAUTION

Avoid penetrating the engine oil tank area.This area can be a fire ignition source.

ENGINE PYLON(TYPICAL)

ACCESS PANEL TOFIRE EXTINGUISHERBOTTLES

ACCESS TOFAN AIR DUCT

ACCESS TO EBUELECTRICALHARNESSESAND PNEUMATICSYSTEMS

ACCESS TO EBU,HYDRAULICS,FUEL LINES ANDLRU HYDRUALICACCUMULATOR

IDG POWER FEEDER

PNEUMATIC

ELECTRICAL

PNEUMATICBLEEDCONTROL

DRAIN

FUEL &HYDRAULICS

FIREBOTTLES

NOTE: There are no honeycomb materials.

NOTE: A recent modification has changed the the fire bottles. (See page C-5.16.)

T.O

. 00-105E-9

C-5

C-5. AIRCRAFT SKIN PENETRATION POINTS- Continued4

TROOP DECK F.S. 1944 W.L. 345 F.S. 1999 W.L. 345

TROOP DECK F.S. 1944 W.R. 345 F.S. 1999 W.R. 345

AFT CARGO DECK F.S. 1784 W.R. 213

AFT CARGO DECK F.S. 1784 W.L. 213

FORWARD CARGO DECK F.S. 1024 W.L. 213

FORWARD CARGO DECK F.S. 1024 W.R. 213

CREW DECK AT APPROXIMATELY F.S. 700 W.R. 340

CREW DECK AT APPROXIMATELY F.S. 700 W.L. 340

T.O

. 00-105E-9

C-5

C-5.

20 940

50 370

100 115

20 680

50 595

100 415 16

150 270 13

200 195 11

300 120 7

400 95 4

500 75

600 65700 55800 50900 451000 401220 35

5 AIRCRAFT HAZARD INFORMATIONDISTANCE FROM BYPASS NOZZLE EXIT

JET WAKE TEMPERATURE

DISTANCE FROM BYPASS NOZZLE EXIT

JET WAKE VELOCITY PROFILE

HIGH FREQUENCY FAN NOISEVIBRATION, AND INGESTIONAPU EXHAUST DANGER AREA(MAIN LANDING GEAR POD)

TEMPERATURE - DEGREES FMAXIMUM THRUST TEMPERATURE

VELOCITY - MPHMAXIMUM THRUST VELOCITY

HAZARDOUS RADIATION AREAWITH RADAR OPERATING

NOTE: Dynamic pressures developed at thrust settings required to start the aircraft moving at maximum gross weight on level ramp. (EPR 1.75)

6 FT

77 FT77 FT

35 FT

EN

GIN

E D

AN

GE

R A

RE

AS

AT TA

KE

OFF P

OW

ER

FT

MP

H LB

/FT

FT

*F

T.O

. 00-105E-9

C-5

C-5.

20 340

50 65

100 60

6 AIRCRAFT HAZARD INFORMATION-Continued


JET WAKE TEMPERATURE


VELOCITY - MPHMAXIMUM THRUST VELOCITY

JET WAKE VELOCITY PROFILE


EN

GIN

E D

AN

GE

R A

RE

AS

AT ID

LE P

OW

ER

6 FT

35 FT

FT

*FM

PH

FT

80 20

52 50

39 100

35 130/170

HIGH FREQUENCY FAN NOISEVIBRATION, AND INGESTION

APU EXHAUST DANGER AREA(MAIN LANDING GEAR POD)


T.O

. 00-105E-9

C-5

C-5.7 AIRCRAFT HAZARD INFORMATION-Continued

FSS LIQUID NITROGEN OVERBOARD VENT, DANGER AREAS

LIQUID OXYGEN75 LITRES/25 LITRESRIGHT MAIN LANDING GEAR PODBETWEEN FORWARD AND AFTMAIN LANDING GEAR.

HYDRAULIC RESERVOIRS BOTHSIDES 10 GALLONS/5.7 GALLONSNEAR F.S. 1300 FORWARD ANDABOVE FORWARD MAINLANDING GEAR.

BATTERIES-CARGO COMPARTMENT RIGHT FORWARDWALL OPPOSITE THE CREW ENTRY DOOR

BILGE ACCESS DOORSENGINE OIL9.1 GALLONSEACH TANK (4)

T.O

. 00-105E-9

C-5

C-5.8 AIRCRAFT HAZARD INFORMATION-Continued

VIEW FROM TOP OF AIRCRAFT

RAM AIRTURBINE

PRESSURE FROMNO.2 ENGINE DRIVENHYDRAULIC PUMPS




HYDRAULIC SERVICECENTER NO. 2

NO.1-2 HYDRAULIC POWERTRANSFER UNIT



NO.3-4 HYDRAULIC POWERTRANSFER UNIT


NO. 2-3 POWERTRANSFER UNIT

LOCATED ONWING REAR BEAM

AIR TURBINE MOTORSAND HYDRAULIC PUMPS

HYDRAULIC RESERVOIRAND SUCTION BOOST PUMP

VIEW FROM TOP OF AIRCRAFT

T.O

. 00-105E-9

C-5

C-5.9

SPECIAL TOOLS/EQUIPMENT35 Ft. Extension “A” Frame Ladder *3/8 In. Drive Ratchet for Engine CowlingPower Rescue Saw Portable LightsFire Drill II

AIRCRAFT ENTRY ALL MODELSNOTE: Crew entry door will usually have a mechanical lock installed on the inside and entry will not be possible. Use 7LT or 7RT. (See page C-5.10 topics 1 and 2 graphics)

1. NORMAL ENTRYa. Open crew entry door control access cover.

Ensure no personnel are standing under crew door.

b. Pull the latch release handle (gray) down to pressurize the door system.c. Push crew door operate handle (black) up.NOTE: If the hydraulic system accumulator is depleted, the door can be extended by using the hydraulic hand pump located behind the crew entrance door controls access cover.d. Open aft personnel doors, No. 7LT and 7RT by pulling

handles out, rotating clockwise and push in top of doorlifting upward, to full up and locked position.

NOTE: Escape slides must be deployed from inside.

2. CREW ENTRY DOOR (INSIDE OPERATION)a. Remove the Mechanical Lock from the door.b. Pull down on the crew entrance door emergency egress handle, and push out on crew door.c. Push down and hold on control if needed, then push door open.

The crew entrance ladder may not fully extend and may be as much as 5 feet above the ground.

WARNING

WARNING

Do not attempt to fight fire through APU and ATMcompartment push-in doors during APU operation.

BATTERIES

FUEL DUMPMAST

AIR TURBINE MOTOR ANDAUXILIARY POWER UNIT(TYPICAL BOTH SIDES)

FUEL DUMPMAST

OXYGENCONVERTERS

1aCREW ENTRY DOOR(MAX HT FROM GRD 9.9 FT)

1dAFT PERSONNEL DOORS

LADDER TO TROOP COMPARTMENT

SERVICELADDER

TOTAL JP-8 FUEL:51,400 US GALS.FUEL TANK QUANTITIES ARESAME FOR BOTH SIDES

MAINTENANCEACCESS DOOR

3700

4800

42004900

42003900

WARNING

NOTE:The new APU starting batteryprovides starting power to the newAPUs. The battery provides 54 Amp-Hr, Nickel-Cadmium (Ni-Cad),located in the right side cargo bay,in the vicinity of the right APU.

NOTE:An emergency lock mechanism hasbeen redesigned for the crew doorto insure door stays locked duringflight.

T.O

. 00-105E-9

C-5

C-5. AIRCRAFT ENTRY-Continued

EXTERNAL CONTROLACCESS DOOR

HANDRAILLOCKPINASSEMBLY

HANDRAIL

LADDERSUPPORTLEGS

STAIR &LADDERASSEMBLY

STAIR &LADDERACTUATOR

STAIR & LADDERDETENT HYDRAULICACTUATOR

CREW ENTRYDOOR ASSEMBLY

CREW ENTRY DOOR AIRFRAMEOPENING AND TO FLIGHTDECK STAIRWAY

10 CREW ENTRY DOOR - EXTERNAL AND INTERNAL VIEWS LOCK HYDRAULIC ACTUATOR

SAFETY LATCH

EMERGENCYEGRESS HANDLE

ACCUMULATOR

F.S. 524

AIRFRAME OPENING

MANIFOLD COVER

CREW ENTRY DOOR CONTROL HANDLE

AFT HYDRAULIC ACTUATOR

EXTERNAL ACCESSDOOR AND CONTROLS

EXTERNAL CREW ENTRY DOOR ANDSTAIR/LADDER CONTROL MECHANISM

CREW ENTRY DOOR ANDSTAIR & LADDERHYDRAULIC MANIFOLD

FLIGHT STATION STAIR &LADDER CONTROL HANDLE

EXTERNAL VIEW INTERNAL VIEW

LATCH RELEASE HANDLE

1bLATCH

1aACCESSDOOR

1cHANDLE

LADDER

UP

NUET

DOWN

LADDERCONTROLHANDLE

T.O

. 00-105E-9

C-5

C-5.11

3aNO. 5 ESCAPE DOOR(MAX HT FROM GRD24.3 FT.)

3cNO. 7 LT AND RT AFTPERSONNEL DOORS(MAX HT FROM GRD8.7 FT.)

2fNO. 4 ESCAPE HATCH(RT SIDE ONLY, MAXHT FROM GRD 25.1 FT.)3e

NO. 6 ESCAPE DOOR(LT SIDE ONLY, MAXHT FROM GRD24.5 FT.)

3bNO. 1 ESCAPEHATCH (MAXHT FROM GRD30.6 FT.)

3bNO. 2 ESCAPE HATCH (MAX HT FROM GRD 30.6 FT.)

3dNO. 3 LT AND RT ESCAPEHATCHES (MAX HT FROM GRD 29.4 FT.)

NOTE: Heights are with landing gear in taxi or takeoff position.

3. EMERGENCY ENTRY

NOTE:• All escape doors and hatches; if jamming occurs, break guide

on top left corner of doors, doors will fall inward, then removeprior to deploying slide.

• * Bed ladder should be marked at 10th rung from bottom toindicate middle fly ladder catch location. This will extend properamount of ladder to enter doors No. 5 and 6.

• Due to fuselage curvature and wing fillets, handles No. 1, 2, 3 LT,and 3RT should not be used as primary entry points with aladder.

a. Open escape door No. 5 by pulling handle, rotating clockwiseand push in at top and lift upward, to full up and locked position.

b. Open escape hatch No. 1 and hatch No. 2 by pulling handlesand removing hatches. Hatch No. 1 is hinged. Hatch No. 2 fallsfree.

c. Open aft personnel doors No. 7LT and 7RT by pulling handlesout, rotate clockwise and push in top of door and lift upward tofull up and locked position.

d. Open escape hatches No. 3LT and 3RT (troop compartment) bydepressing lock on panel and pulling handle upward, push indoor and pull upward at bottom of door. Hatches will fall inward.

e. Open escape door No. 6 3LT and 3RT (troop compartment)service door (left side only) by pulling handle out, rotate clock-wise and push door in and lift upward to full up and lockedposition.

f. Open escape door No. 4 (right side only) by pulling handle outand down. Hatch falls inward when unlatched.

NOTE: Access cannot be gained from flight deck to the troop compartment in the upper deck and vice versa.

AIRCRAFT ENTRY-Continued

T.O

. 00-105E-9

C-5

C-5. AIRCRAFT ENTRY-Continued

3. ESCAPE SLIDE DEPLOYMENT

a. Release the quick disconnect buckle.

b. Using the assist handle(s), lift case straight upand rest bottom of case on sill of hatch.

c. Push case overboard by applying force to theupper edge of the case. The case should splitand fall. The escape slide should unfold andautomatically inflate as it falls to the ground.

d. If the case does not split or the slide does notinflate, grasp both cables attached to the girtbar, slide your hand down the cables as far aspossible and then sharply pull the cables. Theretaining straps should part, case split, and theslide inflate. If the slide does not inflate pullthe red webbing handle marked “Pull to Inflate”.

NOTE: Five (5) slides are installed, escape doors No. 5 and 6; and escape hatches No. 3LT and RT and 4.

4. DESCENT REELS

NOTE:Four descent reels are located on the upperdeck for emergency escape.

a. Remove/open either or both pilot or co-pilotwindows, using descent reels for emergencyescape.

b. Remove No. 1 escape hatch using descent reelfor emergency escape.

c. Remove the No. 2 escape hatch using descentreel for emergency escape.

ESCAPE SLIDE DEPLOYMENT

a. SLIDE DEPLOYMENT b. SLIDE INFLATION

d. SLIDE EXTENSION IN CORRECT POSITION

c. SHOULD WIND MOVE SLIDE DURING OR AFTER EXTENSION, STRAIGHTEN AS SHOWN IN 4.

12

DESCENTREELS(TYPICAL)(4 LOCATIONSILLUSTRATED)

4aFLIGHTDECKWINDOWREELS

4bNO.1 ESCAPEHATCH REEL

4cNO. 2 ESCAPEHATCH REEL

T.O

. 00-105E-9

C-5

C-5. 13

5. CUT-IN

a. Left and right side of relief crew compartment.

b. Two (2) each side of troop compartment aft of service door No. 6 and escape hatch No. 4.

c. Left and right side of forward cargo compartment forward of wheel pods.

NOTE: Access cannot be gained from flight deck to the troop compartment in the upper deck.

d. Left and right side forward of aft cargo compartment personnel doors.

NOTE: Escape slides are installed at doors 7R&L when pallet seats are on aircraft.

4aCREWCOMPARTMENT

4cFORWARD CARGOCOMPARTMENT

AIRCRAFT ENTRY-Continued4bTROOPCOMPARTMENT

4dAFT CARGOCOMPARTMENT

T.O

. 00-105E-9

C-5

C-5.14

1. ENGINE/APU SHUTDOWN

a. Pull fire emergency control T-handles, located topcenter portion of the pilot instrument panel.

NOTE: Battery switch is not required to be turned off.

b. Pull fire emergency control T-handles located onupper left corner of flight engineer control panel,to shut off both auxiliary power units.

NOTE: Fire Emergency Control T-handles for APUs are located inside crew entry door at the Fwd Load Masters Panel.

ENGINE/APU SHUTDOWN PILOT’S INSTRUMENT PANEL

ENGINE FIRE DETECTION AND EXTINGUISHING SYSTEM CONTROLS AND INDICATOR PANEL

1aPULL FIRE EMERGENCY CONTROL T-HANDLES

FLIGHTENGINEER’SCONTROLPANEL

1bAPU FIRET-HANDLES

APU FIRE EMERGENCY CONTROLT-HANDLES AT FWD LOADMASTER’S PANEL

FIRE APU PULL FIRE APU PULL

FIRE APU PULL FIRE APU PULL

APU -- LEFT SIDE FUSELAGE

REPLACEMENT APU

ENGINE THROTTLES (TYPICAL)

T.O

. 00-105E-9

C-5

C-5. MISCELLANEOUS PANELS

1. MISCELLANEOUS PANELS

NOTE: Recent modifications are changing the analog

gauges to digital on the flightdeck.

PROPULSION SYSTEM AT FLIGHT STATION PANEL

APU SWITCHES AT FLIGHT STATION PANEL

ELECTRICAL SYSTEMS AT FLIGHT STATION PANEL

ENVIRONMENTAL CONTROL/APU SWITCHES (APU CONTROL VALVE RELOCATED HERE)

15

T.O

. 00-105E-9

C-5

C-5.16

FIRE SUPPRESSION SYSTEM (FSS)

WARNING

Do not remain in a closed space with nitrogen without an oxygen mask. Nitrogenis a harmless gas, but when it occupies a closed space to the exclusion ofbreathable air it can result in suffocation of personnel.

NOTE:All C-5 aircraft have a fire detection system; FE1301 FSS, and nitrogen FSS.FE1301 FSS on C-5A aircraft is a one-shot discharge into the affected area. AllC-5B aircraft have a fire detection system and nitrogen FSS. C-5B DOES NOThave FE1301 FSS. For the C-5B aircraft, the buttons on the FSS control panelsfor occupied areas are indicator lights only, for the detection system. They willnot discharge FE1301. C-5A and C-5B nitrogen FSS can be discharged morethan once (2 of 3 times) into the same affected area if needed. For ALL C-5Aaircraft, the FE1301 FSS can be armed from the nose wheel well or the flightengineer’s control panel. The FE1301 system can be discharged only from theflight engineer’s control panel. There is a FE1301 indicator panel in the cargobay near door 7 left.

a. Nose wheel well nitrogen control panel provides fire suppression capabilities forthe left wing; right wing; under floor fwd; under floor compartments. Control panelwill be inaccessible if aircraft is encountered in a gear up crash configuration orforward kneel position, and other fire suppression methods must be employed.The FSS panel operates off the battery.

NOTE:Recent modications to the engine fire detection and suppression systemwill provide detection of fire in each engine / nacelle. Crew annunciationof fire via C-5 A/B Fire Warning Lights on FireX Panel. Crew initiation offire suppression agent located in pylon to suppress fire. Fire extinguish-ing system modification CF6 Certified to Halon 1301 replaces Halon 1202on C-5 A/B. H1301 requires new fire bottles to replace C-5 H1202 bottlesH1301 agent characteristics require short run to nacelle. Therefore 2bottles per pylon vs 2 bottles per wing. On C-5 A/B new bottles requireintegration with pylon and new distribution. Ducting to engine fire detec-tion system CF6 has unique fire detectors (Pneumatic Loops) requiring anew fire detection system. The 8 bottles per aircraft require electricalswitch change on FireX Panel in flightdeck. New engine and pylon firedetector panel – Engine/APU Fire Detection Test Panel.

PUSH BUTTONS

1aNOSE WHEEL WELL NITROGENAND FE 1301 FIRE SUPPRESSIONCONTROL AND INDICATOR PANEL

LAMP TEST

ARMINGSWITCH

PANEL SAFE

LEFTWING

RIGHT WING

UNDERFLOOR AFT

UNDERFLOOR FWD

CARGOCTRWINGAVIONICS

PANEL SAFESWITCH

1. NOSE WHEEL NITROGEN FIRE SUPPRESSION CONTROL AND INDICATOR PANEL

T.O

. 00-105E-9

C-5

C-5.17

FE 1301 FIRE SUPPRESSIONCONTROL AND INDICATOR PANEL

FLIGHT ENGINEER’S CONTROL PANEL

2a ARMING SWITCH

4b PUSHBUTTONSNITROGEN FIRE SUPPRESSIONCONTROL AND INDICATOR PANEL

FIRE SUPPRESSION SYSTEM-Continued2. NITROGEN FIRE SUPPRESSION CONTROL AND INDICATOR PANELNOTE: Nitrogen can be semi-depleted on long flights. Nitrogen gas fills the empty space of used fuel.

a. Place arming control switch, located on the FE1301 Fire Suppression Control and Indicator Panel on lower left section of flight engineer’s overhead control panel to ARM position.

NOTE: On C-5B 83-1285 and up, the fire suppression control panel is inscribed FIRE SUPPRESSION.

b. Depress discharge pushbuttons for affected area to discharge nitrogen fire suppression system.

NOTE: The twelve nitrogen discharge pushbuttons located on the nitrogen fire suppression control and indicator panel at the flight engineer’s station discharge nitrogen into their asso- ciated fire zones, as indicated in chart below. Aircraft power is required to operate this panel.

NITROGEN FIRE SUPPRESSION ZONES AND CONTROLS

(ON AIRCRAFT MODIFIED BY TO 1387)

FE 1301 FIRE SUPPRESSION

AVIONICS CTR WING CARGO

ARMED

OPTICALRESET

ARM

PANELSAFE

DISCHARGE

MANIFOLDPRESSURE

FUEL TANKPRESSURE WARNING

LEFT WING RIGHT WING

ISOCLOSED

VENTOPEN

HORN TEST

HORN SILENCE TESTMAN PRSS

DETECTIONDISCHARGE

LEFTOUTBD WING

LEFTINBDWING

RIGHT INBDWING

RIGHT OUTBD WING

RIGHT PTURIGHT MAIN WHEEL WELL

LEFT MAIN WHEEL WELL

LEFT PTU

NOSEWHEEL WELL

UNDERFLOOR FWD

UNDERFLOOR MID

UNDERFLOOR AFT

FE 1301 FIRESUPPRESSION

CARGO VOLUME SELECTOR10,000 TO 20,000 CU FT

UNDER10,000CU FT

OVER20,000CU FT

SAFEPANEL

ARM

HORNSILENCE

NORMAL

LAMP TEST

FE 1301FIRE SUPPRESSION

AVIONICS

CTR WING

CARGO

CARGO COMPARTMENT FE 1301 FSS PANEL

CARGO VOLUME SELECTOR PANEL

NITROGEN FIRE SUPPRESSION

T.O

. 00-105E-9

C-5

C-5.18

1. OXYGEN SHUTDOWN

NOTE:Manual oxygen shut-off valve should be shut offduring interior fire fighting operations or any timethe possibility of an oxygen-enriched fire occurs.The valve is normally safety-wired open, so a pairof wire cutters may be required to shutoff thevalve. The valve is located behind a small compartment door which may be covered by aircraftinsulation. Approximate location of the valve:

a) Midway through cargo compartment, left side.b) Near station #1460c) 79 ft. from normal crew entry door.d) 32 ft. from door 7L.e) 3 ft. above cargo deck.

NOTE:Hydraulic system operating pressure is 3000 PSI.Four systems are located in the walls of the cargocompartment: (1) 10 gallons on the left wall nearfuselage station 1300, just forward and above theleft forward main landing gear. (2) 5.7 gallons onthe left wall just forward of the #1 system. (3) 5.7gallons on the right wall opposite #2 system. (4)10 gallons on the right wall aft of #3 and opposite #1 system.

When landing gears are in the extended position,hydraulic lines to doors and locks are pressurized.This creates a possible hazard should lines beruptured. A ruptured condition can be identified bya high pressure mist.

WARNING

MANUALSHUT-OFFVALVE

OXYGENCONVERTERS25 AND 75 LITERS

MANUALSHUT-OFFVALVE

EMERGENCYOXYGEN SUPPLYSHUT-OFF VALVE

VALVE HANDWHEELTO BE SAFETY WIRED IN THE OPEN POSITION FORNORMAL OPERATION CLOSE VALVE IN CASE OF FIRE OR FOR MAINTENANCE

OXYGEN SHUTDOWN

THUMBLATCH

T.O

. 00-105E-9

C-5

C-5.19

PILOT’S AND COPILOT’S SEAT C-5B AF83-1285 AND UP C-5A 66-8303 - 70-0467

2aHORIZONTALADJUSTMENT

OBSERVER’S SEATC-5B AF83-1285 AND UP C-5A 66-8303 - 70-0467

SHOULDER HARNESS LOCK LEVER

LATERALADJUSTMENTCONTROL(OBSERVERONLY)

2bHORIZONTAL ANDSWIVEL ADJUSTMENTLEVERS (BOTHSEATS ALIKE)

AIRCREW EXTRACTIONNOTE:

The older, non-repairable Weber or legacy seats are beingreplaced by Ipeco seats. The newer seats will have thesame adjustment controls.

1. AIRCREW EXTRACTION CREW COMPARTMENT C-5AAF 66-8303 THROUGH 70-0467

a. Seats for NAV, ENGR, and OB, pivot and position aft.For pilot and copilot seats, push outboard.

b. Release lap belts and remove shoulder harness restraintstraps.

c. Push knob forward to move seat horizontally in track.Rotate knob clockwise to rotate seat 90 degrees left orright.

2. AIRCREW EXTRACTION CREW COMPARTMENT C-5BAF 83-1285 AND UP.

a. Move pilot’s and copilot’s seats full aft and outboard.Pull aft on horizontal adjustment lever to move the seatforward and aft and push lever toward the seat for lateralmovement.

b. Rotate navigator’s, flight engineer’s, and observer’s seat90 degrees left or right. Push down on the horizontaladjustment lever and the swivel release lever on theseats to move them horizontally and to swivel.

c. Release lap belts and remove shoulder harnesses.

NOTE:The Navigator’s seat can also be designated SpecialMission when appropriate.

PILOT’S ANDCOPILOT’S SEATS

HORIZONTALADJUSTMENT LEVER

SHOULDER HARNESS LOCK LEVER

1cHORIZONTALAND SWIVELADJUSTMENTLEVER

NAVIGATOR’S, FLIGHT ENGINEER’S, AND OBSERVER’S SEATS

NAVIGATOR’S ANDFLIGHT ENGINEER’S SEAT C-5B AF83-1285 AND UP C-5A 66-8303 - 70-0467

T.O

. 00-105E-9

C-5

C-5.

COURIER COMPARTMENT 8 CREWMEMBERS

BUNKROOMS

LADDER TOFLIGHT DECK

FLIGHT DECK

RELIEF CREW7 CREWMEMBERS

TROOP COMPARTMENT SEATING LOCATIONS UPPER-75 PEOPLE CARGO-270 PEOPLE

LADDER TO TROOP COMPARTMENT

ACTIVE CREW - 5RELIEF CREW/COURIER - 15

AIRCREW AND TROOP EXTRACTION20

SEPARATION BETWEEN FLIGHT DECK AND TROOP COMPARTMENT(NO CONNECTION BETWEEN AREAS)

3. OTHER AIRCRAFT SEATING

a. Upper level seats for crew relief and courier are equipped with lap belts only.

b. Cargo seating, when installed at lower level, are equipped with lap belts only.

T.O. 00-105E

-9

C-7

C-7.1 AIRCRAFT SKIN PENETRATION POINTS

NOTE: Penetration points are the same for both left and right engines.

ENGINE NACELLES (BOTH SIDES)11” FORWARD OF WING LEADING EDGEMEASURED 10” DOWN

CARGO/PASSENGER COMPARTMENTCENTER LEFT FUSELAGE BENEATH WING

T.O. 00-105E

-9

C-7

C-7. 2

SPECIAL TOOLS/EQUIPMENTPower Rescue Saw12 FT LadderFire Drill II

AIRCRAFT ENTRY- ALL MODELS FUEL TANK

414

414

OXYGENCYLINDERS(2)

EMERGENCYOXYGENCYLINDERS

BATTERY

BOTTOMHATCH

2bEXTERNALHANDLE

CARGO DOOR JETTISON

PASSENGERDOORS

1a, 2cEXTERNAL UNLOCKHANDLE

CUT HEREFOREMERGENCY RESCUE

2aEMERGENCYRELEASEBUTTON

1. NORMAL ENTRY

a. Press button and turn handle, located onpassenger door, counterclockwise to openpassenger doors.

2. EMERGENCY ENTRY

a. Press emergency release button and rotateexternal handle clockwise to open flight com-partment roof hatch.

b. Open hatch and pull external handle, locatedright side aft fuselage, to jettison cargo door.

c. Press button and turn handle, located onpassenger

3. CUT-IN

a. Cut-in area located beneath wing, left side offuselage.

T.O. 00-105E

-9

C-7

C-7.3 ENGINE SHUTDOWN ANDAIRCREW EXTRACTION1. ENGINE SHUTDOWN

a. Retard throttles, located on center overhead console, tofull THROTTLE CLOSED position.

b. Retard engine mixture levers, located on center overheadconsole, to IDLE CUT-OFF position.

c. Place ignition switches, located center overhead console,to OFF position.

d. Place battery master switch, located left forward electricalswitch panel, to OFF position.

2. AIRCREW EXTRACTION

a. Unlatch lap belt and remove shoulder harness fromcrewmember(s).

NOTE: The passengers seats are equipped with seat belts only. If seat’s tracks are not damaged during crash landing, use adjustable seat controls to retract seats in aft position to aid in removing crewmember(s).

1cIGNITION SWITCHES

1aTHROTTLE

1bENGINE MIXTURE LEVER

OVERHEADCONSOLE

1dBATTERY MASTER SWITCH

ELECTRICAL SWITCH PANEL

(V)C-9A/CT.O

. 00-105E-9

(V)C

-9A/C

.

AIRCRAFT PAINT SCHEME

1

(V)C-9A/CT.O

. 00-105E-9

(V)C

-9A/C

.

AIRCRAFT DIMENSIONS

2

STATICGROUNDPLANE

FUSELAGE REFERENCE PLANE

WINGSPAN

LENGTH

HEIGHT

NOTE: These dimensions are valid for all models.

(V)C-9A/CT.O

. 00-105E-9

(V)C

-9A/C

.

AIRCRAFT SKIN PENETRATION POINTS

3

FUSELAGE (BOTH SIDES)PENETRATE APPROXIMATELY 4 INCHESBELOW CABIN WINDOWS. AVOIDPENETRATING EMERGENCY EXITS.

ENGINE NACELLES (BOTH SIDES)PENETRATE MID-SECTION OF ENGINEBELOW ENGINE CENTERLINE

(V)C-9A/CT.O

. 00-105E-9

(V)C

-9A/C

.

SPECIAL TOOLS/EQUIPMENTPower Rescue Saw12 FT LadderFire Drill II

1. NORMAL ENTRYa. Pull forward entrance and service door external

handle, entrance door located on forward left fuselage, service door located on forward right fuselage, out and rotate counterclockwise to OPEN position (service door opposite).

b. Lift stairwell external door handle, located below forward entrance door, and raise to up position.

NOTE: If aircraft is shut down, auxiliary power switch under latch handle must be held in the ON position while depressing DOWN button.

c. Depress lower button marked DN to extend stairwell ladder.

d. Open rear stairway control panel, located on aftleft exterior fuselage, push control handle to

forward OPEN position to release stairway.

Stairway free falls to down position. Keep area clear.

2. EMERGENCY ENTRY

Caution must be exercised when releasing tail cone. Keep personnel clear. Tail cone free falls when re- leased from aircraft.

a. Push in jettisonable tail cone T-handle door, located on left fuselage forward of tail cone, pull T-handle to jettison tail cone. Jettison door is approximately 8.5 feet high.

b. Push overwing exit door handle release, two doors arelocated over each wing, pull handle to unlatch door,

push in and lift up forcibly.

AIRCRAFT ENTRY - ALL MODELS

WARNING

WARNING

1cEXTERNALSTAIRWELLLADDERBUTTON 1b

FWDSTAIRWELL DOOR LATCH

1aHANDLE -ENTRANCE (RH) -SERVICE DOOR (LH)

1dHANDLE REARSTAIRWAYCONTROLPANEL

EXTERIORAPUCONTROLPANEL

JETTISONABLETAIL CONE

AFT ENTRANCESTAIRWAY

2aTAIL CONEJETTISONHANDLE

2bOVERWINGEXIT DOOR

NOTE: Tail cone entrance and aft stairway cannot be used at the same time.

4

(V)C-9A/CT.O

. 00-105E-9

(V)C

-9A/C

.

ENGINE SHUTDOWN ANDAIRCREW EXTRACTION1. ENGINE SHUTDOWN

a. Pull engine fire shut-off T-handles, located on upper portion of instrument panel.

b. Place APU fire control switch, located on over-head switch panel, to OFF and AGENT ARM

position.

c. Place battery switch, located below APU control panel to OFF position.

d. Main oxygen shutoff valves (2 each; 1- crew oxygen and 2- passenger oxygen). Valves are painted red and located 15-1/2” above flightdeck floor.


a. Raise (ACM) additional crewmember seat, located in doorway of crew cabin, for access to cabin.

b. Pull seat lock knobs, located left side seat, inward and raise seat to wall of cabin.

c. Raise pilot’s armrest as necessary.

d. Unlatch lap belt and remove shoulder harness from crewmember(s).

NOTE: If seat tracks are not damaged during crash

landing, use adjustable seat control handle to retract seat to aft position.

1bAPU SWITCH

1cBATTERYSWITCH

EMERGENCY ANDTHERAPEUTICOXYGEN LOW LIGHT

EMERGENCY AND THERAPEUTIC OXYGEN SHUTOFF VALVES

PILOT’SOXYGENMASK HOSECONNECTION

1aENGINE FIRESHUT OFFT-HANDLES

2dSHOULDERHARNESS STRAPS

2dLAP BELT

2cARMREST

PILOT’SSEAT

2aACMSEAT

2bSEATLOCKKNOBS

THROTTLES

5

(V)C-9A/CT.O

. 00-105E-9

(V)C

-9A/C

.

CABIN CONFIGURATIONS1. CABIN CONFIGURATION FOR INTERIOR ARRANGEMENT - 40 AMBULATORY PATIENT6

1 FLIGHT COMPARTMENT 15 AFT LOWER CARGO COMPARTMENT DOOR 28 CENTRAL STOWAGE COMPARTMENT:2 CREW STOWAGE 16 FORWARD LOWER COMPARTMENT DOOR LITTERS, PILLOW, ETC3 SERVICE DOOR 17 FORWARD LOWER CARGO COMPARTMENT 29 LITTER PATIENT RAMP4 STANCHION - SPECIAL CARE AREA 18 FORWARD GALLEY 30 LITTER PATIENT DOOR5 SPECIAL CARE AREA 19 WASTE CONTAINER 31 WEATHER CURTAIN6 UTILITY STANCHION - SPECIAL CARE AREA 20 SPECIAL CARE AREA PATIENT’S LITTER 32 DOOR AND RAMP CONTROL CONSOLE7 MEDICAL STOWAGE 21 MEDICAL CREW DIRECTOR’S DESK 33 COATROOM8 MEDICAL CREW DIRECTOR’S SEAT 22 AMBULATORY PATIENT’S SEAT 34 WORK TABLE, MEDICAL BOTTLE RACK,9 MEDICAL CREW SEAT 23 CURTAIN MISCELLANEOUS STOWAGE10 AMBULATORY PATIENT’S SEAT 24 STOWAGE AND WASTE CONTAINERS 35 MEDICAL SINK11 AFT LAVATORY 25 AFT ENTRANCE DOOR 36 FORWARD LAVATORY12 AFT STAIRWAY DOOR 26 AFT STAIRWAY 37 FORWARD STAIRWAY13 SENIOR AEROMEDICAL TECHNICIAN’S SEAT 27 AFT GALLEY 38 FORWARD ENTRANCE DOOR14 AFT LOWER CARGO COMPARTMENT 39 DOUBLE SEAT FOR ADDITIONAL

MEDICAL CREW MEMBERS

1 2 3 4 5 6 7 8 7 9 10 11

17 16 15 14 13 12

1 2 18 3 19 20 9 8 21 22 9 23 24 11 25

39 31 38 37 36 35 34 33 32 31 30 29 28 9 27 26

(V)C-9A/CT.O

. 00-105E-9

(V)C

-9A/C

.

CABIN CONFIGURATIONS - Continued

7

1. CABIN CONFIGURATION FOR INTERIOR ARRANGEMENT - 30 LITTER PATIENT

1 FLIGHT COMPARTMENT 15 AFT LOWER CARGO COMPARTMENT DOOR 29 CENTRAL STOWAGE COMPARTMENT:2 CREW STOWAGE 16 FORWARD LOWER CARGO COMPARTMENT DOOR LITTERS, PILLOW, ETC.3 SERVICE DOOR 17 FORWARD LOWER CARGO COMPARTMENT 30 LITTER PATIENT RAMP4 STANCHION - SPECIAL CARE AREA 18 FORWARD GALLEY 31 LITTER PATIENT DOOR5 SPECIAL CARE AREA 19 WASTE CONTAINER 32 WEATHER CURTAIN6 UTILITY STANCHION - SPECIAL CARE AREA 20 SPECIAL CARE AREA PATIENT’S LITTER 33 DOOR AND RAMP CONTROL CONSOLE7 MEDICAL STOWAGE 21 MEDICAL CREW SEAT 34 COATROOM8 MEDICAL CREW DIRECTOR’S SEAT 22 MEDICAL CREW DIRECTOR’S DESK 35 WORK TABLE, MEDICAL BOTTLE RACK,9 STANCHION 23 PATIENT’S LITTER MISCELLANEOUS STOWAGE10 UTILITY STANCHION 24 CURTAIN 36 MEDICAL SINK11 AFT LAVATORY 25 STOWAGE AND WASTE CONTAINERS 37 FORWARD LAVATORY12 AFT STAIRWAY DOOR 26 AFT ENTRANCE DOOR 38 FORWARD STAIRWAY13 SENIOR MEDICAL TECHNICIAN’S SEAT 27 AFT STAIRWAY 39 FORWARD ENTRANCE DOOR14 AFT LOWER CARGO COMPARTMENT 28 AFT GALLEY 40 DOUBLE SEAT FOR ADDITIONAL

MEDICAL CREW MEMBERS

1 2 3 4 5 6 7 8 7 9 10 11

17 16 15 14 13 12

2 8 3 19 20 21 8 22 23 21 24 25 11 26

40 32 39 38 37 36 35 34 33 32 31 30 29 21 28 27

(V)C-9A/CT.O

. 00-105E-9

(V)C

-9A/C

.


8

1. CABIN CONFIGURATION FOR INTERIOR ARRANGEMENT - 18 LITTER PATIENT AND 20 AMBULATORY PATIENT

1 FLIGHT COMPARTMENT 16 AFT LOWER CARGO COMPARTMENT DOOR 31LITTER PATIENT RAMP2 CREW STOWAGE 17 FORWARD LOWER CARGO COMPARTMENT DOOR 32 LITTER PATIENT DOOR3 SERVICE DOOR 18 FORWARD LOWER CARGO COMPARTMENT 33 WEATHER CURTAIN4 STANCHION - SPECIAL CARE AREA 19 FORWARD GALLEY 34 DOOR AND RAMP CONTROL CONSOLE5 SPECIAL CARE AREA 20 WASTE CONTAINER 35 COATROOM6 AFT STANCHION - SPECIAL CARE AREA 21 SPECIAL CARE AREA PATIENT’S LITTER 36 WORK TABLE, MEDICAL BOTTLE RACK,7 MEDICAL STOWAGE 22 MEDICAL CREW SEAT MISCELLANEOUS STOWAGE8 MEDICAL CREW DIRECTOR’S SEAT 23 MEDICAL CREW DIRECTOR’S DESK 37 MEDICAL SINK9 FORWARD STANCHION 24 PATIENT’S LITTER 38 FORWARD LAVATORY10 UTILITY STANCHION 25 CURTAIN 39 FORWARD STAIRWAY11 AMBULATORY PATIENT’S SEAT 26 STOWAGE AND WASTE CONTAINERS 40 FORWARD ENTRANCE DOOR12 AFT LAVATORY 27 AFT ENTRANCE DOOR 41 DOUBLE SEAT FOR ADDITIONAL13 AFT STAIRWAY DOOR 28 AFT STAIRWAY MEDICAL CREW MEMBERS14 SENIOR MEDICAL TECHNICIAN’S SEAT 29 AFT GALLEY15 AFT LOWER CARGO COMPARTMENT 30 CENTRAL STOWAGE COMPARTMENT:

LITTER, STOWAGE, ETC.

1 2 3 4 5 6 7 8 7 9 10 11 12

18 17 16 15 14 13

2 19 3 20 21 22 8 23 24 22 25 26 12 27

41 33 40 39 38 37 36 35 34 33 32 31 30 22 29 28

(V)C-9A/CT.O

. 00-105E-9

(V)C

-9A/C

.


9

1. CABIN CONFIGURATION FOR INTERIOR ARRANGEMENT - 42 PASSENGERS AND 4 STEWARDS

7

205.

522

4

281

335

375

470

857

920

996

16 17 20 21 22 23 24 25 26 27

3 4 5 6 7 8 9 10 11 12 13 14 15

148.

5

198

213

243

280.

25

370

428

495

628

669

877

897

963

1019

1291

1 PILOT 15 VENTRAL STAIRWAY2 CO-PILOT 16 FLIGHT MECHANIC’S SEAT3 DOUBLE STEWARD’S SEAT 17 FORWARD GALLEY4 FORWARD STAIRWAY 18 27 X 485 FORWARD CABIN 19 34 X 726 LAVATORY 20 COATROOM7 PARTITION WITH FOLDING DOOR 21 A COUCH MAY BE LOCATED HERE IN LIEU OF TABLE AND CHAIRS8 2 TABLES 22 2 SWIVEL CHAIRS9 PARTITION WITH FOLDING DOOR 23 DISTINGUISHED VISITOR’S COMPARTMENT10 MAIN CABIN 24 OVERWING EMERGENCY EXITS11 COATROOM 25 DOUBLE COATROOM12 AFT GALLEY 26 ENGINE MOUNT BULKHEAD13 LAVATORY 27 LAVATORY14 28 X 72 28 DOUBLE STEWARD’S SEAT

1

2 18 1928

T.O. 00-105E

-9

C-12C/D/F

C-12C

/D/F.

AIRCRAFT PAINT SCHEME

1

T.O. 00-105E

-9

C-12C/D/F

C-12C

/D/F.

AIRCRAFT DIMENSIONS

29’ 6”

18’ 5”

43’ 10”

15’ 5”

9’ 0”

14.04”

14’ 11.4”

54’ 6”

8’ 2.5”DIAMETER

8’ 7”17’ 2”

CABIN ARRANGEMENT: CAPACITY 8 TO 15 PASSENGERS

LENGTH

HEIGHT

WING SPAN

2

APPLICABILITY: C MODEL

T.O. 00-105E

-9

C-12C/D/F

C-12C

/D/F.

AIRCRAFT DIMENSIONS

29’ 6”

18’ 5”

43’ 9”

14’ 9”

9’ 0”14.04”

14’ 11.4”

54’ 6”

8’ 2.5”DIAMETER

8’ 7”17’ 2”

CABIN ARRANGEMENT: CAPACITY 8 TO 15 PASSENGERS

LENGTH

HEIGHT

WING SPAN

3

APPLICABILITY: D MODEL

T.O. 00-105E

-9

C-12C/D/F

C-12C

/D/F.

AIRCRAFT DIMENSIONS

4

29.6”

CABIN ARRANGEMENT: PASSENGER CAPACITY= 8 TO 15

18’5”

43’9”

9’0”

14.04”

11’11.4”

14’6”

54’6”

8’ 2.5” DIA

8’7”17’2”

APPLICABILITY: F MODEL

HEIGHT

LENGTH

WING SPAN

T.O. 00-105E

-9

C-12C/D/F

C-12C

/D/F.5

SPECIAL TOOLS/EQUIPMENTPower Rescue SawFire Drill II

AIRCRAFT ENTRY

1. NORMAL ENTRY

a. Depress button adjacent to door handle in center ofpassenger door.

b. Rotate handle, located in center of passenger door leftside of aircraft, and swing door down.

NOTE:· Difficulty in opening door with engine(s) running may be

caused by inflated door seal.

· On D & F models the cargo door can only be opened frominside.

2. EMERGENCY ENTRY

a. Pull out handle on Emergency Exit hatch, located on rightside of fuselage.

b. Push in on hatch and remove from fuselage.

NOTE: Hatch may be locked with key from inside of aircraft.

3. CUT-IN

a. Cut cabin enclosure as required.

NOTE: All Models of the C-12 aircraft have a 57 gallon fuel tank located in each engine nacelle. Each engine nacelle contains 3.5 gallons of oil.

48 GALFUELTANKS

OXYGENCYLINDER

40 GAL

40 GAL

48 GAL

79 GAL

FUELTANKS

2bPASSENGERDOORHANDLE

CARGO DOORD & F MODELS ONLY

BATTERY2aEMERGENCYEXIT HATCHHANDLE

T.O. 00-105E

-9

C-12C/D/F

C-12C

/D/F.

AIRCRAFT ENTRY AND EXIT

EXTERNALEMERGENCY HANDLE

KEY LOCK

INTERNALEMERGENCY HANDLE

TO OPEN WITH INSIDE HANDLE TO OPEN WITH OUTSIDE HANDLE TO LOCK WITH INSIDE HANDLE

LOCK

ROTATE HANDLE TOLOCK POSITIONLIFT STEP TOINSPECT DOOR LOCK.

HOLD BUTTON,ROTATE HANDLE DOWNAND LOWER DOOR.

HOLD BUTTON,ROTATE HANDLEUP AND PUSHDOOR OUT.

APPLICABILITY: C MODEL

6

PUSH INAFTER RELEASE

PUSH INAFTER RELEASE

PUSH

PULL HANDLE TO RELEASE

EMERGENCY EXIT DOOR(Internal and external views)

NOTE:The emergency exit door is located atthe first window behind the co-pilot onright side of aircraft.

T.O. 00-105E

-9

C-12C/D/F

C-12C

/D/F.

AIRCRAFT ENTRY AND EXITAPPLICABILITY: D AND F MODELS

7

TO OPEN WITH INSIDE HANDLE TO OPEN WITH OUTSIDE HANDLE TO LOCK WITH INSIDE HANDLE

ROTATE HANDLE TOLOCK POSITIONLIFT STEP TOINSPECT DOOR LOCK.

HOLD BUTTON,ROTATE HANDLE DOWNAND LOWER DOOR.

HOLD BUTTON,ROTATE HANDLEUP AND PUSHDOOR OUT.

LOCK

EXTERNALEMERGENCY HANDLE

KEYLOCK

INTERNALEMERGENCY HANDLE

EMERGENCY EXIT

CARGO DOOR LOWERLATCHHANDLEACCESS

CARGO DOOR

LATCHHANDLE ACCESS

CARGODOORLATCHHANDLEACCESS

CARGO DOOR LOWER LATCHHANDLE ACCESS

LOCK

NOTE:The emergency exit door is located atthe first window behind the co-pilot onright side of aircraft.

EMERGENCY EXIT DOOR(Internal and external views)

T.O. 00-105E

-9

C-12C/D/F

C-12C

/D/F.8

ENGINE SHUTDOWN1. ENGINE SHUTDOWN - C AND D MODELS

a. Retard condition levers, located on right side ofpilot’s control pedestal, to FUEL, CUT OFFPOSITION.

b. Pull engine fire shutoff T-Handles, located on upperportion of pilot’s instrument panel.

NOTE: If Fire T-Handles are illuminated, actuate Fire Extinguisher Push Button, located between Fire T-Handles.

c. Place master switch, located on pilot’s overheadcontrol panel, to OFF position.

1cMASTER SWITCH

MASTER SWITCH

ON ON

RESETRESET

OFF#2 GEN#1 GENBATT

1aCONDITION LEVERS

CONTROL PEDESTAL

EXTINGUISHERPUSH BUTTON

1bENGINE FIRE SHUTOFFT-HANDLES

#1 FIRE PULL #2 FIRE PULL PUSH TO

EXTINGUISHSQUIB OK

T.O. 00-105E

-9

C-12C/D/F

C-12C

/D/F.

OVERHEAD FUEL, CONTROL, CIRCUIT BREAKER AND OXYGEN PANELS

COCKPIT LAYOUT

CONDITION LEVERS

PEDESTAL(TYPICAL)

REVERSE LEVERS

FEATHER LEVERS

OAT

9

APPLICABILITY: C AND D MODELS

MASTER SWITCH

T.O. 00-105E

-9

C-12C/D/F

C-12C

/D/F.

COCKPIT LAYOUT-Continued

PILOT’S CONTROL WHEEL CO-PILOT’S CONTROL WHEELFORWARD INSTRUMENT PANEL

10

APPLICABILITY: C AND D MODELSENGINE FIRE SHUTOFFT-HANDLES

T.O. 00-105E

-9

C-12C/D/F

C-12C

/D/F. 11

ENGINE SHUTDOWN1. ENGINE SHUTDOWN - F MODEL

a. Retard propeller levers and condition levers, located oncenter control pedestal, to CUT-OFF position.

b. Place firewall fuel switches (2), located on the fuelcontrol panel, left side console below boost pumpswitches, to OFF position.

c. Position gang bar for master switch and battery switch,located left instrument panel, to down position.

NOTE:The aircraft is equipped with a fire detection system, butdoes not have a fire extinguishing system.

1cGANG BAR

1aCONDITION LEVERS

1aPROPELLER LEVERS

CONTROL PEDESTALFUEL CONTROL PANEL

1bFIREWALL FUELSWITCHES (2)

FUEL SYSTEMOPEN OPEN

CLOSE CLOSE LEFT RIGHT

T.O. 00-105E

-9

C-12C/D/F

C-12C

/D/F.

AIRCREW EXTRACTION

12


a. Unlatch lap belts and remove “Y” shoulderharness from crewmember(s). Seats maybe equipped with adjustable head and armrests. Shoulder harnesses are connected toan inertia reel with the unlocking handle onthe side of the seats.

b. Passenger seats are equipped with lapbelts only. Lift center buckle to releaseoccupants. Seats may be equipped withadjustable head and aisle arm rests andseats recline.

c. Extract crewmembers and passengersthrough the passenger door and retractabledoor/stairway at left aft of aircraft.

NOTE:Rescue personnel may encountervariousarrangements for seating, folding tables,refreshment galley, storage cabinets, a fulllength couch, and possibly cargo.

PILOT ANDCO-PILOTSEATS

PILOT ANDCO-PILOTSEATS

PASSENGERSEATS

PASSENGERSEATS

STANDARD SEATING (UP TO 8 PEOPLE)

HIGH DENSITY SEATING (UP TO 15 PEOPLE)

C-12JT.O

. 00-105E-9

C-12J.1

AIRCRAFT DIMENSIONS

54’ 5.8”

9’ 1.5” DIA

6

3 o

o

12.25”17’ 2”

8’ 7” 6.12”

17.25”

18’ 5.8”

14’ 10.8”

57’ 10”

23’ 9.4”

14.07”

C-12JT.O

. 00-105E-9

C-12J.2

SPECIAL TOOLS/EQUIPMENTPower Rescue SawFire Drill II

AIRCRAFT ENTRY

1. NORMAL ENTRY

a. Depress button adjacent to door handle in center ofpassenger door or cargo door.

b. Rotate handle clockwise. Passenger door opensdown. Cargo door opens up.

Do not enter through crew door with left engine running. Beware of left engine exhaust/turbulence when entering the cargo door.

NOTE: Difficulty in opening door with engine(s) running may be caused by inflated door seal.

2. EMERGENCY ENTRY

a. Pull out handle on Emergency Exit Hatch locatedover right wing (two places) and left wing (oneplace).

b. Push in on hatch and remove from fuselage. Doorlocks can be over ridden from inside the aircraftwhen locked.

NOTE: Hatch may be locked with key from inside of aircraft.

3. CUT-IN

a. Cut cabin enclosure as required.

W AR NIN G

PERSONNEL CAPACITY20 PASSENGERS 2 CREWMEMBERS

FUEL CAPACITY: 675.2 GALLONSWET WING DESIGN, NO FUELBLADDERS IN WINGS

EMERGENCYEXIT HATCH (3)

BATTERY

OXYGENBOTTLES (2)

FUELCELLS (4)

247.

624

7.6

9090

2aEMERGENCY HATCHEXIT HANDLE

CREW DOOR CARGO DOOR

FIRE BOTTLE(1 EACH WHEEL WELL)

1aCREW/CARGO DOORBUTTON

1bCREW/CARGO DOORHANDLE

C-12JT.O

. 00-105E-9

C-12J.3

ENGINE SHUTDOWN ANDAIRCREW EXTRACTION1. ENGINE SHUTDOWN

a. Retard Propeller Levers and Condition Levers, located onright side of pilot’s control pedestal, to CUT OFF position.

b. Pull 5 AMP Firewall Valve circuit breakers (right and left),located on the fuel control panel, left side console, to OFFposition. (Go to step e, if no engine fire.)

c. IN CASE OF ENGINE FIRE: Push Fire Bottle ActuatingSwitches, located above right and left fire T-handles.

d. Pull Engine Fire Shutoff T-handles, located on upperportion of pilot’s instrument panel. Agent is CB.

e. Place Master Switch, located on pilot’s lower left instru-ment panel, to OFF position.

NOTE: Oxygen shutoff push/pull switches (2), are located on left side of instrument panel, 0 capacity is 38.3 liters. No LOX is used.


a. Unlatch lap belts and remove should harness fromcrewmembers. Crew seats have up and down and forwardand back movement only. Armrests lift up.

b. Unlatch lap belts from passengers.

1cFIRE BOTTLE ACTUATING SWITCHES

1dFIRE T-HANDLES

1eMASTERSWITCH

OXYGEN SWITCHES

FUEL CONTROL PANEL

1aPROPELLER LEVERS 1a

CONDITION LEVERS

CONTROLPEDESTAL

1bFIREWALL CIRCUIT BREAKERS

FIRE PULL FIRE PULL

2

Documents

WELCOME TO TECHNICAL ORDER 00-105E-9, 1 FEBRUARY 2006