welcome to technical order 00-105e-9, 1 february 2006
TRANSCRIPT
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WELCOME TO TECHNICAL ORDER 00-105E-9, 1 FEBRUARY 2006, REVISION 11.
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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 Retaining out of date rescue information can negatively affect the user’s operability and outcome of emergencies.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
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C-5
C-5. AIRCRAFT PAINT SCHEME1
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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
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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.)
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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
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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
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C-5
C-5.
20 340
50 65
100 60
6 AIRCRAFT HAZARD INFORMATION-Continued
DISTANCE FROM BYPASS NOZZLE EXIT
JET WAKE TEMPERATURE
TEMPERATURE - DEGREES FMAXIMUM THRUST TEMPERATURE
VELOCITY - MPHMAXIMUM THRUST VELOCITY
JET WAKE VELOCITY PROFILE
DISTANCE FROM BYPASS NOZZLE EXIT
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)
TEMPERATURE - DEGREES FMAXIMUM THRUST TEMPERATURE
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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)
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C-5
C-5.8 AIRCRAFT HAZARD INFORMATION-Continued
VIEW FROM TOP OF AIRCRAFT
RAM AIRTURBINE
PRESSURE FROMNO.2 ENGINE DRIVENHYDRAULIC PUMPS
PRESSURE FROMNO.1 ENGINE DRIVENHYDRAULIC PUMPS
PRESSURE FROMNO.3 ENGINE DRIVENHYDRAULIC PUMPS
PRESSURE FROMNO.4 ENGINE DRIVENHYDRAULIC PUMPS
HYDRAULIC SERVICECENTER NO. 2
NO.1-2 HYDRAULIC POWERTRANSFER UNIT
HYDRAULIC SERVICECENTER NO. 1
HYDRAULIC SERVICECENTER NO. 3
NO.3-4 HYDRAULIC POWERTRANSFER UNIT
HYDRAULIC SERVICECENTER NO. 4
NO. 2-3 POWERTRANSFER UNIT
LOCATED ONWING REAR BEAM
AIR TURBINE MOTORSAND HYDRAULIC PUMPS
HYDRAULIC RESERVOIRAND SUCTION BOOST PUMP
VIEW FROM TOP OF AIRCRAFT
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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.
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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
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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 compart- ment in the upper deck and vice versa.
AIRCRAFT ENTRY-Continued
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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
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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
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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)
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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
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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
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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 dis- charge 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
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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
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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.
2. AIRCREW EXTRACTION
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
.
CABIN CONFIGURATIONS - Continued
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
.
CABIN CONFIGURATIONS - Continued
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
1. AIRCREW EXTRACTION
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.
3. AIRCREW EXTRACTION
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