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 9 COVERING CHAPTER 7 from the E-3 30/35 to VC-25A.

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: HQAFCESA.CEXF@tyndall.af.mil

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 Retaining out of date rescue information can negatively affect the user’s operability and outcome of emergencies.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

SEGMENT 9 INFORMATION CHANGE NOTICE

None.

TO 00-105E-9

Chapter 7 Cover

NOTE

Chapter 7 contains emergency rescue andmishap response information for the following aircraft:

USAF E-3 30/35USAF E-4A/BUSAF E-6BUSAF EA-6BUSAF E-8CUSAF E-9AUSAF VC-25 (AF-1)USAF YAL-1A

T.O. 00-105E-9

7-1. INTRODUCTION AND USE.

7-2. 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.

7-3. GENERAL ARRANGEMENT.

7-4. 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 7

U.S. AIR FORCE

ELECTRONIC/VC-25(AF-1)

AEROSPACE EMERGENCY RESCUEAND MISHAP RESPONSE INFORMATION

7-1

E-3 30/35.

E-3 30/35T.O

. 00-105E-9

AIRCRAFT PAINT SCHEME

1

E-3 30/35.

E-3 30/35T.O

. 00-105E-9

NOTE: Dimensions are along the contour of the aircraft.

NOTE: Aircraft Dimensions Length 152’11” Wing Span 145’9” Height 42’5”

FORWARD LOWER LOBE (RIGHT SIDE)PENETRATE 6 INCHES FROM THE LEFTSIDE EDGE AND 9.5 INCHES FROM THEBOTTOM EDGE.

AFT UPPER LOBE (RIGHT SIDE)PENETRATE THE LOWER AFTPART OF THE EMERGENCYCUT-IN LOCATION. AFT LOWER LOBE (RIGHT SIDE)

PENETRATE 9.75 INCHES FORMTHE LEFT EDGE AND 8.75 INCHESFROM THE BOTTOM EDGE.

2

SKIN PENETRATION POINTS AND DIMENSIONS

E-3 30/35.

E-3 30/35T.O

. 00-105E-9

3

SKIN PENETRATION POINTS-ContinuedNOTE: Dimensions are along the contour of the aircraft.

FORWARD UPPER LOBE (LEFT SIDE) PENETRATE 4INCHES UP FROM THE BOTTOM AND 4.5 INCHESAFT OF THE FORWARD EDGE OF THE EMERGENCYCUT-IN LOCATION.

FORWARD LOWER LOBE (LEFT SIDE)PENETRATE 4 INCHES AFT OF F.S.600 AND 14.75 INCHES BELOW THESKIN LAP EDGE AT STRINGER 20.

AFT UPPER LOBE (LEFT SIDE) PENETRATE 4 INCHESUP FROM THE BOTTOM AND 4.5 INCHES AFT OF THEFORWARD EDGE OF THE EMERGENCY CUT-INLOCATION.

AFT LOWER LOBE (LEFT SIDE) PENETRATE 5INCHES FORWARD OF F.S. 1100 AND DOWN13.75 INCHES FROM THE SKIN LAP EDGE ATSTRINGER 20.

23 24

E-3 30/35.

E-3 30/35T.O

. 00-105E-9

4

SKIN PENETRATION POINTS-ContinuedNOTE:• Penetration points for the aircraft engines are identical

regardless of engine position on the aircraft.

• Dimensions are along the contour of the door.

ENGINE COWL DOOR (LEFT SIDE) PENETRATE41 INCHES FROM THE TOP EDGE AND 4.5INCHES FROM THE FORWARD EDGE.

ENGINE COWL DOOR (RIGHT SIDE) 31INCHES FROM THE TOP EDGE AND 4.5INCHES FROM THE FORWARD EDGE.

E-3 30/35.

E-3 30/35T.O

. 00-105E-9

5

NOTE: Personnel on board: Minimum - 21; Maximum - 40. 8 people can be seated in aft section of this aircraft.

AIRCRAFT ENTRY ALL MODELS

CAUTION

When cabin doors are opened from outside, escape slides will automatically deploy but will not inflate.

1. NORMAL ENTRY

a. Pull handle out and rotate clockwise, pull aft side ofdoor outward while pushing forward side inward. Opendoor outward.

2. EMERGENCY ENTRY

a. Depress red panel, located top center of escapehatch(es). Push hatch inward and lift upward.

b. Pull handle out and rotate counterclockwise, pull aftside of door outward while pushing forward side inward.Open door outward.

c. Press catch to release and pull handle down to unlock.Push door in and slide forward. Enter through deckdoors.

d. Press catch to release and rotate handle to unlock, andpush door in. Enter forward compartment and thencabin through deck doors.

3. CUT-IN

a. Cut marked areas as last resort.

SPECIAL TOOLS/EQUIPMENTPower Rescue Saw24 Ft LaddersFire Drill II OXYGEN

OXYGENOXYGEN

OXYGEN

OXYGENFIREFIGHTING

OXYGEN CONVERTER

FUELTANKS

BATTTERIES

439

439

2323

2323

4069

4069

10,193

1aFWD ENTRY DOOREXTERNAL HANDLE

2aESCAPE HATCH(BOTH SIDES) 2b

EMERGENCY EXITEXTERNAL HANDLE

1aAFT ENTRY DOOR

2cCOMPARTMENT DOOREXTERNAL HANDLE

CUT-IN(RIGHT SIDES)

CUT-IN LEFT SIDES)

2dELECTRONIC ACCESSDOOR HANDLE

LIFE RAFT(BOTH SIDES)

E-3 30/35.

E-3 30/35T.O

. 00-105E-9

6

ENGINE SHUTDOWN ANDAIRCREW EXTRACTION1. ENGINE SHUTDOWN

a. Retard throttles, located on pilot’s centerconsole, to CUTOFF position (shuts offfuel and ignition).

b. Pull engine fire switches located onoverhead electrical distribution panel.

c. Place battery switch, located top centeron flight engineer’s panel, to OFFposition.

NOTE: Open circuit breakers at batteries forward in lower lobe instead of disconnecting or removing batteries for power shutdown.

2. AIRCREW EXTRACTION

a. Unlatch seat belts and remove shoulderharnesses from flight crew and missioncrew.

NOTE:• If seat tracks are not damaged during

crash landing, use adjustable seatcontrols for retraction.

• Rest area seats are equipped with seatbelts only.

• Flight crew seat arm rests release to liftup.

1bENGINE FIRE SWITCHES

ELECTRICALDISTRIBUTIONPANEL

FLIGHTENGINEER’SPANEL

FLIGHTCREWSTATIONS

MISSIONCREWSTATIONS

1aTHROTTLESCUTOFF

AISLE CONTROL STAND

1cBATTERYSWITCH

REST SEATS

BUNKS

ON

OFF

BATTERY

E-3 30/35.

E-3 30/35T.O

. 00-105E-9

7

CABIN ARRANGEMENT

ROTARY ANTENNAMAIN DECK WITH CREW WORKSTATIONS AND CREW REST AREAS

FLIGHT DECK

FORWARD LOWERCOMPARTMENTROTARY

AFT LOWERCOMPARTMENT

E-3 30/35.

E-3 30/35T.O

. 00-105E-9

8

CABIN ARRANGEMENT-Continued

FLIGHT DECK MAIN DECK

NEWRESTSEATS (4)

NEWCREWSTATIONS(5 SEATS)

NEWRESTSEATS (4)

ROTARY ANTENNA

LOWER COMPARTMENTS

UPPER COMPARTMENTS

E-4. E-4

T.O. 00-105E

-9

AIRCRAFT PAINT SCHEME1

E-4. E-4

T.O. 00-105E

-9

AIRCRAFT SKIN PENETRATION POINTS2

NOTE: Aircraft Dimensions Length 231’ 4” Wing Span 195’ 8” Height 63’ 5”

FWD FUSELAGE (BOTH SIDES)B.S. 690W.L. 260R/L.B.L. 124BETWEEN STRINGERS 18 AND 19

SECTION 41 SECTION 42SHF/SATCOMRADOME E-4B ONLY

854

615

488

434

134.75

AERIALREFUELINGRECEPTACLE

TOP OF PILOT’SFLOOR WL 312

WL 265APPROX

TOP OF FLOORWL 199.8

WL 118.00WL 91

E-4. E-4

T.O. 00-105E

-9

3 AIRCRAFT SKIN PENETRATION POINTS-Continued

AFT FUSELAGE(BOTH SIDES)B.S. 2130W.L. 260R/L.B.L. 117BETWEEN STRINGERS 18 AND 19

SECTION 46 SECTION 48

24.00FRAMESPACING

22.80FRAMESPACING

DROGUENESTE-4B ONLY

W.L. 286.0W.L. 276.0

APU ACCESS DOORB.S. 2728.5W.L. 264L.B.L. 10

STABILIZATIONHINGE POINT

DROGUE BAYE-4B ONLY

2007

2231

2285

E-4. E-4

T.O. 00-105E

-9

4 AIRCRAFT SKIN PENETRATION POINTS-Continued

ENGINE PYLONS (BOTH SIDES)

ENGINE ACCESSORYSECTION (BOTH SIDES)

NOTE: Penetration points for the aircraft engines are identical regardless of position on the aircraft.

E-4. E-4

T.O. 00-105E

-9

5 AIRCRAFT HAZARDS

200 FT

150 FT

100 FT

50 FT

0 FT

50 FT

75 FT

150 FT 100 FT 50 FT 0 50 FT 100 FT 150 FT

0 10 20 30 40 50 60 70 80 DISTANCE IN FEET

IN FAHRENHEIT1200 500 300 200

APU EXHAUST GAS TEMPERATURE

POWER SETTING RADIUS RADIUS

GROUND IDLE 75’ 100’BREAK AWAY 100’ 150’THRUST 52% N1TAKEOFF THRUST 100’ 200’

Prolonged exposure of one hour,even with ear protection, cancause ear damage.

Ear protection required within thisarea.

NOISE HAZARD AREAS

IDLE THRUST

25 FOOT RADIUS

TEMPERATURE IN F

340240140

0

0

0

WARNING

NOTE: Includes 20 knot crosswind effect.

INLET SUCTION DANGERWIND VELOCITY APPROXIMATELY 210 TO 145 MPH

WIND VELOCITY APPROXIMATELY 145 TO 105 MPHWIND VELOCITY APPROXIMATELY 105 TO 65 MPHWIND VELOCITY APPROXIMATELY 65 TO 20 MPH

0 0 0 0

E-4. E-4

T.O. 00-105E

-9

6 AIRCRAFT HAZARDS-Continued

RADIATION HAZARD AREASRADAR AND HIGH FREQUENCY (HF)

APU FIRE DETECTION AND CONTROL

WARNING

RADARPERSONNEL RADIATIONHAZARD AREA - 40 FEETPOSSIBLE FUEL IGNITIONAREA - 60 FEETPOSSIBLE ELECTRO EXPLOSIVEDEVICE DETONATION - 75 FEET

HF ANTENNAS

During periods of HF transmission on the ground,personnel should stay away from all external surfacesof the aircraft and handling of metal objects such aslight cords, cooling ducts, grounding cables, etc.attached to the aircraft. RF voltages can reach inexcess of 700 volts between aircraft structure andground. The RF voltages can result in shock or skinburns.

Ground operation of the AN/ARC-58 is prohibitedunless the aircraft is at least 200 feet from thefollowing:

(1) Unloaded weapons or warheads.

(2) Loaded weapons in an aircraft with bomb bay doors open.

(3) Missles with warhead compartment doors open, or thruster and squib access door open.

2

1

1 - WHEN PULLED, WILL SHUTDOWN THE APU AND ARM THE APU FIRE EXTINGUISHER CIRCUIT.

2 - WHEN PUSHED, WILL DISCHARGE THE CONTENTS OF THE APU FIRE EXTINGUISHER INTO THE APU COMPARTMENT.

75 FEET

40 FEET

60 FEET

E-4. E-4

T.O. 00-105E

-9

7 AIRCRAFT HAZARDS-Continued

WARNING

UHF, UHF SATCOM AND SHF SATCOM RADIATION

The radiation hazard shown is around the SHF SATCOMantenna and the UHF Transmitter Antennas. Accidentalentry into the hazard area does not result in injury. It isonly through prolonged exposure that the possibility ofdanger exists.

POSSIBLE FUEL IGNITION AREA

UHF AREAS HAZARDOUS TO PERSONNEL

SHF RADIO AREAS HAZARDOUS TOPERSONNEL

40

40

0

0

0

0

0

0

+ 10

0

-5

20 FEET

25 FEET10 FEET

+10

0

-5

10 FOOTRADIUS

25 FOOTRADIUS

PERSONNEL AND FUEL

SEE TABLENEXT PAGE

SEE TABLENEXT PAGE

E-4. E-4

T.O. 00-105E

-9

8 AIRCRAFT HAZARDS-Continued

WARNING

UHF, UHF SATCOM AND SHF SATCOM RADIATION

WARNING

• UHF FDM hazard extends form transmit antennas No. 1-5: 100 feet• UHF SATCOM hazard area is elliptical extending 40 feet from each antenna• SHF SATCOM hazard area extends a maximum of 740 feet from the antenna (station 750.64)

ELECTRO EXPLOSIVE DEVICES HAZARD

UHF FDM

UHF SATCOM

SHF SATCOM

100 FEET100 FEET

40 FEET

SEE TABLE

40

SHF SATCOMMAIN BEAN RADIATION HAZARDS

DISTANCE (FEET)TRANSMITPOWER(WATTS)

PERSONNEL ELECTROEXPLOSIVEDEVICES

FUEL

1000 110 210 5

3000 200 365 10

5000 250 470 10

7000 300 560 15

12500 380 740 20

• Radiation hazard exists in the main beam (+ 2 degreesfrom antenna centerline).

• 1000 watts is the maximum power limit for SHF SATCOMground operation without radiation hazard override. Theradiation hazard override permits operation of the SHFSATCOM antenna at full Transmitter power and at antennaelevations of +10 degrees to -5 degrees from horizontal.

100 FEET

SEE TABLE

ELECTRO EXPLOSIVE40

40 FEET+10

0

-5

0

0

00

0

0+10

-50

E-4. E-4

T.O. 00-105E

-9

9 AIRCRAFT ESCAPE ROUTES

CAUTION

During ditching do not deployslide at No. 3 Right EntryDoor. It will interfere with No.4 Right Escape Route.

NOTE:• No. 4 Left Entry Door deactivated.

• Use Escape slides during ditch-ing, if feasible, use of slidesdetermined by height of doorsabove water.

• All positions with escape routesdesignated may be occupied fortakeoff and landing, exceptpositions in forward and aft lowerequipment areas and the twoseats in projection room.

• All seats that rotate shall face aftfor ditching and crash landing.

• Do not inflate life rafts in aircraftas they will not then passthrough the exits.

• Life raft compartment doors mustbe closed after deployment raftsto permit unrestricted exit.

• If personnel caught in projectionroom, exit aft door of room pastpodium and through right door ofbriefing room to No. 2 Right EntryDoor.

WARNING

NOTE: Flight Engineer assists upper rest area & NCA evacuation.

FLIGHTDECK UPPER DECK REST AREA

AREA 1

UPPER DECK

AREA 9 AREA 10

LIFE RAFT (20 MAN)ESCAPE ROPEKNOCK OUT PANEL

FWD LOWER LOBE

PILOT’S ESCAPE - MONITORING ROUTECO-PILOT’S ESCAPE - MONITORING ROUTE

NAVIGATOR’S ESCAPE - MONITORING ROUTE

AREA 11 AREA 12

AFT LOWER LOBE

NO. 1 RIGHT DOOR NO. 2 RIGHT DOOR NO. 3 RIGHT DOOR NO. 4 RIGHT DOOR NO. 5 RIGHT DOOR

NCA AREA 2 FWD ENTRY CONFERENCE RM BRIEFING RM BATTLE STAFF COMM CONTROL TECH CONTROL/REST AREA 3 AREA 4 AREA 5 AREA 6 AREA 7 AREA 8

MAIN DECK MAIN DECK MAIN DECK

NO.1 LEFT NO. 2 LEFT NO. 3 LEFT DOOR NO. 5 LEFT DOOR DOOR DOOR

E-4. E-4

T.O. 00-105E

-9

10

SPECIAL TOOLS/EQUIPMENTPower Rescue Saw35 Ft LadderFire Drill II

AIRCRAFT ENTRY ALL MODELS

1. NORMAL/EMERGENCY ENTRY

a. Pull entry door handles from recess position androtate 180 degrees clockwise for entry doorslocated on left side and counterclockwise for entrydoors on right side.

NOTE: All ten entry doors open outward, number (4) entry door left side of aircraft is blocked.

b. Press release button on crew escape hatch,located top forward center of crew compartment,and rotate escape hatch handle 180 degreesclockwise. Push escape hatch inward.

c. Pull handle, located on crew door, and rotate 180degrees counterclockwise. Push door inward untilslide tracks are engaged, then slide door aft.

NOTE:• Opening a door from the outside disengages the

emergency evacuation system and the escapechute will not deploy.

• All emergency escape chutes are deployed frominside the aircraft only.

2. CUT-IN

a. Cut areas along window lines as last resort.

E10 UPPEREQUIPMENTCENTER(RH SIDE)

MAIN BATTERY

FLIGHT DECK

1bCREWESCAPEHATCH

17,000

FUEL TANKS

4,420

12,300

APU

APU BATTERY

DOOR 4L BLOCKED

4,42012,300

4 OXYGEN CONVERTERS 75 LITERSEACH IN FORWARD LOWER LOBE

1cCREW DOOR(RH SIDE ONLY) ENTRY DOORS ENTRY DOORS

BELOWFLIGHTDECKENTRYHATCH

1bRELEASEBUTTON

1bESCAPEHATCH HANDLE

1cENTRY DOORAND CREWDOOREXTERNALHANDLE

1aENTRY DOOREXTERNAL HANDLE(LH SIDE)

NOTE: 2 inch band of contrasting color around all doors and hatch operable from outside the aircraft.

E-4. E-4

T.O. 00-105E

-9

11 ENGINE SHUTDOWN ANDAIRCREW EXTRACTION1. ENGINE SHUTDOWN

a. Retard THROTTLES, located on pilot’s center console,by pulling UP and FULL DOWN to IDLE CUT-OFFposition.

b. Place ENGINE START LEVERS, located on pilot’scenter console, to CUT-OFF position.

NOTE: If engines fail to shutdown, pull emergency fire T- handles, located on pilot’s overhead panel.

c. Use this if needed. Place APU switch, located on flightengineer’s upper left panel, to STOP position. ForEXTERNAL APU shutdown, see page E-4.5.

NOTE: If APU fails to shutdown, pull emergency fire T-handle, located on flight engineer’s overhead panel.

d. Place BATTERY SWITCH, located on flight engineer’scenter panel upper left side, to OFF position.

2. AIRCREW EXTRACTION

a. Unlatch lap belts and remove shoulder harness fromcrewmembers.

b. Depress control handles and rotate flight engineer’sseat from left to right. A foot pedal at base of pedestalcan be depressed to move the navigator’s seat aft.Use the third handle inboard of pilot and copilot’s seatfor forward and aft adjustments. A dial knob is used torelease restraints.

c. Passenger seats are equipped with lap belts only.

FORWARD INSTRUMENT PANELEMERGENCY FIRE T-HANDLES

1aTHROTTLES

FLIGHT ENGINEER’S PANEL

1bENGINE START LEVERS

APU FIRE SHUTDOWNT-HANDLE

1cAPU SWITCH

1dBATTERY SWITCH

APU

FIRE

PULLAPU

START

ON

STOP

BATTERY

ON

OFF

E-4. E-4

T.O. 00-105E

-9

12 AIRCREW SEATING AND POSITIONINGNOTE: Pilot’s seat is shown, copilot’s seat is identical except controls are on left side.

LEGEND

1. INERTIA REEL SHOULDER HARNESS2. ARMREST ADJUSTMENT CONTROL HANDLE3. SEAT BOTTOM TILT (T) ADJUSTMENT CONTROL HANDLE4. VERTICAL (V) ADJUSTMENT CONTROL HANDLE5. FORE/AFT/LATERAL (H) ADJUSTMENT CONTROL HANDLE6. BACKREST RECLINE (R) ADJUSTMENT CONTROL HANDLE7. ROTARY RELEASE BUCKLE FOR SAFETY RESTRAINTS

1

2

7

3

4

5

6

PILOT’S/COPILOT’S SEAT

E-4. E-4

T.O. 00-105E

-9

13 AIRCREW SEAT AND POSITIONING-Continued

ENGINEER’S/NAVIGATOR’S SEAT

NOTE: The swivel(s) adjustment control handle and the lateral adjustment control handle are located on the right hand side of the seat.

NOTE: The navigator’s seat is identical to the flight engineer’s seat, except that it is equipped with a headrest.

LEGEND

1. INERTIA REEL SHOULDER HARNESS2. ARMREST ADJUSTMENT CONTROL HANDLE3. VERTICAL (V) ADJUSTMENT CONTROL HANDLE4. FORWARD/AFT(H) ADJUSTMENT CONTROL HANDLE5. BACKREST RECLINE (R) ADJUSTMENT CONTROL HANDLE6. SAFETY RESTRAINT LEVER BUCKLE

1

2

2

6

5

4

3

E-4. E-4

T.O. 00-105E

-9

14 AIRCREW SEAT AND POSITIONING-ContinuedNOTE: The backrest folover control handle is located on the lower inboard side of the seat back. The forward and aft adjustment control handle is located on the left side of the seat.

LEGEND

1. FOLDING AND STOWAGE CONTROL HANDLE2. BACKREST RECLINE ADJUSTMENT CONTROL HANDLE

OBSERVER’S SEAT

12

E-4. E-4

T.O. 00-105E

-9

15 E-4A GENERAL CABIN ARRANGEMENTNOTE: Doors that have a keyless lock are equipped with an emergency kickout panel. These entrances are marked on the floor plan with an asterisk(*). KICKOUT

PANEL

KEYLESS DOOR (TYPICAL)

AFT LOWER LOBE

NO. 1 LEFT NO. 2 LEFT NO. 3 LEFT NO. 5 LEFTMAIN DECK MAIN DECK MAIN DECK MAIN DECKENTRY DOOR ENTRY DOOR ENTRY DOOR ENTRY DOOR

NO. 1 RIGHT NO. 2 RIGHT NO. 3 RIGHT NO. 4 RIGHT NO. 5 LEFTMAIN DECK MAIN DECK MAIN DECK MAIN DECK MAIN DECKENTRY DOOR ENTRY DOOR ENTRY DOOR ENTRY DOOR ENTRY DOOR

CREW SERVICEENTRANCE DOOR

UPPER DECK REST AREA

FLIGHTDECK

EQUIP ROOMOPERATOR AREA

MAIN DECK REST AREAVOICE AREADATAAREA

BRIEFINGROOMPROJ

RMFWDENTRYAREA

NCA AREA

CONFERENCE AREA

AISLEWAY

BATTLE STAFF AREA

UPPER FORWARD LOBE

UPPERFORWARDLOBE

AFTLOWERLOBE

E-4. E-4

T.O. 00-105E

-9

16 E-4B GENERAL CABIN ARRANGEMENT

NOTE: Doors that have a keyless lock are equipped with an emergency kickout panel. These entrances are marked on the floor plan with an asterisk(*).

KICKOUTPANEL

KEYLESS DOOR (TYPICAL)

NOTE: AIRCRAFT DIMENSIONS LENGTH 231’ 4” WING SPAN 195’ 8” HEIGHT 63’ 5”

8.0

7.0

6.0

12.0

11.0

10.0

1.0

9.0

5.0

4.03.0

2.0

1.0 FLIGHT DECK AND UPPER DECK REST AREA 7.0 COMMUNICATION CONTROL AREA2.0 NCA AREA 8.0 TECHNICAL CONTROL/REST AREA3.0 FORWARD ENTRY AREA 9.0 FLIGHT AVIONICS AREA4.0 CONFERENCE ROOM 10.0 FORWARD LOWER EQUIPMENT AREA5.0 BRIEFING ROOM 11.0 AFT LOWER EQUIPMENT AREA6.0 BATTLE STAFF AREA 12.0 LOWER TRAILING WIRE ANTENNA AREAFLIGHT DECK UPPER DECK

REST AREA AREA 1UPPER DECK

AREA 9 AREA 10 FWD LOWER LOBE

FOUR OXYGENCONVERTERS75 LITERS EACH

AREA11 AREA 12 AFT LOWER LOBE

NO. 1 FLIGHT DOOR NO.2 FLIGHT DOOR NO. 3 FLIGHT DOOR NO. 4 FLIGHT DOOR NO. 5 FLIGHT DOOR

NO. 1 LEFT DOOR NO.2 LEFT DOOR NO. 3 LEFT DOOR NO. 5 LEFT DOOR FWD ENTRY CONFERENCE BRIEFING ROOM BATTLE STAFF COMM CONTROL TECH CONTROL/ NCA AREA AREA 3 ROOM AREA 4 AREA 5 AREA 6 AREA 7 REST AREA 8

AISLEWAY

E-4. E-4

T.O. 00-105E

-9

17 E-4B OXYGEN SYSTEMINCORPORATING TCTO 1E-4B-573

NOTE: TCTO 1E-4B-573 changes location of oxygen system and uses oxygen con- verters instead of oxygen cylinders. Referrring to page E-4.15, the unmodified aircraft oxygen system is located in area 10 of the forward lower lobe. Modified aircraft oxygen converters are located in the aft right side of area 9.

CAPACITY: 75 LITERSTYPE: GASEOUSLOX PRESSURE: 300 +/- 15 PSI

FORWARDLOWERLOBE

FORWARD LOWER LOBE

FORWARDOXYGENSHROUDASSEMBLY

MANUALINTERCONNECTVALVE (2 PLACES)

DRIP PAN

SUPPLY PORT

OVERBOARDCONVERTER VENT OVERBOARD

CONDENSATEDRAIN MAST

BUILDUP PORT

FILL PORT

RELIEF PORT

GAS PORT

CONVERTER(4 PLACES)

MANUALSHUTOFF(4 PLACES)

HEAT EXCHANGER(4 PLACES)

INBOARDOXYGENSHROUDASSEMBLY

RACK ASSY

E-6B

. E-6BT.O

. 00-105E-9

1

AIRCRAFT PAINT SCHEME

E-6B

. E-6BT.O

. 00-105E-9

2

AIRCRAFT DIMENSIONS AND HAZARDSDIMENSIONSLENGTH 152 FT 11 IN (46.61 m)HEIGHT 42 FT 5 IN (12.93 m)WING SPAN 148 FT 2 IN (45.16 m)

NOTE: The Mercury Tacamo II (TAke Charge And Move Out) is 75% common to the E-3. The main differences are: (1) Deletion of the dorsal radome and its support structure (2) Addition of wing tip ESM/SATCOM pods (3) HF antenna fairings (4) Increased corrossion protection (5) Retained the nuclear/EMP (electromagnetic pulse) hardened airframe (6) Incorporation of large forward freight door (707-320C) (7) Landing gear identical to the E-3 (8) Powerplant: Four 97-86 kN (22,000 lb st) CFM International F108-CF-100 turbofans (9) Single point refueling (10) In-flight refueling via boom receptacle above flight deck

INLET SUCTION 25 FEET

HF RADIATION360 DEGREE ARC 10 FEET

ENGINEEXHAUST 500 FEET

TURBINEBLADEFAILURE300 FEET

APU INTAKEAND EXHAUST 25 FEET

UHF RADIATION360 DEGREE ARC60 FEET

RADAR RADIATIONFWD 240 DEGREE ARC 60 FEET

E-6B

. E-6BT.O

. 00-105E-9

3 AIRFRAME MATERIALS

ALUMINUM

STEEL

OTHER-FIBERGLASS

NOTE: Skin penetration points are similar to the E-3. See pages E-3 30/35.1, .2, & .3.

E-6B

. E-6BT.O

. 00-105E-9

4

SPECIAL TOOLS/EQUIPMENTPower Rescue SawCrash AxeSPAAT/Fire Drill II24 Foot Ladders

AIRCRAFT ENTRY1. NORMAL ENTRYNOTE: Normal entry to the main deck is through the forward and aft main doors on the left side. Normal entry to the forward and aft lower compartments is through the forward and aft cargo doors on the right side. The forward and aft lower compartemnts also provide access to the main deck through access hatches located on the overhead of each compartment.

a. Pull either the main door handle out and rotate clockwise.b. Release and stow handle.c. Pull on aft side of door while pushing in on forward side until door is parallel to aircraft and door open latch has caught.d. Press catch on either forward or aft cargo door handle.e. Rotate handle counterclockwise, push door in, and slide door forward. f. To access the main deck, depress latch on access hatch and push upward on bottom of hatch until uplock is engaged.

2. EMERGENCY ENTRYNOTE: Emergency entry may gained through the radio access door (aft of nose landing gear doors), emergency exit hatches (over each wing), and bailout door (aft right side).

a. Press catch on radio access door release handle.b. Rotate handle counterclockwise and push up and forward on door.

BATTERIES

ENGINEOIL54 GALTOTAL ALLENGINES

ENGINE OIL

HYDRAULIC72 GAL

OXYGEN/LOX75 LITERS LOX18 PORTABLEBOTTLES(TYPICAL)

1aFWDANDAFTMAINDOORHANDLE

1dRIGHT CARGODOOR HANDLE

2aRADIO ACCESS HATCH

1fACCESSHATCH

NOTE: To gain entry to the main deck from the radio access door, proceed through compartment and open hatch to the main deck.

E-6B

. E-6BT.O

. 00-105E-9

5

AIRCRAFT ENTRY-Continued2. EMERGENCY ENTRY-Continued

Rescue crews are at risk if the forward or aftdoors to the main decks on the left side areopened from the outside, the escape slides/chutes will deploy if they have not been discon-nected from the inside.

Radio Access Door - Nose Landing Geara. Press catch to release handle.b. Rotate handle counterclockwise and push door inward.

Emergency Exit Hatches - Over Wingsc. Push panel inward to unlatchd. Push hatch inward and lift upward. Hatch weighs about 50 pounds.

Bailout Door - Right Hand Afte. Pull door handle out and rotate counter- clockwise.f. Push door inward. Door is free-standing and weighs about 69 pounds.

3. CUT-IN

a. Cut in entry areas as indicated on graphic using power rescue saw or crash axe.

2aRADIO ACCESS DOOR

3aCUT-INAREAS

2cEMERGENCY EXIT HATCHES

2eBAILOUT DOOR

CUT HERE FOREMERGENCY RESCUE

WARNING

E-6B

. E-6BT.O

. 00-105E-9

6 ENGINE/APU SHUTDOWN ANDBATTERY DISCONNECT1. ENGINE/APU SHUTDOWN

a. Retard throttles to full aft position.

b. Pull start levers aft and place in full down position.

c. Pull engine fire switches.

d. Pull APU fire switch.

e. Lift red guard and place battery switch down in OFF position.

2. BATTERY DISCONNECT

NOTE: Batteries are located in the forward lower compartment accessible through the radio access door, labeled Battery Access.

a. To further deactivate the batteries, remove quick disconnect fittings, if time permits.

1aTHROTTLES

1bSTARTLEVERS

1cENGINE FIRE SWITCHES

1dAPU FIRE SWITCH

1eBATTERY SWITCHWITH RED GUARD

E-6B

. E-6BT.O

. 00-105E-9

7 AIRCREW EXTRACTION1. AIRCREW EXTRACTION

NOTE: All crewmembers are attached to their seats by shoulder harnesses secured to lap belts equipped with quick disconnect buckles (rotary type). Aft facing crew rest seats are not equipped with shoulder harnesses; forward facing seats are so equipped. Both have quick disconnect buckles similar to the pilot’s seat.

a. Rotate rotary release buckle in either direction to release shoulder harness, lap belt belt, and crotch strap.

FOR CREW REST SEATS

b. Rotate rotary release buckle in either direction to release shoulder harness and lap belt on forward facing seats or lap belt only on aft facing seats.

1aROTARY RELEASE BUCKLE

1bROTARY RELEASE BUCKLE

1bCREW REST SEATS

1aCREW SEAT (TYPICAL)

EA

-6B.

T.O. 00-105E

-9

EA-6B

1

AIRCRAFT DIMENSIONS AND HAZARDS

INLET SUCTION 25 FEET

RADIATION HAZARD 80 FEETFORWARD 114 ARC0

TURBINE BLADE FAILURE 300 FEET

ENGINE EXHAUST HAZARD 300 FEETIDLE 75 FEETMAX 270 FEET

DIMENSIONSLENGTH 59 FT 10 IN (18.24 m)HEIGHT 16 FT 3 IN (4.95 m)WING SPAN 53 FT (16.15 m)WINGS FOLDED 25 FT 10 IN (7.87 m)

EA

-6B.

T.O. 00-105E

-9

EA-6BAIRCRAFT HAZARDS

2 ARMAMENT4 Wing Stations1 Fuselage StationChaff and FlaresPylon Ejector Cartridges

FUSELAGE STATION

PYLON EJECTOR CARTRIDGES

WING STATIONS

PYLON EJECTOR CARTRIDGES (FOURTH AREA NOT SHOWN SAME AS LEFT WING)

CHAFF/FLARES

EA

-6B.

T.O. 00-105E

-9

EA-6B

3

AIRFRAME MATERIALS

ALUMINUM

STEEL

OTHER

FIBERGLASS

EA

-6B.

T.O. 00-105E

-9

EA-6B

4

SPECIAL TOOLS/EQUIPMENTPower Rescue SawCrash AxeFire Drill II20 Ft Ladder

AIRCRAFT ENTRY

1. NORMAL ENTRYa. Unlatch and lower boarding ladder.b. Open canopies by rotating Canopy Contro Handle counterclockwise.c. To enter forward cockpit, unlatch Hinged Boarding Platform, use platform step.

2. EMERGENCY ENTRYa. Canopy Jettison Controls are located aft of engine intakes on either side.b. Push thumb catch to lower canopy jettison access door.c. Pull exposed Canopy Jettison Handle to jettison canopies.

3. CUT-INa. Canopies are acrylic plastic and may be cut with power rescue saw or crash axe.b. Cut along canopy frames on all four sides.

INTERNAL FUEL2300 GALS

EXTERNAL FUEL1500 GALS

OXYGENTHREE 10 LITERCONVERTERS

BATTERY (1)

OILENGINE 15.6 GALHYDRAULIC 13 GAL

1aBOARDINGLADDER

1cHINGEDBOARDINGPLATFORM

1bCANOPYCONTROLHANDLE

2a,b,cCANOPYJETTISONACCESSDOORS ANDCONTROLS

EA

-6B.

T.O. 00-105E

-9

EA-6B

5

ENGINE SHUTDOWN AND CANOPY SAFETY1. ENGINE SHUTDOWNa. Retard throttles to the IDLE STOP position, then outboard (around the horn to the OFF position.

NOTE: A stop in the thottle quadrant prevents simultaneous movement of both throttles to or from the off position. Only one engine at a time may be shut completely off.

b. Place Engine and Fuel Master Switches in the OFF position.

c. Place Master Generator Switches in the OFF position.

2. CANOPY SAFETYa. The canopy may be safetied by inserting the Canopy Safety Lockpins in the forward and aft Canopy Jettison Handles located on the central instrument panel.

Insertion of safety lockpins into the forward and aft canopy jettison handles DOES NOT eliminate jettison of the canopy by external emergency entry method. Emergency entry may still be accomplished with safety pins installed by using external emergency entry.

WARNING

1aTHROTTLES

2aINTERNAL CANOPY JETTISONHANDLE AND LOCKPIN

1cMASTERGENERATORSWITCHES

1bENGINE ANDFUEL MASTERSWITCHES

EA

-6B.

T.O. 00-105E

-9

EA-6B

6

SEAT SAFETYINGNOTE: The EA-6B is equipped with four Martin- Baker GRUEA-7 Ejection Seat.

1. NORMAL SEAT SAFETYING

NOTE: Immediately upon gaining access to the aircraft cockpit, if time permits and no hazardous condition exists, proceed with normal seat safetying procedures.

a. Place Safety Flag, located top forward center of seat, in the UP/LOCKED position and insert safety pin. This safes the face curtain pull ring.

b. Rotate the Alternate Firing Handle Lock, located forward center of seat bucket, to the UP/LOCKED (vertical) position and insert safety pin. The safes the D ring.

c. Insert safety pin into the Gas Sequence Gas Generator (right hand of pilot’s seat only) in multiseat aircraft only.

d. Insert Ejection Gun safety pin, located on aft top of seat, into the firing mechanism. This safes the rocket catapult.

1aSAFETY FLAGWITH SAFETY PIN

1dEJECTION GUNWITH SAFETY PIN

1cGAS SEQUENCEGAS GENERATORWITH SAFETY PIN

1bALTERNATE FIRINGHANDLE LOCKWITH SAFETY PIN

EA

-6B.

T.O. 00-105E

-9

EA-6BSEAT SAFETYING-Continued

7 1. NORMAL SEAT SAFETYING-Continued

e. Insert the safety pin into the Drogue Gun, located on the upper left side of seat.

f. Insert safety pin into the Rocket Motor Initiator Firing Mechanism Sear, located on the upper left side of seat near the Droque Gun.

g. After removing crewmember, insert Lock Assembly into the Emergency Release Handle, located the forward right hand side of the seat.

In multi-seat aircraft, all ejection seats must be safetied due to command ejection possibility. (This component will sequence all seats for ejection.)

When removing personnel from ejection seats, do not allow crewmembers or rescue personnel to become entangled in lower seat ejection handle or use the face curtain handle as a support or hand hold.

2. EMERGENCY SEAT SAFETYING

a. Comply with the first three steps of Normal Seat Safetying procedures on page EA-6B.6.

WARNING

WARNING

1gEMERGENCY RELEASE HANDLE

1gLOCKASSEMBLY

1fROCKET MOTOR INITIATORFIRING MECHANISMWITH SAFETY PIN

1eDROGUE GUNWITH SAFETY PIN

EA

-6B.

T.O. 00-105E

-9

EA-6B

8

AIRCREW EXTRACTION3. AIRCREW EXTRACTIONNOTE: The crewmember is attached to the ejection seat by the use of an integrated harness and leg restraints (at thighs and ankles). Additionally, the oxygen/communication lead and anti-G suit hose are attached to the personnel services block on the left side of the seat.

a. Remove oxygen mask by pulling down on release tabs on either side of the mask.

b. The oxygen/communication lead is joined by a positive locking ring, located on the lower aft left side of the seat. Pull up on collar while pulling apart the connection.

c. Disconnect the anti-G suit hose, located on the lower aft left side of the seat, by pulling hose from personnel services block disconnect.

d. Release the leg restraint lines by pulling the leg line snubber release lever located on the outer side of each snubber box.

e. Release the two lap belts by squeezing the latch and release bar simultaneously.

f. Release the two shoulder harness koch fittings by squeezing the latch and release bar simultaneously for each fitting.

4. EMERGENCY RELEASE

a. Squeeze Emergency Restraint Release Handle and rotate aft. This releases lap belts, shoulder harnesses, and leg restraint lines.

NOTE: Survival kit and parachute will remain attached to crewmember and will have to be disconnected manually before extraction to avoid more effort and possible delay in the rescue process.

3aOXYGEN MASKRELEASE TAB(TYPICAL BOTHSIDES)

3bOXYGEN/COMMUNICATIONLEAD

3cANTI-G SUIT HOSEDISCONNECT

3dLEG LINE SNUBBERRELEASE LEVER

4aEMERGENCYRESTRAINTRELEASEHANDLE

3e,fKOCH FITTINGSFOR LAP BELTAND SHOULDERHARNESSES

E-8C

. E-8CT.O

. 00-105E-9

AIRCRAFT PAINT SCHEME

1

E-8C

. E-8CT.O

. 00-105E-9

2

AIRCRAFT DIMENSIONSNOTE• DIMENSIONS GIVEN AT FULL WEIGHT• HEIGHT AND GROUND CLEARANCE INCREASES 4 TO 6 INCHES AT EMPTY WEIGHT• MISSION RADOME GROUND CLEARANCE IS 1 FOOT 7 INCHES

145 FT 6 IN

42 FT 6 IN14 FT 2.5 IN

18 FT 3 IN

BODY STA 130

TOP OF FLOOR 10 FT 1 IN

4 FT 8 IN4 FT 8 IN 59 FT

17 FT 5 IN 5 FT 10 IN

152 FT 11 IN

71 FT 9 IN

12 FT 4 IN

145 FT 9 IN

51 FT 11.5 IN

33 FT 45 FT 8 IN

7DIHEDRAL

7DIHEDRAL TRUE

0

0

12 FT 1 IN

4 FT 7 IN 2 FT 9 IN 22 FT 1 IN

E-8C

. E-8CT.O

. 00-105E-9

3

AIRCRAFT HAZARDSNOTE: Skin penetration could be hazardous to the crew and passengers of this special purpose aircraft. Use Fire Drill 2 at marked areas only. For the engines, penetrate through the fire extinguisher panels. See page C-135.1.

WEATHER RADAR RADIATION AREA

If weather radar is operating:

• 60 foot area is hazardous to personnel. Over exposurecould result in sterility.

• Within 100 feet of nose radome area for possible fuel vaporignition to any equipment being refueled or defueled anddetonation of ungrounded electro explosive devices.

ANTENNA LOCATIONS

Operating distances indicated in FEET that can ignite fuel vapors. If operating, safe personnel limit is FEET. Transmission could cause shock. If mission radar is operating, distance is 1,000 feet.

1. GLIDESCOPE2. TACAN/UHF {200} [4]3. VHF AM/FM {200} [4]4. ADF LOOP5. IFF/UHF {200} [4]6. MISSILE WARNING SYSTEM7. GPS8. RAP HDIS9. SDS/TACAN10. UHF L-BAND11. X-BAND TRANSPONDER12. SCDL (2) {200} [15]13. RAP HDIS

WARNING

WARNING

14. UHF/JTIDS {200} [3]15. ELT16. VOR/ILS17. HF PROBE (2) {200} [10]18. UHF (5) {200} [4]19. RADIO ALTIMETER (4)20. SDS/JTIDS21. SINCGARS (GROWTH)22. ADF SENSE23. MARKER BEACON24. JOINTS STARS RADAR25. IFF26. WEATHER RADAR

2400

012060 FEET

100 FEET

1

2 3 4 5 6 7 8 9 7 10 10 11 12 13 14 15 16

26

25 18 24 3 23 2 22 21 20 6 19 19 12 18 18 172 3 1818

E-8C

. E-8CT.O

. 00-105E-9

4

AIRCRAFT HAZARDS-ContinuedHYDRAULIC SYSTEM• There are two hydraulic systems; auxiliary and utility systems

normally operate at 3,000 PSI.• No. 1 auxiliary reservoir is located in the left wheel well.• No. 2 auxiliary reservoir is located in the right wheel well.• Quantity is 3.2 gallons of SKYDROL LD-4. This fluid is toxic

and flammable. Face shield, gloves, and area ventilation isrequired. Avoid contact with skin, eyes, and clothes or injurywill result.

• The utility reservoir, holding 6.9 gallons, is located in the leftmain wheel well.

OXYGEN SYSTEM• There is a single oxygen system supplying oxygen for both the

flight and mission crews.• Liquid oxygen is stored in a 75-litre capacity converter,

equipped with a shutoff valve, located on left side fuselage inthe aft cargo compartment.

• There are 34 portable oxygen bottles located throughout.• Each bottle is charged to at least 290 PSI.

OIL SYSTEM• Engine oil systems are normally serviced with MIL-L-7808 oil

which is toxic. Use face shield, gloves, and ventilate areawhere present.

PNUEMATIC SYSTEM• There is an emergency brake air bottle, charged to 1,200 PSI,

located forward in the nose wheel well.

GALLEY HAZARDS• Located on left side between forward main door and crew rest

seats. An oven, electrical wiring, possible microwave oven, twocoffee makers with hot and cold water dispensers, two hot cupsfor heating liquids, and two dual-temperature refrigerator-freezers are fuel vapor ignition sources.

FWD LOWER COMPARTMENT AFT LOWER COMPARTMENT

MISSIONCREW

MISSIONCREW

MISSIONCREW

MISSIONCREW

MISSIONCREW

MISSIONCREW

ATWS ATWS

ATWS ATWS

LAVATORY

ATWS

ATWSFLIGHTDECK

CREW REST AREA CREW REST AREA

CREWRESTAREALAVATORY NOWS

PRESSURE DEMANDOXYGEN REGULATOR(39) (TYPICAL)

RECHARGER STATION (15)(TYPICAL)

FILL/BUILDUP/VENTVALVE DRAIN VALVE

LOX CONVERTERCRYOGENIC ISOLATIONSHUTOFF VALVE RELIEF VALVEHEAT EXCHANGER (3)DRIP APN (3)

PORTABLE OXYGENBOTTLE (34) (TYPICAL)

OXYGENPRESSURESWITCH

E-8C

. E-8CT.O

. 00-105E-9

5

AIRCRAFT HAZARDS-Continued

BATTERY

AIR REFUELINGRECEPTACLE

DUAL SINGLE POINTREFUELINGRECEPTACLES

VENT SURGE TANK

VENT SURGE TANKOVERWING FILLERPORT (7)

APUBATTERY

RESERVE TANK NO. 4439 GAL

MAIN TANK NO. 42,323 GAL

MAIN TANK NO. 34,069 GAL CENTER TANK 10,193 GAL

APU

MAIN TANKNO.24,069GAL

MAIN TANKNO.12,323GAL

RESERVETANK NO.1439 GAL

FUEL TANK LOCATIONS AND QUANTITIES• Fuel type is JP-8• US Gallons

AIRCRAFT BATTERY• 24 Volt Lead Acid• Located on an extendable mount in a

compartment in right lower nose section.

APU BATTERY• 24 Volt Nickel Cadium• Located in right wheel well on aft bulk-

head (station 960) below electroniccontrol box.

APU (GAS TURBINE)• Located in aft lower compartment and is

enclosed in a fireproof shroud.

E-8C

. E-8CT.O

. 00-105E-9

6

SPECIAL TOOLS/EQUIPMENTPower Rescue Saw25 Foot LadderFire Drill 2AIRCRAFT ENTRY

1. NORMAL ENTRYa. To open entry doors, located left forward

and left aft fuselage, pull external handleoutward and rotate clockwise.

b. Pull door outward.

2. EMERGENCY ENTRY

a. Same as NORMAL ENTRY doors.b. To open cargo doors, located forward

and aft right fuselage, press catch onrelease handle.

c. Pull handle down to unlock door.d. Push door in and slide door forward.e. To open bailout door, located aft of

cargo doors, and pull external handleoutward and rotate counterclockwise.

f. Pull door outward.g. To open electronic compartment door,

located forward of nose gear, presscatch to release handle.

h. Rotate handle counterclockwise.i. Push door inward.j. To open hatches, located over and just

aft of either wing, push in panel.k. Push hatch inward.l. Co-pilot’s sliding window can be opened

from the outside for entry.

NOTE: Some doors are pushed inward to release from fuselage opening. Leaving door or hatch in opening will impede rescue.

3. CUT-IN

a. Cut-in only at indicated marked area.

ELECTRONIC COMPARTMENT EXTERNAL DOOR HANDLE HATCHES PUSH PANEL

BAILOUT DOOREXTERNAL HANDLE

BAILOUTDOORCARGO

DOORSHATCHES

ELECTRONICCOMPARTMENT

ENTRY DOOR CARGO DOOR

ENTRY DOOREXTERNAL HANDLE

ENTRY DOOR

HATCHES

CATCH

LOCKED

UNLOCKED

CARGO DOOR EXTERNAL HANDLE

E-8C

. E-8CT.O

. 00-105E-9

7

ENGINE AND APU SHUTDOWN4. ENGINE SHUTDOWN

NOTE: Aircraft is equipped with thrust reversers.

a. Place engine thrust lever friction handle,located on control stand, to aft position,then retard engine thrust levers to IDLEposition.

b. Place engine start levers, located on lowerportion of control stand, down to CUT-OFFposition.

c. If no engine or APU fire, proceed to step f.d. If an engine or APU fire is observed or

indicated, pull engine fire switches or T-handles, located on pilot’s instrumentpanel and APU T-handle on cabin APUpanel, OUT to discharge agent.

e. Press the engine or APU fire dischargebuttons and hold for 2 seconds. Enginebuttons are located top of pilot’s centerinstrument panel. APU button is locatedon the aft bulkhead right of cabin door onAPU panel or remote panel located on leftside fuselage aft of left wing root.

f. Place guarded battery switch, located onupper left flight engineer’s panel, to OFF.

4dENGINET-HANDLES

4fBATTERYSWITCH

4aFRICTIONLEVER

4bTHROTTLELEVERS

4d,eAPUPANEL

APU AREA

REMOTE APU PANEL

APUBATTERYSWITCH

4eAPUT-HANDLE

FIREWARNINGLIGHT

4eEXTINGUISHERDISCHARGEBUTTON

4dAPUT-HANDLE

4eEXTINGUISHERDISCHARGEBUTTON

APU CONTROL PANEL

APU FIRECONTROL

E-8C

. E-8CT.O

. 00-105E-9

8

AIRCREW EXTRACTION5. AIRCREW EXTRACTION

NOTE: Flightdeck seating arrangement is the same for C/KC-135 aircraft.

a. The pilot, co-pilot, flight engineer, navigator,and observer seats are all equipped with aseat belt and inertia reel shoulder harness.

b. To release crewmember from seat, turn thesingle release rotary buckle.

c. To release the shoulder harness only, pressthe black tap on the rotary buckle.

d. For easier extraction, the seats have variousadjustments; tilt, horizontal, and vertical.These adjustments are located on the rightside of the seat except for the co-pilot andflight engineer which are on the left side.

e. There are twelve crew rest seats, locatedjust aft of forward lavatory (see page

E-8C.2), are equipped with seat belts only.f. There are three crew rest bunks, located aft

of left side crew rest area (see page E-8C.2), are equipped with seat belts.g. Passenger seats are equipped with seat

belts only.h. The aircraft has three lower compartment

interior access hatches. Personnel may befound in these areas at any time.

HINGES

FORWARD LOWERAVIONICS BAYINTERIOR ACCESSHATCH FORWARD LOWER

COMPARTMENTINTERIOR ACCESSHATCH

AFT LOWERCOMPARTMENTINTERIOR ACCESSHATCH

LATCH

HATCH

HATCHVIEWING WINDOW

VIEWINGWINDOW

PULLHANDLE

E-8C

. E-8CT.O

. 00-105E-9

9

AIRCRAFT INTERIOR ARRANGEMENT1. STORAGE2. LAVATORY3. CREW REST TABLE4. CREW BUNKS5. NOWS CONSOLE6. COMM RACKS 2-57. OWS CONSOLES8. DATA RACK 7B9. EMERGENCY EQUIPMENT RACK10. DATA RACK 7A11. DATA RACK 812. SAFE13. BAILOUT EQUIPMENT STORAGE14. DATA RACK 515. DATA RACK216. AFT LOWER COMP. ACCESS HATCH17. 400-60 HZ CONVERTER18. EMERGENCY EQUIPMENT PANEL19. LIQUID OXYGEN BOTTLE20. PORTABLE WATER TANK21. VAPOR CYCLE22. VAPOR CYCLE INLET23. LOX HEAT CONVERTERS24. CARGO ENTRY LADDER25. LADDER26. APU INLET DUCT27. APU28. APU EXHAUST DUCT29. RADIO ALTIMETER T/R30. COMM RACK 131. LIFERAFT STORAGE CONTAINER32. LIFERAFTS33. DATA RACK 6A-6D34. DATA RACK 9A & 9B35. COAT CLOSET36. FWD LOWER COMP. ACCESS HATCH37. INTERTIAL NAVIGATION UNITS38. TOOL STORAGE RACK39. RADAR CIRCUIT BREAKER PANEL

40. CIRCUIT BREAKER PANEL41. TRANSFORMER-RECTIFIER UNITS42. RADAR LRU’S43. LOWER COMPARTMENT ACCESS STAIRS44. RADAR LIQUID COOLING HEAT EXCHANGER45. RADAR TRANSMITTER RACK46. JUNCTION BOXES47. EMERGENCY EQUIPMENT RACK48. GALLEY49. FOOD LOCKER

12

3

56

4

78 9 7

7 77

7

7

10

7

11 1122

13

141516

3031327333435

364849

1

4647 37 38 39

4041

4243

4445

2829 17 1819

20

21

2324 222526

27

E-9A

. E-9AT.O

. 00-105E-9

1

AIRCRAFT HAZARDS

NO. 1 SYSTEM HYDRAULIC RESERVOIR

NOTE: NO radiation associated with right fuselage pod.

NOTE: This Tyndall AFB Drone System aircraft has no composites in the aircraft materials.

STANDARD FUEL TANKS US GALS LITRESTOTAL CAPACITY 846 3202

SINGLE TANK DIVIDE BY 2FUEL TYPE: JP-8

HYDRAULIC FLUID US QTS LITRESNO.1 SYSTEM RESERVOIR 2.68 2.50NO. 2 SYSTEM RESERVOIR 5.19 4.90NOSE RESERVOIR 1.25 1.20

ALL SYSTEMS USE PHOSPHATE ESTER-BASEDFLUID eg.SKYDROL

NO. 1 SYSTEM HYDRAULIC RESERVOIR

NOSE GEAR WHEELWELLHYDRAULIC RESERVOIR

CREW OXYGEN CYLINDER

NOSE RADAR +/- 60DEGREE SWEEPRANGE 100 FT/3,048 Cm.NOTE: System is on during landing.

BATTERY2 EACH

NITROGEN BOTTLE

NO. 1 TANK OVERWINGREFUEL POINT

PRESSURE REFUEL POINT

NO. 2 TANK OVERWINGREFUEL POINT

TOTAL OIL CAPACITYFOR BOTH ENGINESUS GALS LITRES 11.09 42

US AIR FORCE

E-9A

. E-9AT.O

. 00-105E-9

AIRCRAFT HAZARDS-Continue

2

WARNING

• Hot exhaust gases are vented aft of engines.

• Shaded areas represent rotating propeller areas, hot exhaust engine gases and APU hot exhaust gas.

CO-PILOT OXYGENSUPPLY OUTLET

OXYGENINDICATOR

DISCHARGEINDICATOR

CREW OXYGENCYLINDER ASSY(39.4 FT3)(1.1 m3)

CO-PILOT’SOXYGEN MASK

PILOT’S OXYGENMASK

PILOT’S OXYGENSUPPLY OUTLET

CREW PORTABLEOXYGEN CYLINDER(11.4 FT3) (0.3 m3)

APU EXHAUST*

*NOT ALL AIRCRAFT

0 3.05 6.10 9.14 12.19 15.2 18.3 21.3 24.4

0 10 20 30 40 50 60 70 80

0 0

10 3.05

20 6.10

30 9.14

40 12.19

50 15.2

60 18.3

70 21.3

METRESFEET

FEET

METRES

NOTE: Oxygen system is gaseous type.

E-9A

. E-9AT.O

. 00-105E-9

AIRCRAFT DIMENSIONS

3

NOTE: DIMENSIONS TO GROUND LINE INDICATED:• ARE APPROXIMATELY ONLY AND VARY

DEPENDING ON LOADING CONDITIONS ANDAIRCRAFT CONFIGURATION.

• BASIC WEIGHT WILL VARY DUE TO CON-FIGURATION AND MODIFICATION NO FUEL,NO PAX OR CREW.

WHEELS EXTENDEDA= 125.00 IN. (3.18m)B= 43.00 IN. (1.09m)C= 63.00 IN. (1.6m)

WHEELS RETRACTEDAPPROX 2 FT (.61m)LOWER IN WHEELSRETRACTED SITUATION

*BASIC WEIGHT - 21,047GROSS WEIGHT - 33.2 0 lb (15,059 kg)SEATING CAPACITY - UP TO 36 PAX AND 3 CREW

85 FT 0 IN(25.89 m)26 ft 0 IN (7.93 m)

3 FT 1 IN(937 m)CLEARANCE(STATIC)

11 FT 11 IN (3.63 m)

13 FT 0 IN DIAMETER(3.96 m)

25 FT 10.4 IN (7.88 m)

AB BC

26 FT 1IN (7.95 m)

73 FT 0.1 IN (22.26 m)

24 FT 7 IN (7.49 m)

6 FT 8 IN (2.03 m)

4 FT 11 IN

(1.49 m)

8 FT 4 IN (2.54 m)

4 FT 3 IN (1.3 m)

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AIRCRAFT SKIN PENETRATIONPOINTS AND CUT-IN AREAS

4

1. AIRCRAFT SKIN PENETRATION POINTS AND CUT-IN AREAS

a. Areas require the Fire Drill II for penetration and a power rescue saw for cut-in. It is recommended that a major effort to gain access be directed to hatches and doors due to the type of structure and possible injury to personnel within.

b. There is no externally accessible engine fire access panels.

c. The third window (see color filled window) aft of airstair door is recommended for first choice cut-in (any window is suitable).

TYPICAL CUT-IN AREA DIMENSIONS(42.0 X 20.0 IN) (1067 X 508m)

PASSENGERCOMPARTMENT WINDOWS

CUT-IN AREAS(TYPICAL BOTH SIDES)

SIDE WINDOW(NON OPENING)

WINDSHIELD

INTAKE TO GROUND LEVEL (7.53 FT) (2.30m)

EXHAUST TO GROUND LEVEL(7.53 FT) (2.30m)

NOTE: Approximately 2 feet lower in wheels-up situation.

Interior Construction− Stringers run above & below windows− Skin thickness .060 In. (1.50mm)

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ESCAPE ROUTES AND OVERHEADEMERGENCY ESCAPE HATCH

5

HATCH OPERATION

NOTE: Opening hatch permits depressurization and modest amount of ventilation.

a. To open, rotate handle 72 degrees counterclockwise.b. Pull downward on handle using 40 pounds of force to release mechanisms allowing hatch to be completely removed.

NOTE: In an emergency it may be possible by cutting through the outer skin to gain access to reposition the operating handle from outside and then force the hatch downwards.

SPRINGROLLER

DETENT

TORQUESHAFTASSEMBLY

ARM

OVERCENTERSPRING

OPERATINGHANDLE

ROLLERSPRING

SEAL

10 X 8 IN. (254 X 203mm)

REAR SUPPORTFITTINGS

FORWARDFLIGHTDECKEMERGENCYEXIT HATCH

ENTRYDOOR

ESCAPEROPE

Beware of operating propellerswhen using the Entry Door andForward Cabin Emergency Exit.

WARNING

MID CABINEMERGENCYEXIT

MID CABINEMERGENCYEXIT

OVERHEADFLIGHTDECKEMERGENCYEXIT HATCH

VENT CLOSED

PULL HANDLE DOWN TO REMOVE HATCH

LAVATORY

UHF & FM Retransmit Rack Unit 5

R

ecor

der

Rac

k

U

int 3

R

ecei

ver

Rac

k

U

int 4

RadarOperator’s Console Unit 2

CARGODOOR

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FLIGHTDECK AND CABIN ARRANGEMENT

6

CREW - 4PASSENGERS - 4

FLIGHTDECK

PILOT COPILOT

EMERGENCY EXITS RIGHT SIDE BOTH SIDES 20.2 IN X 55.3 IN 20.2 IN X35.6 IN (513MM X 1403 MM) (523 MM X 904 MM)

CARGO DOOR

PASSENGER CABIN LENGTH 30 FT 1 IN (9162mm)

107 IN(2718 mm)

43 IN (1092 mm) (NOMINAL)

AFT VIEW OF FLIGHTDECK

FORWARD VIEW

LAVATORY LIFERAFT

FIRE EXTINGUISHER RADAROPERATOR TM

OPERATOR

FIREEXTINGUISHER

CARGO DOOR50 IN WIDE X 60 IN HIGH (1270 X 1524 mm)

RECORDER RACK

TM RACKRADARSTATION

FIRE EXTINGUISHER

AVIONICS RACKS

ENTRY DOOR30 IN WIDE X 66 IN HIGH(762 X 1676 mm)

WARDROBE

PASSENGER SEATING

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SPECIAL TOOLS/EQUIPMENTPower Rescue SawFire Drill II

7

1. NORMAL ENTRYa. Approach aircraft on left side staying close to the

fuselage and away from propeller and heatedengine cowling.

b. Locate entry door and open by pulling the dooraccess handle down and support door whilelowering.

c. If step 2 fails, go to rear cargo door and pushrelease button and rotate butterfly control handleclockwise until door unlocks, then raise door upuntil door locks in place. Door only opens from theoutside.

2. EMERGENCY ENTRYa. Use entry door.b. Use cargo door as a secondary option. (1) Push center (red) button, RT and LT handles

will pop out (2) Turn counterclockwise (3) Lift doorto open - handle to be flush in open position.

c. For mid cabin emergency exit doors, push handlerelease button to extend handle.

d. Rotate operating handle counterclockwise downand push exit door in.

3. EMERGENCY EXITSa. Once inside aircraft, to use the mid cabin emergency exit door, pull internal operating handle down and then pull exit door in.b. When using the emergency escape hatch use the jump seat for step up. Release latch is at lower right of seat.c. Cargo door - to open, pull knob while turning handle clockwise until knob retracts. Ensure knob is fully retracted before raising door. (See page E-9A.8.)

NOTE: Right side cabin emergency exit doors may be partially blocked by antenna array fairing.

3. CUT-INa. Using a power rescue saw, cut around the passen- ger compartment windows. First window of choice is third windows. First window of choice is third window aft of entry door; however, any window is suitable.

NOTE: AF version with right side fuselage fairing for large, electronically steerable phased array antenna, a ventral radome, and extensive internal avionics and electronics.

FORWARD CABINEMERGENCY EXITDOOR (20.2 IN X 55.3 IN)

FLIGHT DECKEMERGENCY HATCH

MID CABIN EMERGENCY EXIT DOORS (20.2 IN X 35.6 IN) (513 MM X 904 MM)

REAR FUSELAGE ACCESS DOOR (AC UNIT)

CARGO DOOR (50.0 IN X 60.0 IN)(1270 MM X 1524 MM)

ENTRY DOOR(30.0 IN X 66 IN)(762 MM X 1676 MM)

NOSECOMPARTMENT DOORS(LT TOP - DC CONTACTORBOX, BOTTOM - NICADBATTERIES (2) & BOTTOMRT - CREW OXYGEN)

2cMID CABINEMERGENCYEXIT EXTERNALOPERATION

3aMID CABIN EMERGENCYEXIT INTERNAL OPERATION

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CREW AND PASSENGER ESCAPE SYSTEMS

8

WARNING KEEP CLEAR OF DOOR PULL HANDLEOUT AND DOWN TO OPENSUPPORT DOORWHILE LOWERING

PUSH

OPEN PUSH

PUSH PUSH TO RELEASE

PUSH TO RELEASE

PULL HANDLE AND TURN TO OPEN

PULL HANDLE AND TURN TO OPEN

LIFT DOOR TO OPEN CAUTIONHANDLE TO BE FLUSH IN OPEN POSITION

PUSH BUTTON

CARGO DOOREXTERNAL VIEW

WINGED EXTERNAL HANDLE (IN OPERATION)

TURN HANDLE DOWN AND PUSH HATCH INOPEN

POSITION

OVERHEADESCAPE HATCH

CREW EMERGENCY DESCENT DEVICE(TYPICAL BOTH SIDES)

RIGHT SIDE VIEW

LEFT SIDE VIEW

CARGO DOORINTERNAL VIEW

TO OPEN PULL KNOB WHILETURNING HANDLE IN DIRECTION OFARROW UNTIL KNOB RETRACTS

NOTE: Ensure knob is fully restracted before raising door.

OPEN

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ENGINE SHUTDOWN ANDAIRCREW EXTRACTION

9

4. ENGINE SHUTDOWNNOTE: Electrical power must be present.

a. Pull both engine condition levers AFT, located on centerconsole, to FEATHER position, then raise finger lifts onlevers, to the IDLE position.

b. Pull both fuel shutoff “T” handles, located on the overheadconsole, to shutoff fuel flow and hydraulic power.

c. Place battery master switch, located on the overhead consoleabove pilot’s head, to the OFF position.

d. Place main (external) power switch, located next to masterbattery switch, to OFF position.

e. To disconnect 2 28VDC batteries, open access panel in leftlower nose, break safewire, turn terminal knobs counterclock-wise.

5. IN CASE OF ENGINE FIRE

a. Electrical power must be present for fire bottles to operate.b. Pull fuel “T” handle.c. Push extinguisher toggle switch either aft to discharge bottle

#1 or forward to discharge #2.

NOTE: Fire bottles and agent discharge indicators are located under left wing root. Agent discharge indicator will show YELLOW if agent has been used and RED if there is a thermal agent escape.

6. CREW EXTRACTION

a. Release inertia reel controls, inboard at elbow, to unlockshoulder harnesses of forward seats.

b. Rotate harness release dial, in either direction, to release lapbelt and shoulder harness for the forward and two workstationseats.

c. Pull lever up at right corner of both forward seats to tilt backfor easier extraction.

d. Disconnect the lap belts of the two passenger seats withoutworkstations.

1dMAINPOWERSWITCH

1cMASTERBATTERYSWITCH

1bFUELSHUTOFFT-HANDLES

1aENGINE CONDITION LEVERS

RED

YELLOW

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AIRCRAFT PAINT SCHEME

1

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RADAR, HF, AND IR RADIATION

AIRCRAFT HAZARDS

1. RADAR· 50 foot area hazardous to personnel· Within 100 feet, possible fuel ignition and electro explosive device detonation

2. HF ANTENNAS

· Ground operation of the HF radios is prohib- ited unless the aircraft is at least 200 feet from the following:

(a) unloaded weapons or warheads(b) loaded weapons in an aircraft with

bomb bay doors open.(c) Missiles with warhead compartment

doors open, or thruster and squib access door open.· Do not transmit on the HF radio when in contact with or in close proximity to the KC- 10 air re- fueling boom, as this may cause uncommanded movement of the boom, endangering the tanker or receiver aircraft and crews.

3. IRCM· Ensure no unnecessary personnel are within 19 feet of the radiating side of an operating IRCM unit, (covert filter assembly installed). Personnel required to be within 19 feet should not look at the IRCM unit windows without appropriate IR safety glasses.

2

100FEET

50FEET

1200

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3

AIRCRAFT HAZARDS-ContinuedENGINES, APU AND NOISE

200 FT

150 FT

100 FT

100 FT

50 FT

75 FT

340 F240 F140 F

0

0

0

TEMPERATURE

25 FOOT RADIUS

IDLE THRUST

NOISE HAZARD AREASNOTE: Includes 20 knot crosswind effect.

APU EXHAUST GAS TEMPERATURE

DISTANCE IN FEET0 10 20 30 40 50 60 70 80

1200 F 500 F 300 F 200 F0 0 0 0

INLET SUCTION DANGER

WIND VELOCITY APPROXIMATELY 145 TO 105 MPHWIND VELOCITY APPROXIMATELY 105 TO 65 MPHWIND VELOCITY APPROXIMATELY 65 TO 20 MPH

WIND VELOCITY APPROXIMATELY 210 TO 145 MPH

150 FT 100 FT 50 FT 0 50 FT 100 FT 150 FT

WARNING

Prolonged exposure of one hour, even withear protection, can cause ear damage.

Ear protection required within this area.

POWER SETTING RADIUS RADIUS

GROUND IDLE 75 FT 100 FTBREAKAWAY 100 FT 150 FT THRUST 52% N1TAKEOFF THRUST 100 FT 200 FT

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4

AIRCRAFT HAZARDS-ContinuedNOISE: APUs AND 3 Air Conditioning Packs

Measured 5 feet above ground Measured 5 feet above floor

1 foot outside door centerline Measured 1 foot below aircraft skin

CONDITIONS: Sound levels in dB Standard day 3 A/C pack in max cooling 2 APUs operating

NOTE: These conditions represent the highest noise environment associated with normal servicing.

Ear protection is required for noise levels above 85 decibels.

WARNING

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AIRCRAFT HAZARDS-Continued

5

OXYGEN SYSTEMS

NOTE: The aircraft oxygen system is divided into three separate and independent systems: the flightcrew, passenger, and medical dispensary oxygen systems. The dedicated storage cylinders for these systems are located right side of forward cargo compartment aft of the forward cargo door. (See illustration.) In addition, portable oxygen bottles are located throughout the aircraft to provide protective and emergency oxygen.

OXYGEN SHUTOFF VALVES All shutoff valves are closed by turning the cylinder shutoff valve knob clockwise. The flightcrew system has two (2) cylinders, passenger system has five (5) cylinders and the medical dispensary system has three (3) cylinders. Each cylinder, when fully charged to 1850 PSI at 70 degrees F, contains 114 cubic feet of oxygen at standard sea level pressure.

WARNING

If valves need to be opened, open valves slowly or excessive temperatures may result.

Residual pressure can be as high as 1850 PSI and oxygen could escape with considerable force.

CYLINDERSHUTOFFVALVE

CYLINDERCOUPLING

PRESSUREREDUCER

MEDIUMPRESSURELINE

PRESSURETRANSDUCER

PASSENGEROXYGENCYLINDER(TYPICAL)

OXYGEN CYLINDER ASSEMBLY

OVERBOARDDISCHARGE LINE

CYLINDERPRESSURE GAGE

THERMAL COMPENSATOR

CHECK VALVEFILLER LINE

PASSENGEROXYGENCYLINDER

CREWOXYGENCYLINDERS

MEDICALOXYGENCYLINDERS

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6

SPECIAL TOOLS/EQUIPMENTPower Rescue Saw35 Foot LadderSPAAT/Fire Drill IIAIRCRAFT ENTRYALL AIR FORCE 1 MODELS

1. NORMAL/EMERGENCY ENTRYa. Pull entry door handles from recess position and rotate 180 degrees clockwise for entry doors located on far left side and counterclockwise for entry doors on right side.

NOTE: All main deck entry door open forward. Number (3) left side entry door and number (1) and (3) right side entry doors are blocked.

b. Press release button on crew escape hatch, located top forward center of crew compartment, and rotate escape hatch 180 degrees clockwise. Push escape handle inward.c. Pull handle, located on crew door, and rotate 180 degrees counterclockwise. Push door inward until slide tracks are engaged, then slide door aft.

Opening a door from the outside disengages the emergency evacuation system and the escape chute/ slide will not deploy.

NOTE: All emergency escape chutes/slides are deployed from inside the aircraft only.

2. CUT-INa. Cut areas along the window lines as a last resort with the power rescue saw.b. Use SPAAT/Fire Drill II for skin penetration points as illustrated for the E-4 on pages E-4.1,.2, and .3.

WARNING

NOTE: 23 Crewmembers 70 Passengers

NOTE: Total Fuel 53,611 US Gallons

VENT SURGE TANK

MAIN BATTERFLIGHT DECK

DOOR IRBLOCKED

OXYGEN CYLINDERS

CREW DOOR(RIGHT SIDE ONLY)

ENTRY DOORS

DOOR 3L AND 3R BLOCKED

APU 1 AND APU 2BATTERIES

APU 2

APU 1789

12,579511

4,350

17,204 12,5794,350 511 789

VENTSURGETANK

1bRELEASEBUTTON

1bESCAPE HATCHHANDLE

1cENTRY DOORAND CREWDOOR EXTERNALHANDLE

1aENTRY DOOREXTERNALHANDLE(LEFT SIDE)

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7

ENGINE SHUTDOWN1. ENGINE SHUTDOWN

a. Retard thrust levers, located on pilot’s center console, to IDLE position.b. Place engine start levers, located on pilot’s center console, to CUTOFF position.c. If engines fail to shutdown, pull emergency fire T-handles, located on pilot’s overhead panel.d. Place battery switch, located on flight engineer’s center panel , to OFF position.e. Place APU1 and APU2 switches located on flight engineer’s upper left panel, to STOP position.f. If APUs fail to shutdown, pull APU1 and APU2 emergency fire T-handles, located on flight engineer’s overhead panel.g. To shutdown APUs outside of aircraft, press and hold APU1 and APU2 shutdown switches for a minimum of 5 seconds.

1fAPU 1 AND APU 2 FIRESHUTDOWN T-HANDLES

1eAPU 1 AND APU 2 FIRE SWITCHES

1cENGINE EMERGENCYFIRE T-HANDLES

1aTHRUSTLEVERS

1bENGINE STARTLEVERS 1d

BATTERY SWITCH

APU EMERGENCY SHUTDOWN EXTERNAL PANEL

1gAPU 1 ANDAPU 2SHUTDOWNSWITCHES

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8

AIRSTAIR OPERATION

1. AIRSTAIRS CONTROLS

a. Fully open the exterior door lock handle.

b. Place and hold the control switch in the OPEN EXTEND position until the airstairs fully extends and contacts the ground. Release control switch when the EXTENDED position light comes on.

NOTE: The door lock handle may be closed or left open after extending the airstairs.

FORWARDAIRSTAIR

AFT AIRSTAIR

1aEXTERIORDOOR LOCKHANDLE

1bCONTROLSWITCH

1bLIGHT

EXTERIOR CONTROL DOOR (DOOR HANDLE OPEN)

FULLY EXTENDED AIRSTAIR

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9

CABIN CONFIGURATION

1 2 3

7654

1 CONTROL CABIN2 CREW REST AREA/COMMUNICATIONS CENTER3 MAIN DECK

4 COMMUNICATIONS EQUIPEMENT5 FORWARD LOWER COMPARTMENT6 AFT LOWER COMPARTMENT7 BULK CARGO COMPARTMENT

COMMUNICATIONS

LUGGAGE

FLIGHTDECK, UPPER DECK REST AREA, AND COMMUNICATIONS CENTER

LOWER FORWARD COMPARTMENTFWD

FWD

LOWER AFT COMPARTMENT

GUEST SECURITY PRESS

STAFF/SECRETARIAL SECURITY SUPPORT CREW

FWD

SENIOR CONFERENCE/OFFICE ANNEX STAFF DINING

EXECUTIVE EXECUTIVE SECURITY FOYER SUITE ENTRY

AIRCRAFT INTERIOR

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10

AIRCREW EXTRACTION, SEATING AND POSITIONING

2. SEATING AND POSITIONING

PILOT’S SEAT

LEGEND

1. HEADREST ADJUSTMENT KNOB2. HARNESS/SEAT BELT ROTARY BUCKLE3. ARMREST ADJUSTMENT CONTROL BUTTON4. VERTICAL ADJUSTMENT CONTROL CRANK (not shown)5. CROTCH STRAP6. TILT CONTROL HANDLE7. HORIZONTAL CONTROL HANDLE8. RECLINE LOCK CONTROL HANDLE9. LUMBER SUPPORT ADJUSTMENT CONTROL KNOB

NOTE: Pilot’s seat is shown. Copilot’s seat is identical except seat controls are on the opposite sides.

1. AIRCREW EXTRACTION

a. Unlatch lap belts and remove shoulder harness from crewmembers.

b. Depress control handles and rotate flight engineer’s seat from left to right.

c. Passenger seats are equipped with lap belts only.

NOTE: If seat tracks are not damaged during crash landing, use adjustable seat controls to retract seats to aft position.

1

2

3

5

9

8

67

4

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11

AIRCREW SEATING AND POSITIONINGENGINEER’S/NAVIGATOR’S SEAT

LEGEND

1. SHOULDER HARNESS2. ARMREST SWIVEL CONTROL BUTTON3. RECLINE CONTROL HANDLE4. FORWARD/AFT CONTROL HANDLE5. VERTICAL CONTROL HANDLE6. SWIVEL CONTROL HANDLE7. LATERAL CONTROL HANDLE (not shown)8. CROTCH STRAP9. LAP BELT

1

2

2

345

9

8

7

6

OBSERVER’S SEAT

LEGEND

1. OBSERVER’S PANEL2. SEAT BACKREST3. FOLD-OVER CONTROL HANDLE (not shown)4. FORWARD/AFT CONTROL HANDLE (not shown)5. FOLDING AND STOWAGE CONTROL HANDLE6. RECLINE LOCK CONTROL HANDLE

1

2

5

6

6

5

2

1

4

3

STOWED POSITION UNSTOWED POSITION