WELCOME TO TECHNICAL ORDER 00-105E-9, 1 FEBRUARY 2006, … Segment 21.pdf · 2007. 12. 18. · POINTS (2 16” PLACES) 8 ... b. Press release button on crew escape hatch, located

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 21 COVERING CHAPTER 18 FROM THE 747 TO THE 777.

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 Retaining out of date rescue information can negatively affect the user’s operability and outcome of emergencies.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

SEGMENT 21 INFORMATION CHANGE NOTICE

None.

TO 00-105E-9

Chapter 18 Cover

NOTE

Chapter 18 contains emergency rescue andmishap response information for the following aircraft:

DC-3DC-6DC-7DC-8DC-9

DC-10MD-11MD-80MD-90

L-1011-1L-1011-500

707717720727737747757767777

747. 747T.O

. 00-105E-9

AIRCRAFT PAINT SCHEME1

747-100/-200 747-300

747-400

747. 747T.O

. 00-105E-9

2

-400/ -400 COMBI/ -400ER

AIRCRAFT DIMENSIONSNOTE:

This file contains many variations of the 747. Oldervariations may still be in use, therefore the infor-mation will be retained. The 747-400 series is themodel currently being marketed and the next threepages detailing the dimensions will be fully illus-trated. Previous models will not, but are typical incomparison.

229’ 2” (69.85 M)166’ 7” (50.78 M)

152’ 7” (46.51 M)

3

3

12

38’ 4”(11.68 M)

68’ 4”(20.83 M)

21’ 4”(6.50 M)

ENGINE INBOARD OUTBOARDCF6-80C2

PW4200

RB211-524H

75’ 6”

76’ 3”

78’ 11”

(23.01 M)

(23.24 M)

(24.05 M)

105’ 6”

106’ 4”

107’ 6”

(32.16 M)

(32.41 M)

(32.77 M)

231’ 10.75” (70.67 M)

55’ 10”(17.02 M)

25’ 5”(7.75 M)

84’ 0”(25.60 M)

10’ 1”(3.07 M)

747-400 COMBI

225’ 2” (68.63 M)

211’ 5” (64.44 M)213’ 0” (64.92 M)

12

GE: 9’ 4” (2.84 M)PW: 9’ 2” (2.79 M)RR: 8’ 6” (2.59 M)

72’ 9”(22.17 M)

36’ 1”(11.00 M) 12’ 7”

(3.84 M)JIG POSITIONAT MAX GROSS WEIGHT (FULL FUEL)

FEET 0 10 20 30 40 50SCALE

METERS 0 5 10 15

747. 747T.O

. 00-105E-9

AIRCRAFT DIMENSIONS - Continued

-400 FREIGHTER/ -400ER FREIGHTER

3

229’ 2” (69.85 M)166’ 7” (50.78 M)

152’ 7” (46.51 M)

3

3

12

38’ 4”(11.68 M)

68’ 4”(20.83 M)

21’ 4”(6.50 M)

ENGINE INBOARD OUTBOARD

CF6-80C2

PW4200

RB211-524H

75’ 6”

76’ 3”

78’ 11”

(23.01 M)

(23.24 M)

(24.05 M)

105’ 6”

106’ 4”

107’ 6”

(32.16 M)

(32.41 M)

(32.77 M)

231’ 10.75” (70.67 M)

55’ 10”(17.02 M)

25’ 5”(7.75 M)

84’ 0”(25.60 M)

10’ 1”(3.07 M)

225’ 2” (68.63 M)

211’ 5” (64.44 M)213’ 0” (64.92 M)

12

GE: 9’ 4” (2.84 M)PW: 9’ 2” (2.79 M)RR: 8’ 6” (2.59 M)

72’ 9”(22.17 M)

36’ 1”(11.00 M) 12’ 7”

(3.84 M)JIG POSITIONAT MAX GROSS WEIGHT (FULL FUEL)

FEET 0 10 20 30 40 50SCALE

METERS 0 5 10 15

747. 747T.O

. 00-105E-9

AIRCRAFT DIMENSIONS - Continued

-400 DOMESTIC

4

229’ 2” (69.85 M)166’ 7” (50.78 M)

152’ 7” (46.51 M)

3

3

38’ 4”(11.68 M)

68’ 4”(20.83 M)

21’ 4”(6.50 M)

ENGINE INBOARD OUTBOARD

CF6-80C2

PW4200

RB211-524H

75’ 6”

76’ 3”

78’ 11”

(23.01 M)

(23.24 M)

(24.05 M)

105’ 6”

106’ 4”

107’ 6”

(32.16 M)

(32.41 M)

(32.77 M)

231’ 10.75” (70.67 M)

55’ 10”(17.02 M)

25’ 5”(7.75 M)

84’ 0”(25.60 M)

10’ 1”(3.07 M)

225’ 2” (68.63 M) 195’ 8”(59.63 M) 1

2

GE: 9’ 4” (2.84 M)PW: 9’ 2” (2.79 M)RR: 8’ 6” (2.59 M)

72’ 9”(22.17 M)

36’ 1”(11.00 M) 12’ 7”

(3.84 M)FEET 0 10 20 30 40 50SCALE

METERS 0 5 10 15

747. 747T.O

. 00-105E-9

5 AIRCRAFT PENETRATION POINTS

BULK CARGO DOOR (NOT ON 747-SP)

PENETRATIONPOINTS (2PLACES)16” 16”

8”

HANDLE

FWD

AFT CARGO DOOR

UPPER AFTACCESS PANEL

HANDLE10”

5”

PENETRATIONPOINTS

FWD

3” 8”

6”

HANDLE

PENETRATIONPOINT

FWD

FWD

PENETRATIONPOINT

HANDLE

FWD CARGO DOOR

CENTER ELECTRONIC ACCESS DOOR (NOT ON 747-SP)

FWD

HANDLE

PENETRATIONPOINTS(4 PLACES)

FWD ELECTRONICS ACCESS DOOR

8” 8”

7”

7”

747. 747T.O

. 00-105E-9

6 AIRCRAFT PENETRATION POINTS-ContinuedFOR RB211-524 B2/C2/D4 ENGINES

PENTRATION POINT

REF DWG65B89690165B89690265B896903

INBOARD NACELLE AND PYLON

OUTBOARD NACELLE AND PYLON

RIGHT HAND VIEW

ROLLS ROYCE RB 211-524 ENGINES

INBOARD NACELLE AND PYLON

LEFT HAND VIEW

747. 747T.O

. 00-105E-9

7 AIRCRAFT PENETRATION POINTS-ContinuedFOR CF6-50, E2 ENGINES

PENETRATION POINTSREF DWG65B9400165B9400265B9400365B94050

OUTBOARD NACELLE AND PYLON LEFT HAND VIEW INBOARD NACELLE AND PYLON

RIGHT HAND VIEW

OUTBOARD NACELLE AND PYLON RIGHT HAND VIEW

INBOARD NACELLE AND PYLON LEFT HAND VIEW

NACELLES AND PYLONS STATION DIAGRAM - GE CFC ENGINES

747. 747T.O

. 00-105E-9

8 AIRCRAFT PENETRATION POINTS-ContinuedFOR JT9D -3, -7, -7Q, AND -7R4G2 ENGINES

PENETRATION POINTS

OUTBOARD NACELLE AND PYLON LEFT HAND VIEW

INBOARD NACELLE AND PYLON LEFT HAND VIEW

INBOARD NACELLE AND PYLON RIGHT HAND VIEW

OUTBOARD NACELLE AND PYLON RIGHT HAND VIEW

747. 747T.O

. 00-105E-9

9

SPECIAL TOOLS/EQUIPMENTPower Rescue Saw35 Foot LadderFire Drill IIAIRCRAFT ENTRY-100 & 200/-100 & 200 COMBI

NOTE: Refer to the E-4 for more extensive information. Both airframes are identical except for military capabilities.

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

NOTE: All ten entry doors open outward.

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

NOTE:· Opening a door from the outside disengages the emergency evacuation system and the escape chute will not deploy.

· All emergency escape chutes are deployed from inside the aircraft only.

2. CUT-INa. Cut areas along window lines as last resort.

NOTE: Fuel capacity varies from model to model.

SURGE TANKOPTIONAL FUEL TANK788 GALS 2983 LITERS

HYD ACCUMULATORS (RT WHEEL WELL AREA)

PORTABLE OXYGENBOTTLES (8 PLACES,UNDER 1ST OUTBDSEAT FWD OFDOOR)

FUEL VENT ANDOVERFLOW (LOCATEDBENEATH WING)

534 GALS 2021 LITERS

12,546 GALS47,492 LITERS

4482 GALS16,966 LITERS


12,546 GALS47,492 LITERS 788 GALS

2983 LITERS

534 GALS2021 LITERS

FUEL VENT ANDOVERFLOW(LOCATEDBENEATH WING)

SURGETANK

SIDE CARGO DOOR (COMBI)

PORTABLE OXYGEN BOTTLES (2PLACES UNDER FLT ATTENDANTSEAT AFT OF DOOR

APU FUEL LINE

APU APU BATTERY

ENGINE OIL TANK -FWD RT SIDE OR AFTLT SIDE OF EACH ENGINE

-10013,200 GALS49,967 LITERS-20017,164 GALS64,973 LITERS

PASSENGEROXYGEN SYSBOTTLES ONFWD CARGOCOMPARTMENTCEILING

CREW OXYGEN SYSBOTTLE IN FWD CARGOCOMPARTMENT

MAIN BATTERY

HYDRAULIC RESERVOIR(4 PLACES ON ENGINE STRUTS)

ENTRY DOORSCREW DOOR (RT SIDE ONLY) ENTRY DOORS

1aENTRY DOOR EXTERNALHANDLE (FIVE LT SIDE)

1a, 1cENTRY AND CREWDOOR EXTERNALHANDLE

1bRELEASEBUTTON

1bESCAPEHATCH HANDLE

747. 747T.O

. 00-105E-9

10

ENGINE SHUTDOWN ANDAIRCREW EXTRACTION-100,-200/ -100/-200 COMBI-200 SPECIAL FREIGHTERSPECIAL PURPOSE AND FREIGHTER

1. ENGINE SHUTDOWNa. Retard throttles, located on pilot’s center console, to IDLE CUTOFF position.

b. Place engine start levers, located on pilot’s center console, to CUTOFF position.

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

c. Place battery switch, located on flight engineer’s center panel, to OFF position.

d. Place APU switch, located on flight engineer’s upper left panel, to STOP position.

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

2. AIRCREW EXTRACTIONa. 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 control to retract seats to aft position.

1aTHROTTLES

1bENGINE START LEVERS

1bBATTERY SWITCH

1dAPU SWITCH

APU FIRE T-HANDLEENGINE FIRE T-HANDLES

747. 747T.O

. 00-105E-9

11 EMERGENCY RESCUE ACCESS-100/-200 AND -100/-200 COMBI

A - Control cabin/lounge floor level to ground Wheels retracted: 18 FT 4 IN. Wheels extended: 24 FT 6 IN.

B - Crew door handle Wheels retracted: 20 FT 4 IN. Wheels extended: 27 FT

C - Passenger cabin floor level to ground Wheels retracted: 9 FT 10 IN. Wheels extended: 16 FT

D - Entry door handle Wheels retracted: 13 FT Wheels extended: 19 FT 2 IN.

E - Escape hatch Wheels retracted: 25 FT 10 IN. Wheels extended: 32 FT

APU ACCESS HATCH


“CHOP OUT” AREA (PASSENGER)

APU EMERGENCY CONTROL PANEL (LOCATEDRT INBOARD MAIN LANDING GEAR BULKHEAD)

“CHOP OUT” AREASENTRYDOOR

ENTRY DOORS

ENTRY DOORSPIRALSTAIRCASE

CABINENTRYDOOR

ENTRYDOOR

FLIGHTDECKOVERHEADESCAPEHATCH

“CHOP OUT”AREAS

ENTRYDOOR

ENTRYDOOR

ENTRYDOOR

ENTRYDOORS

“CHOP OUT”AREA

“CHOP OUT”AREAS

AC

DB

E

NOTE: Not all “chop out” areas are marked.

747. 747T.O

. 00-105E-9

12

SPECIAL TOOLS/EQUIPMENTPower Rescue Saw35 Foot LadderFire Drill II

AIRCRAFT ENTRY - 200 SPECIAL FREIGHTER

1. NORMAL/EMERGENCY ENTRY

a. Pull entry door handles from recess position and rotate 180 degrees clockwise for entry doors located on left side and counterclockwise for entry doors on right side.

NOTE: All entry doors open outward.





2. CUT-IN

a. Cut areas along window lines as last resort.

ENTRY DOORS CREW DOOR(RT SIDE ONLY)



1bRELEASEBUTTON


SURGE TANKOPTIONAL FUEL TANK788 GALS2983 LITERS

HYD ACCUMULATORS(RT WHEEL WELL AREA)


534 GALS2021 LITERS



4550 GALS17,224 LITERS12,647 GALS

47,874 LITERS

FUEL VENTAND OVER-FLOW(LOCATEDBENEATHWING)

APU FUEL LINE

APU BATTERY



UPPER DECKOXYGEN SYSBOTTLES ONFWD SIDE OF480 WALL

MAINBATTERY

APU

SURGETANK

OPTIONAL FUEL TANK788 GALS 2983 LITERS

HYDRAULICRESERVOIR(4 PLACES ONENGINE STRUTS)


OPTIONAL SIDE CARGO DOOR

534 GALS2021 LITERS

NOSECARGODOOR

747. 747T.O

. 00-105E-9

EMERGENCY RESCUE ACCESS13

APU ACCESS HATCH

SIDE CARGO DOOR

APU EMERGENCY CONTROL PANEL(LOCATED RT INBOARD MAIN LANDINGGEAR BULKHEAD)

ENTRY DOOR (10)

FLIGHTDECKDOOR

FLIGHT DECK OVERHEADESCAPE HATCH

“CHOP OUT” AREAS(4 ON EACH SIDE)

AC

DB

E

-200 SPECIAL FREIGHTER






747. 747T.O

. 00-105E-9

14


AIRCRAFT ENTRY - SPECIAL PURPOSE (SP)






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




1bRELEASEBUTTON


1aENTRY DOOREXTERNALHANDLE(FIVE LT SIDE)

SURGE TANKOPTIONAL FUEL TANK788 GALS2983 LITERS


PORTABLE OXYGEN BOTTLES(8 PLACES, UNDER 1ST OUTBDSEAT FWD OFDOOR)

FUEL VENT ANDOVERFLOW (LOCATEDBENEATH WING) 534 GALS

2021 LITERS





FUEL VENTANDOVERFLOW(LOCATEDBENEATHWING)

PORTABLE OXYGEN BOTTLES(2 PLACES ON WALL)

APU FUEL LINE

APU BATTERY


-10013,200 GALS49,967 LITERSPORTABLE

OXYGEN SYSBOTTLES ONFWD CARGOCOMPARTMENTCEILING 3 TO 9BOTTLES

PORTABLE OXYGENBOTTLE (UPPER DECKIN LH WALL AT TOP OFSTAIRS)

MAINBATTERY

APU

SURGE TANK




747. 747T.O

. 00-105E-9

15

EMERGENCY RESCUE ACCESS-SPECIAL PURPOSE (SP)






APU ACCESS HATCH


ENTRYDOOR

ENTRYDOORS

CABINENTRYDOORS

FLIGHTDECKOVERHEADESCAPE HATCH

“CHOP OUT”AREAS

ENTRY DOOR

ENTRYDOORS“CHOP

OUT”AREAS

“CHOPOUT”AREAS

ACD

BE


ENTRY DOOR

747. 747T.O

. 00-105E-9

16


AIRCRAFT ENTRY - FREIGHTER








2. CUT-IN





1bRELEASEBUTTON


SURGE TANK OPTIONAL FUEL TANK788 GALS2983 LITERS



534 GALS2021 LITERS



4550 GALS17,224 LITERS12,647 GALS

47,874 LITERS

FUEL VENTAND OVER-FLOW(LOCATEDBENEATHWING)

APU FUEL LINE

APU BATTERY



UPPER DECKOXYGEN SYSBOTTLES ONFWD SIDE OF480 WALL

MAINBATTERY

APU

SURGETANK




OPTIONAL SIDE CARGO DOOR

534 GALS2021 LITERS

NOSECARGODOOR

747. 747T.O

. 00-105E-9

17

EMERGENCY RESCUE ACCESS-FREIGHTER






APU ACCESS HATCH


ENTRYDOOR

ENTRY DOOR

CABINENTRYDOOR


“CHOP OUT”AREAS

NOSE CARGODOOR

“CHOPOUT”AREAS

ACD

BE


SIDE CARGO DOOR (OPTIONAL)

747. 747T.O

. 00-105E-9

18


AIRCRAFT ENTRY -300/-300 COMBI

NOTE: Refer to the E-4 for more extensive information. Both airframes are identical except for military capabilities.

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


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


NOTE:· Opening a door from the outside disengages the emer-

gency evacuation system and the escape chute will not deploy.

· All emergency escape chutes are deployed from insidethe aircraft only.

2. UPPER DECK EMERGENCY DOORSa. Push access panel and lift door handle.

NOTE: Lifting external handle disarms slide and disengages door interlock. Control access cover aft of door.

b. Open cover and move guarded emergency door switch to open.


SURGE TANKOPTIONAL FUEL TANK788 GALS 2983 LITERS


PORTABLE OXYGENBOTTLES (8 PLACES,UNDER 1ST OUTBDSEAT FWD OFDOOR)






12,546 GALS47,492 LITERS 788 GALS

2983 LITERS

534 GALS2021 LITERS


SURGETANK



APU FUELLINE

APU

APU BATTERY



PASSENGEROXYGEN SYSBOTTLES ONFWD CARGOCOMPARTMENTCEILING

UPPER DECK OXYGENSYS BOTTLE IN FWDCARGO COMPARTMENT

MAINBATTERY



ENTRY DOORS



1bRELEASEBUTTON


STAIR TOUPPER DECK

2aDOORHANDLE

2bEMERGENCYDOOR SWITCH

747. 747T.O

. 00-105E-9

19

ENGINE SHUTDOWN ANDAIRCREW EXTRACTION-300/-300COMBI AND SPECIAL FREIGHTER

1. ENGINE SHUTDOWNa. Retard throttles, located on pilot’s center console, to IDLE CUTOFF position.

b. Place engine start levers, located on pilot’s center console, to CUTOFF position.

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

c. Place battery switch, located on flight engineer’s center panel, to OFF position.

d. Place APU switch, located on flight engineer’s upper left panel, to STOP position.

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




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

1aTHROTTLES

1bENGINE START LEVERS

1bBATTERY SWITCH

1dAPU SWITCH

APU FIRE T-HANDLEENGINE FIRE T-HANDLES

747. 747T.O

. 00-105E-9

20

EMERGENCY RESCUE ACCESS-300/-300 COMBI






APU ACCESS



ENTRYDOORS

ENTRY DOOR

CABINENTRYDOORS

FLIGHTDECK OVERHEADESCAPE HATCH

“CHOP OUT” AREAS

ENTRY DOORS

ENTRYDOOR

ENTRYDOORS

“CHOP OUT”AREAS

“CHOPOUT”AREA

A

CD B

E


ENTRY DOORS

“CHOP OUT” AREA

“CHOPOUT”AREA

“CHOP OUT” AREA (PASSENGER)STAIR TO UPPER DECK

747. 747T.O

. 00-105E-9

21


AIRCRAFT ENTRY -300 SPECIAL FREIGHTER

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


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


NOTE:· Opening a door from the outside disengages the emer-

gency evacuation system and the escape chute will not deploy.

· All emergency escape chutes are deployed from insidethe aircraft only.

2. UPPER DECK EMERGENCY DOORSa. Push access panel and lift door handle.

NOTE: Lifting external handle disarms slide and disengages door interlock. Control access cover aft of door.

b. Open cover and move guarded emergency door switch to open.


SURGE TANK









788 GALS2983 LITERS



SURGE TANK


APU FUEL LINE

APU

APU BATTERY



PORTABLE OXYGEN BOTTLESON FWD CARGO COMPARTMENTCEILING

CREW OXYGEN SYSBOTTLE IN FWDCARGO COMPARTMENT

MAINBATTERY





1bRELEASEBUTTON


2aDOORHANDLE

2bEMERGENCYDOOR SWITCH

747. 747T.O

. 00-105E-9


APU ACCESS HATCH

SIDE CARGO DOOR


FLIGHTDECKDOOR

FLIGHT DECK OVERHEADESCAPE HATCH

“CHOP OUT” AREAS(4 ON EACH SIDE)

AC

DB

E

-300 SPECIAL FREIGHTER






747. 747T.O

. 00-105E-9

23


AIRCRAFT ENTRY -400 & 400 COMBI








2. CUT-IN


SURGE TANKOPTIONALFUEL TANK2,644 GALS10,009 LITERS

HYDRAULICACCUMULATORS (RT WHEEL WELL AREA)

PORTABLE OXYGENBOTTLES (8 PLACES,UNDER 1ST OUTBDSEAT FWD OF DOORIF PASSENGER AREAOTHERWISE6 PLACES










APU FUEL LINE

APU

APU BATTERY



PASSENGEROXYGEN SYSBOTTLES ONFWD CARGOCOMPARTMENTWALL IMMEDIATELYAFT OF DOOR

UPPER DECK OXYGENPORTABLE SYSTEMBOTTLE AT OUTBDLT AND RT ATTENDANTSTATION

MAINBATTERY

HYDRAULIC RESERVOIR(4 PLACES ON ENGINESTRUTS)


ENTRY DOORS



1bRELEASEBUTTON


STAIR TOUPPER DECK

SURGE TANK

SURGE TANKHORIZONTALSTABILIZERFUEL TANK3300 GALS12,492 LITERS

CREW OXYGENSYSTEM BOTTLEIN FWD CARGOCOMPARTMENT

747. 747T.O

. 00-105E-9

24

ENGINE SHUTDOWN ANDAIRCREW EXTRACTION1. ENGINE SHUTDOWN -400/-400 COMBI AND -400 FREIGHTER

a. Retard thrust levers, located on pilot’s center console, to RETARD position.

b. Place fuel control switches, located on pilot’s center console under thrust levers, to CUT OFF position.

c. In case of engine fire, pull engine fire switches, located on pilot’s overhead center panel. If not illuminated, may require pushing and holding the button under the switch to release.

d. In case of APU fire, pull APU fire switch, located on pilot’s overhead center panel under engine fire switches. If not illuminated, may require pushing and holding the button under the switch to release. Rotate APU selector to OFF.

e. Press battery switch, located on pilot’s overhead center panel left side, to OFF.

2. AIRCREW EXTRACTION

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



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

1cENGINE FIRE SWITCHES

1dAPU FIRESWITCH

1dAPUSELECTOR

1eBATTERYSWITCHNOTE:On symbolis removed.

1aTHRUST LEVERS

1bFUEL CONTROL SWITCHES

747. 747T.O

. 00-105E-9

25

EMERGENCY RESCUE ACCESS-400 AND 400 COMBI






APU ACCESSHATCH


ENTRYDOORS

ENTRY DOORS

CABINENTRYDOORS


“CHOP OUT”AREAS

“CHOPOUT”AREAS

A

CD B

E


SIDE CARGO DOOR ON COMBI

“CHOPOUT”AREA

“CHOPOUT”AREA

ENTRYDOOR

ENTRYDOOR

CREW REST AREA (8 bunks, 2 seats)

ENTRY DOOR

“CHOP OUT” AREA

“CHOP OUT” AREA

ENTRYDOORS

747. 747T.O

. 00-105E-9

26

SPECIAL TOOLS/EQUIPMENTPower Rescue Saw35 Foot LadderFire Drill IIAIRCRAFT ENTRY -400 FREIGHTER








2. UPPER DECK CREW SERVICE DOOR

a. To unlock door, push access panel.

b. Lift door handle.

3. CUT-IN


SURGE TANKOPTIONALFUEL TANK1,322 GALS5,004 LITERS

HYDRAULICACCUMULATORS(RT WHEEL WELLAREA)








SIDE CARGO DOOR

APU FUEL LINE

APU

APU BATTERY



FLIGHTDECK PORTABLEOXYGEN BOTTLE

MAINBATTERY

HYDRAULIC RESERVOIR(4 PLACES ON ENGINESTRUTS)

STAIR TOUPPER DECK

SURGE TANK

SURGE TANK

HORIZONTALSTABILIZERFUEL TANK3300 GALS12,492 LITERS

CREW OXYGENSYSTEM BOTTLEIN FWD CARGOCOMPARTMENT




1bRELEASEBUTTON


2bDOORHANDLE

747. 747T.O

. 00-105E-9

27

EMERGENCY RESCUE ACCESS- 400 FREIGHTER






APU ACCESS HATCH


ENTRYDOOR

ENTRY DOOR


“CHOPOUT”AREAS

A

CD

BE


SIDE CARGO DOOR ON COMBI

747. 747T.O

. 00-105E-9

AIRFRAME COMPOSITE MATERIALS- 400 FREIGHTER

28

RUDDER

VERTICAL STABILIZERTRAILING EDGE PANELS

ELEVATORS

STABILIZER TIP

UPPER WINGTRAILING EDGE

WINGLETS (ONLY - 400)

LOWER WINGTRAILING EDGE

RADOME

WING TO BODY FAIRING

AILERONS

FLAP TRACKFAIRINGS

LOWER WINGTRAILING EDGE

SPOILERSENGINE PYLONS

INLET, FAN ANDREVERSER COWLS

UPPER WINGTRAILING EDGE

TIP FAIRING

VERTICAL STABILIZERFORWARD TORQUE BOX

747. 747T.O

. 00-105E-9

CABIN CONFIGURATION29

A ATTENDANT

T TOILET

C CLOSET

S STOWAGE

R CREW REST

G GALLEY

C/L CART LIFT

EFFECTIVITY: 747-400 (TRI-CLASS)

A

A

RC

C

C L

G

GGG

T T

C S G

T

TAA

AA

AA

AA

G

C/LG

G

GS

T T

T

T

AA

AA

AA

AA

G

G G

A

A

TT T

T T T

SS

S

S

A

A

TTT

T T T

SS

S

CT

AA

AA

GG

A

AA

T

T

CG

G

S

C C/L

AA

AA

A

A

T

T

T

T

C

UPPER DECK*42 BUSINESS RATE SEATS AT 38” (.96 M) PITCH

MAIN DECK*32 FIRST CLASS SEATS AT 61” (1.55 M) PITCH*34 BUSINESS RATE SEATS AT 39” (1.00 M) PITCH*322 ECONOMY SEATS AT 32” (.81 M) PITCH

MAIN DECK*32 FIRST CLASS SEATS AT 61” (1.55 M) PITCH*34 BUSINESS RATE SEATS AT 39” (1.00 M) PITCH*309 ECONOMY SEATS AT 32” (.81 M) PITCH

OPTIONAL IN=FLIGHTOVERHEAD CREW REST8 BUNKS AND 2 SEATS

747. 747T.O

. 00-105E-9

CABIN CONFIGURATION-Continued30

A ATTENDANT

T TOILET

C CLOSET

S STOWAGE

R CREW REST

G GALLEY

C/L CART LIFT

EFFECTIVITY: 747-400ER (TRI-CLASS)

416 PASSENGERS

MAIN DECK*23 FIRST CLASS SEATS AT 61” (1.55 M) PITCH*38 BUSINESS RATE SEATS AT 39” (1.00 M) PITCH*269 ECONOMY SEATS AT 32” (.81 M) PITCH*46 ECONOMY SEATS AT 31” (.79 M) PITCH

UPPER DECK*40 BUSINESS CLASS SEATS AT 39” (1.00 M) PTICH

UPPER DECKOVERHEAD CREW REST8 BUNKS AND 2 SEATS

MAIN DECK

AAR

C

CC/L

S

GGG

G

T T

A

A

S

C/L

TT

S

G GGG

TT

AA

AA

AAA

A

AA A

AAA

AA

SG

GS

S

S

747. 747T.O

. 00-105E-9


A ATTENDANT

T TOILET

C CLOSET

S STOWAGE

R CREW REST

G GALLEY

C/L CART LIFT

EFFECTIVITY: 747-400ER (DUAL CLASS)

UPPER DECKOVERHEAD CREW REST8 BUNKS AND 2 SEATS

MAIN DECK

500 PASSENGERS

MAIN DECK*42 FIRST CLASS SEATS AT 39” (1.00 M) PITCH*333 ECONOMY SEATS AT 32” (.81 M) PITCH*53 ECONOMY SEATS AT 31” (.79 M) PITCH

UPPER DECK*33 ECONOMY SEATS AT 32” (.81 M) PITCH*39 ECONOMY CLASS SEATS AT 31” (.79 M) PTICH

A

ARC

CC/L

G

G GG

T T

S

A

A

S

C/L

TT

S

G GG

TT

AA

AA

AAA

A

AA A

AAA

AA

SG

GS

S

S

T

T

T

T

T

T

747. 747T.O

. 00-105E-9


T TOILET

S STOWAGE

R CREW REST

G GALLEY

C/L CART LIFT

EFFECTIVITY: 747-400 COMBI

UPPER DECK*42 BUSINESS CLASS SEATS AT 38” (.96 M) PITCH

MAIN DECK - COMBI LOAD*21 FIRST CLASS SEATS AT 61” (1.55 M) PITCH*35 BUSINESS CLASS SEATS AT 38” (.96 M) PITCH*168 ECONOMY SEATS AT 32” (.81 M) PITCH*7 PALLETS

A

R

C

C/L

A

GG

GT T

S S

C/L

G GR

TAAA

AAA

AA A

A AA AT

S

G

G

C

T

T

T

T

747. 747T.O

. 00-105E-9


CABIN CONFIGURATION-ContinuedEFFECTIVITY: 747-400ER FREIGHTER

*29 10’ (3 M) CONTAINERS

*13 20’ (6 M) CONTAINERS* 5 10’ (3 M) CONTAINERS

*RANDOM MIX OF CARGO PALLETSAND CONTAINERS UP TO 40’ (12 M)

747. 747T.O

. 00-105E-9


A ATTENDANT

T TOILET

S STOWAGE

G GALLEY

EFFECTIVITY: 747-400 DOMESTIC

UPPER DECK

MAIN DECK*539 ECONOMY CLASS SEATS AT 31” (.79 M) OR 32” (.81 M) PITCH

UPPER DECK*85 ECONOMY SEATS AT 31” (.79 M) OR 32” (.81 M) PITCH

A

AT

S

G

T T

C

A

AC/L

TT

S

G

TT

AAA

AA

A

S

AAA A

S

GG

S

T

T

T

T

T

T

T

T

T

747. 747T.O

. 00-105E-9

CROSS CABIN CONFIGURATION

BUSINESS CLASS UPPER DECK - 4 ABREAST MAIN DECK FIRST CLASS - 6 ABREAST

-400

15’ 10” (4.83 M) AT 18’ (5.49 M)AFT OF NOSE LOOKING AFT FORWARD CABIN

21’ 4” (6.50 M)(CONSTANT CABIN CROSS SECTION)

14’ 6” (4.42 M)(TRIM-TO-TRIM) 7’ 11”

(2.41 M)

FIRST CLASSSEATS (TYPICAL)

35

7’ 11”(2.41 M)

7’ 11”(2.41 M)

1’ 10”(0.56 M)

4’ 9” (1.45 M) TYPICAL

4’ 9” (1.45 M) TYPICAL

2’ 10” (0.86 M) TYPICAL

1’ 8” (0.51 M)

DOUBLE SEAT

4’ 1” (1.24 M) TYPICAL

9’ 0”(2.73 M)

2” (5 CM) 1’ 9” (0.53 M) TYPICAL

UPPER DECK - 4 ABREAST MAIN DECK - 8 ABREAST

MAIN DECK - 7 ABREAST

4’ 6” (1.37 M) TYPICAL 6’ 10” (2.08 M)

21’ 4” (6.50 M)(CONSTANT AFT CABIN SECTION)

2’ 1” (0.63 M) TYPICAL

BUSINESS CLASSFIRST CLASS

747. 747T.O

. 00-105E-9

36

CROSS CABIN CONFIGURATION-Continued

UPPER DECK - 6 ABREAST MAIN DECK - 10 ABREAST

MAIN DECK - 9 ABREAST

-400ECONOMY CLASS GALLEY AND STAIRS

9’ 0”(2.73 M)

7’ 11”(2.41 M)

1’ 5”(0.43 M)

3’ 4.5” (1.03 M) (TYPICAL)

1’ 7.5” (0.50 M) (TYPICAL)

.5” (1.3 CM)

4’ 11.5” (1.51 M) (TYPICAL)

5’ 1.5” (1.59 M)7’ 0” (2.13 M) 3’ 7”

(1.09 M)

2’ 9” (0.53 M) (TYPICAL)



SECTION THROUGH STAIRS(VIEW LOOKING FORWARD)

GALLEYFOUR CARTGALLEY MODULE

STORAGE

STORAGESTAIRS(FORWARD OFSTORAGE CABINET) 1’ 8.75” (0.53 M)

(TYPICAL)

4’ 11.5” (1.51 M)

TYPICAL TRIPLE SEAT

STORAGE

1’ 8.75” (0.53 M)

2’ 6.75” (0.78 M)

747. 747T.O

. 00-105E-9

37

CARGO CONFIGURATIONS-400, 400 COMBI, -400 DOMESTIC, -400ER,-400 FREIGHTER, -400ER FREIGHTER

NOTE:Container weight and data are typical. Consult using airline forspecific data. Options are offered for carriage of certain standardmilitary and commercial pallets in container compartments.

31.5”(0.80 M)

31.5”(0.80 M)

60.4”(1.53 M)

60.4”(1.53 M)

61.5”(1.93 M)

64”(1.63 M)

92”(2.33 M)

186”(4.72 M)

64”(1.63 M)

125”(3.18 M)

HALF-WIDTH CONTAINER LD1

FULL-WIDTH CONTAINER LD2

CONTAINER CARGODOORS (RH SIDE ONLY)

BULK CARGO DOOR(RH SIDE ONLY)


BULK CARGO DOOR (RH SIDE ONLY)

BULK CARGO DOOR (RH SIDE ONLY)


FORWARD COMPARMENT(8 FULL-WIDTH OR 16HALF-WIDTH CONTAINERS)

AFT COMPARMENT(8 FULL-WIDTH OR16 HALF-WIDTH CONTAINERS)

BULK CARGO COMPARMENT835 CU FT (23.6 CU M)-400, -400 DOMESTIC710 CU FT (20.1 CU M)-400 COMBI)

-400 FREIGHTER-400ER FREIGHTER

-400ER

-400, -400 COMBI, -400 DOMESTIC

BULK CARGO DOOR789 CU FT (22.3 CU M)

AFT COMPARMENT (8 FULL-WIDTH OR16 HALF-WIDTH CONTAINERS)

AUXILIARY FUEL TANK OPTIONAL SECONDAUXILIARY FUEL TANK

FORWARD COMPARMENT(5 FULL-WIDTH OR 10 HALF-WIDTHCONTAINERS)

FORWARD COMPARMENT(8 FULL-WIDTH OR16 HALF-WIDTH CONTAINERS) (5 96X125” PALLETS)

AFT COMPARMENT (8 FULL-WIDTHOR 16 HALF-WIDTH CONTAINERS) (5 96X125” PALLETS

BULK CARGO COMPARTMENT520 CU FT (14.7 CU M)

757. 757T.O

. 00-105E-9


757. 757T.O

. 00-105E-9

AIRCRAFT DIMENSIONS2

757-200/-200PF 757-300

(PW) 54’ 6” (16.61 M)(RR) 55’ 3” (16.84 M)

(3.76 M)

21’ 3”(6.48 M)

12’ 4”

155’ 3” (47.32 M)

44’ 3”(13.49 M)

19’ 4”(5.89 M)

60’ 0”(18.29 M)

13’ 2” (4.01 M)

154’ 1” (46.97 M)124’ 10”(38.05 M)

49’ 11”(15.21 M)

24’ 0”(7.32 M)

(PW) 8’ 10” (2.69 M)(RR) 8’ 1” (2.46 M)

FEET

METERS

SCALE 1” = 40’

0 10 20 30 40 50

0 5 10 15

(PW) 67’ 10” (20.68 M)(RR) 68’ 7” (20.90 M)

(3.76 M) 21’ 3”(6.50 M)

12’ 4”

177’ 5” (54.08 M)

44’ 6”(13.56 M)

19’ 4”(5.89 M) 73’ 4”(22.35 M)

124’ 10”(38.05 M) 49’ 11”(15.21 M)

24’ 0”(7.32 M)

(PW) 8’ 10” (2.70 M)(RR) 8’ 1” (2.46 M)

FEET

METERS

SCALE 1” = 40’

0 10 20 30 40 50

0 5 10 15

178’ 7” (54.43 M)

757. 757T.O

. 00-105E-9

3 AIRCRAFT SKIN PENETRATION POINTS

#3 CARGO DOOR

CARGO DOOR

#1#2

18”

PENETRATIONPOINT

FWD

HANDLE

CL

8” 8”20”PENETRATION

POINTS

HANDLE

FWD

757. 757T.O

. 00-105E-9

4 AIRCRAFT SKIN PENETRATION POINTS-Continued

ENGINE NACELLE LEFT SIDE VIEW

ENGINE NACELLERIGHT SIDE VIEW

PENETRATION POINTSPENETRATION POINTSWINGWING 8”

18”18”

8”

30”30”

REARMOUNT

REARMOUNT

PRESSURE RELIEF DOORPRESSURE RELIEF DOOR

CORE COWLCORE COWL

FAN COWL

FAN COWL

THRUST REVERSER COWLTHRUST REVERSER COWL

OIL TANK FILLER DOOR

1.5” X 8” COWL VENT AT BL 0USE FOR FIRE EXTINGUISHERACCESS TO FAN COMPARTMENT.

1.5” X 8” COWL VENT AT BL 0USE FOR FIRE EXTINGUISHERACCESS TO FAN COMPARTMENT.

C NACELLE

INLET

FRONTMOUNT

FRONTMOUNT

CL

CL

CL

CL

L

CL

CL

-200/ -300

NOTE: The 757-200 and -300 uses two Pratt & Whitney or Rolls-Royce turbofans with varying thrust mounted in underwing pods.

757. 757T.O

. 00-105E-9

5


AIRCRAFT ENTRY -200 & 200 COMBI

1. NORMAL/EMERGENCY

a. To open entry and service doors: push handle release latch.b. Pull butterfly handle from recess and rotate 180 degrees in direction of “open” arrow.c. Pull door outward.d. To open overwing escape hatches (if installed): lift lower portion of handle away from the side of the aircraft.e. Continue to raise handle to the pull up position.f. Push hatch inward and upward.g. To open number 3 emergency exit (if installed): push on “push” panel to gain access to handle.h. Pull handle forward and outward.

NOTE:• Escape slide disarms automatically when door or hatch is opened from the outside, except No. 3 emergency exit.

• Cockpit windows cannot be opened from the outside.

2. CUT-IN

a. Cut along window lines as last resort.

SURGETANKS

APU2,170 GALS8,214 LITERS

2,170 GALS 8,214 LITERS

HYD RESERVOIR ANDACCUMULATOR IN RTWHEEL WELL

APU FUEL LINE

HYD RESERVOIR IN LT WING FILLET

ENGINE OIL TANK LT OR RTSIDE OF EACH ENGINE

HYD RESERVOIR IN LT WHEEL WELL6,900 GALS26,119 LITERS

CREW OXYGEN BOTTLEIN RT SIDE, FWD CARGOCOMPARTMENT AFT OFDOOR

APU EMERGENCYCONTROL PANELLOCATED ONTHE NOSEGEAR

FLT DECK PORTABLEOXYGEN BOTTLE ONBLKHD BEHIND PILOT

PORTABLE OXYGENBOTTLES IN FWDPASSENGER CABIN

1aHANDLERELEASELATCH

1bHANDLE

1dOVERWINGESCAPEHATCHHANDLE

1g, 1hEMERGENCYEXIT HANDLE

APUBATTERYAFT

CARGODOOR

NOSE GEAR COMPARTMENT

ACCESS DOOR

MAIN BATTERY

SURGE TANKS

757. 757T.O

. 00-105E-9

6

ENGINE AND APU SHUTDOWNAND AIRCREW EXTRACTION-200/-200 COMBI & -200 PACKAGE FREIGHTER

1. ENGINE AND APU SHUTDOWN

a. Retard thrust levers, located on pilot’s center console, to RETARD position.b. Place fuel control switches, located on pilot’s center console under thrust levers, to CUT OFF position.c. In case of engine fire, pull engine fire switches, located on pilot’s center console. Turn left or right to release agent. If not illuminated, push and hold the button under the switch to release.d. In case of APU fire, pull APU fire switch, located on pilot’s center console to the right of the engine fire switches. Turn switch up or down to release agent. If not illuminated, push and hold the button under the switch to release.e. Rotate APU control switch, located on pilot’s overhead panel to OFF.f. Press battery switch, located on pilot’s overhead center panel left side, to OFF.g. There is a set of remote APU shutdown controls mounted on the forward landing gear. The APU ground control panel contains a fire warning light, a warning horn, a shutdown switch which shuts down the APU, arms a fire extinguisher, activates the horn and a bottle discharge switch which discharges agent into the APU compartment.


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.


1fBATTERYSWITCHNOTE:On symbol is removed.

1aTHRUST LEVERS


1cENGINE FIRESWITCHES

1dAPU FIRESWITCH

1eAPU CONTROLSWITCH

757. 757T.O

. 00-105E-9

7 EMERGENCY RESCUE ACCESS-200 & 200 COMBI

ENTRYDOORS

ENTRYDOORS

ENTRYDOORS“CHOP

OUT”AREAS

“CHOPOUT”AREAS

OVERWING ESCAPEHATCHES (IF INSTALLED)

APUACCESS

CARGO DOOR (RT SIDE)(OPTIONAL) OPERATINGINSTRUCTIONS ON DOOR

EMERGENCY EXITS(IF INSTALLED)

CARGO DOOR (RT SIDE)OPERATING INSTRUCTIONSON DOORCARGO

DOOR (COMBI)

CARGO DOOR (RT SIDE)OPERATING INSTRUCTIONSON DOOR

AVERAGE DISTANCE -FLOOR LEVEL TO GROUND:WHEEL RETRACTED : 6 FT 6 INWHEELS EXTENDED: 13 FT

757. 757T.O

. 00-105E-9

8


-200 PACKAGE FREIGHTER

AIRCRAFT ENTRY

1. NORMAL/EMERGENCY

a. To open window from outside: push in external door.

b. Pull external pull handle.

c. Unfold crank handle.

d. Rotate crank handle clockwise.

e. To open entry door: pull out aft end of handle.

f. Rotate handle counter clockwise.

g. Push door inward.

2. CUT-IN


MAINBATTERY


ACCESS DOOR

APUBATTERY

NOTE: APU battery compartment located forward of APU.

1e, 1gENTRYDOORHANDLE

1aEXTERNALCRANKHANDLE

APU

APU FUEL LINE

HYDRAULIC RESERVOIR (LT WING FILLET)

SURGETANK

HYDRAULIC RESERVOIR (LT WHEEL WELL)

HYDRAULIC RESERVOIR ANDACCUMULATOR (RIGHT WHEEL WELL)

SURGETANK

DRYBAY




ENGINE OIL TANK - LT OR RTSIDE OF EACH ENGINECREW OXYGEN

BOTTLE IN RT SIDE, FWDCARGO COMPARTMENTAFT OF DOOR

FLIGHT DECKPORTABLEOXYGENBOTTLE ONBULKHEADBEHIND PILOT

PORTABLEOXYGENBOTTLESINLAVATORY

APU EMERGENCYCONTROLPANEL ONNOSE GEAR

757. 757T.O

. 00-105E-9

9 EMERGENCY RESCUE ACCESS-200 PACKAGE FREIGHTER


ENTRYDOOR

CO-PILOT’SWINDOW(RT SIDE)

LOWER DECK CARGO DOOR(RT SIDE) OPERATINGINSTRUCTIONS ON DOOR

SIDE CARGODOOR

“CHOP OUT” AREAS(NOT MARKED ONALL AIRCRAFT)

APUACCESS

LOWER DECK CARGO DOOR(RT SIDE) OPERATINGINSTRUCTIONS ON DOOR

757. 757T.O

. 00-105E-9

10


AIRCRAFT ENTRY -300

1. NORMAL/EMERGENCY

a. To open entry and service doors: push handle release latch.b. Pull butterfly handle from recess and rotate 180 degrees in direction of “open” arrow.c. Pull door outward.d. To open overwing escape hatches (if installed): lift lower portion of handle away from the side of the aircraft.e. Continue to raise handle to the pull up position.f. Push hatch inward and upward.g. To open number 3 emergency exit (if installed): push on “push” panel to gain access to handle.h. Pull handle forward and outward.

NOTE:• Escape slide disarms automatically when door or hatch is opened from the outside, except No. 3 emergency exit.

• Cockpit windows cannot be opened from the outside.

2. CUT-IN


SURGETANKS

APU2,220 GALS8,404 LITERS


HYD RESERVOIR ANDACCUMULATOR IN RTWHEEL WELL

APU FUEL LINE

HYD RESERVOIR IN LT WING FILLET

ENGINE OIL TANK LT OR RTSIDE OF EACH ENGINE

HYD RESERVOIR IN LT WHEEL WELL7,050 GALS26,687 LITERS

CREW OXYGEN BOTTLEIN RT SIDE, FWD CARGOCOMPARTMENT AFT OFDOOR

APU EMERGENCYCONTROL PANELLOCATED ONTHE NOSEGEAR

FLT DECK PORTABLEOXYGEN BOTTLE ONBLKHD BEHIND PILOT

PORTABLE OXYGENBOTTLES IN FWDPASSENGER CABIN

1aHANDLERELEASELATCH

1bHANDLE

1dOVERWINGESCAPEHATCHHANDLE

1g, 1hEMERGENCYEXIT HANDLE

APUBATTERYAFT

CARGODOOR


ACCESS DOOR

MAIN BATTERY

SURGE TANKS

757. 757T.O

. 00-105E-9

11

ENGINE AND APU SHUTDOWNAND AIRCREW EXTRACTION-300

1. ENGINE AND APU SHUTDOWN

a. Retard thrust levers, located on pilot’s center console, to RETARD position.b. Place fuel control switches, located on pilot’s center console under thrust levers, to CUT OFF position.c. In case of engine fire, pull engine fire switches, located on pilot’s center console. Turn left or right to release agent. If not illuminated, push and hold the button under the switch to release.d. In case of APU fire, pull APU fire switch, located on pilot’s center console to the right of the engine fire switches. Turn switch up or down to release agent. If not illuminated, push and hold the button under the switch to release.e. Rotate APU control switch, located on pilot’s overhead panel to OFF.f. Press battery switch, located on pilot’s overhead center panel left side, to OFF.g. There is a set of remote APU shutdown controls mounted on the forward landing gear. The APU ground control panel contains a fire warning light, a warning horn, a shutdown switch which shuts down the APU, arms a fire extinguisher, activates the horn and a bottle discharge switch which discharges agent into the APU compartment.


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.



1aTHRUST LEVERS



1dAPU FIRESWITCH

1eAPU CONTROLSWITCH

757. 757T.O

. 00-105E-9


ENTRYDOORS

ENTRYDOORS

ENTRYDOORS

“CHOPOUT”AREAS

“CHOPOUT”AREAS

OVERWING ESCAPEHATCHES (IF INSTALLED)

APUACCESS


EMERGENCY EXITS(IF INSTALLED)

OPTIONAL CARGO DOOR (RT SIDE)OPERATING INSTRUCTIONSON DOOR

CARGODOOR(COMBI)CARGO DOOR (RT SIDE)

OPERATING INSTRUCTIONSON DOOR


-300

757. 757T.O

. 00-105E-9

AIRFRAME MATERIALS13

-300

COMPOSITES

FLAP TRACK FAIRINGS WING TO BODYFAIRING

NOSE LANDINGGEAR DOORS

HORIZONTAL STABILIZERUPPER/LOWER TRAILINGEDGE PANELS

AILERONS

INBOARD/OUTBOARDSPOILERS AND FLAPS

LEADING EDGE SLATAND FIXED PANELS

INLET/FAN THRUSTREVERSER COWL

RADOME

STRUTFAIRING

ELEVATORS AND TABS

RUDDER

PYLON FAIRING PANELS

HORIZONTAL STABILIZERUPPER/LOWER SKIN PANELS

MAIN LANDINGGEAR DOORS

757. 757T.O

. 00-105E-9

CABIN CONFIGURATION

A ATTENDANT

G GALLEY

L LAVATORY

C CLOSET

DUAL CLASS ARRANGEMENT - 186 SEATS16 FIRST CLASS SEATS 170 ECONOMY CLASS SEATS

SINGLE CLASS ARRANGEMENT 220 ECONOMY CLASS SEATS



OVERWING EXIT

FOURDOOR

-200

AAL

G G A

A

L

L LG

G

GL

L A

AAA

L

AAL

G G

AAL

GC C

AAL

L

L

G

AA

A

AG

AL

LL L

G

AA

14

757. 757T.O

. 00-105E-9

CABIN CONFIGURATION-Continued-200PF (MAIN DECK CARGO)

80.78”(2.05 M)

125”(3.17 M)

88”(2.23 M)

80.78”(2.05 M)

125”(3.17 M)

88”(2.23 M)

440 CU FT (12.47 CU M) CONTAINER

STRAPPED PALLET UP TO 440 CU FT (12.47 CU M)

LAVATORY

RIGID BARRIER

15 UNIT LOAD DEVICES

MAIN DECK CARGO DOOR (LH) 134X86” (3.40X18.0 M)

CREW ENTRY DOOR (LH) 22X48” (0.56X1.220 M)

15

757. 757T.O

. 00-105E-9

CABIN CONFIGURATION-Continued

A ATTENDANT

G GALLEY

L LAVATORY

-300



GG

L AAA

L

L

L

L

A

AAG

AAG

AA

AA

AL

L

L

LL

GG

A

16

T.O. 00-105E

-9

767

767. AIRCRAFT PAINT SCHEME1

T.O. 00-105E

-9

767

767. AIRCRAFT DIMENSIONS

-400ER

2

201’ 4” (61.4 M)

16’ 6”(5.03 M) 26’ 0”

(7.92 M)

67’ 1.4”(20.46 M)

GE: 71’ 10” (21.9 M)PW 72’ 5” (22.4 M)

85’ 10” (26.2 M)14’ 11” (9.6 M)

197’ 1.5” (60.1 M)

61’ 1” (18.6 M)170’ 4” (51.9 M)

APPROX 9’ 2”(2.79 M) 30’ 6”

(9.3 M)

0 10 20 30 40SCALE

0 2 4 6 8 10 12

FEETMETERS

54’ 9”(16.68 M)

T.O. 00-105E

-9

767

767.3 AIRCRAFT SKIN PENETRATION POINTS

8” 8”

8”

9”

6” 6”

8”

8” 9” 5”

5”

5”

FWD FWD

FWD

FWD

FWD

HANDLE

PENETRATIONPOINTS

PENETRATIONPOINTS

PENETRATIONPOINTS

4 EACH PENETRATION POINTSELECTRONICSACCESS DOOR

FWD ACCESS DOOR

VENT DOORS

ACCESS PANELS

AFT CARGO (RH) (EXCEPT LARGEFWD CARGO DOOR)

LARGE FWD CARGO DOOR (RH)

BULK CARGO (LH)

HANDLE

VENT DOORS

HANDLE

T.O. 00-105E

-9

767

767.4


AIRCRAFT ENTRY - ALL MODELS


a. To open entry/service door: push in lower part of handle.

b. Lift handle to unlock door.

c. Raise door upward.

d. To open overwing escape hatches: lift lower portion of handle away from the side of the aircraft.

e. Continue to raise handle to the full up position.

f. Push hatch inward and upward.

NOTES:

• Escape slide disarms automatically when door or hatch is opened from the outside.

• Flightdeck windows cannot be opened from the outside.

2. CUT-IN


MAINBATTERY

NOSE GEAR DOOR

EQUIPMENTACCESS DOOR

AFTCARGODOOR

APU BATTERY

1d -1fESCAPE HATCH HANDLE

1a -1cENTRY/SERVICEDOOR HANDLE

APU

APU FUEL LINE

PORTABLE OXYGEN BOTTLE(S)(THROUGOUT CABIN) (OPTIONAL)

SURGETANK

SURGE TANK

HYD ACCUMULATOR(RT WHEEL WELL)

HYD RESERVOIR (RT WHEEL WELL)



CENTER FUEL TANK CAPACITIESMODEL GALLONS LITERSSTANDARD 4,560 17,261 -200ER 8,310 31,457 -300ER 12,000 45,425 -400ER 12,000 45,425

1

1

DRY BAY

CREW OXYGEN BOTTLE(RT SIDE E&E COMPARTMENT

APU EMERGENCYCONTROL PANELON NOSE GEAR

PORTABLE OXYGENBOTTLES (FWD SIDE OFBULKHEAD) (OPTIONAL)

ENGINE OIL TANK (FWD RTOR AFT LT SIDE OF EACHENGINE)

T.O. 00-105E

-9

767

767.5 ENGINE SHUTDOWN ANDAIRCREW EXTRACTION1. ENGINE SHUTDOWNa. Retard thrust levers, located on pilot’s center console, to RETARD position.


c. In case of engine fire, pull engine fire switches, located on pilot’s center console. Turn left or right to release agent. If not illuminated, push and hold the button under the switch to release.

d. In case of APU fire, pull APU fire switch, located on pilot’s center console to the right of the engine fire switches. Turn switch up or down to release agent. If not illuminated, push and hold the button under the switch to release.

e. Rotate APU control switch, located on pilot’s over head panel to OFF.

f. Press battery switch, located on pilot’s overhead center panel left side, to OFF.






1aTHRUST LEVERS

1bFUEL CONTROLSWITCHES


1dAPU FIRESWITCH

1eAPU CONTROLSWITCH

T.O. 00-105E

-9

767

767.6 EMERGENCY RESCUE ACCESS

AVERAGE DISTANCE -FLOOR LEVEL TO GROUND:WHEEL RETRACTED : 7 FT 6 INWHEELS EXTENDED: 13 FT 6 IN

APUACCESS

ENTRY/SERVICE DOOR


ENTRY/SERVICEDOOR (OPTIONAL)

ENTRY/SERVICE DOOR

ENTRY/SERVICEDOOR

CARGO DOOR(RT SIDE)OPERATINGINSTRUCTIONSON DOOR

CARGO DOOR(RT SIDE)OPERATINGINSTRUCTIONSON DOOR



ENTRY/SERVICEDOOR (OPTIONAL)

OPTIONAL OVERWINGESCAPE HATCHESON -300, ON ALL -400

OPTIONAL OVERWING ESCAPE HATCHES

ENTRY/SERVICEDOOR

TYPE 1 EMERGENCY EXIT(OPTIONAL ON -300, ON ALL -400)

767-400 FREIGHTERS - RT SIDEFLIGHTDECK CAN BE OPENEDFROM THE OUTSIDE

T.O. 00-105E

-9

767

767. AIRFRAME MATERIALS7

COMPOSITES RUDDERVERTICAL STABILIZER TIP

ELEVATORS AND TABS

INBOARD/INBOARDSPOILERS AND FLAPS

PYLON FAIRING PANELS

RADOME

MAIN LANDING GEARDOORS HEAT SHIELDS

HORIZONTALSTABILIZER TIP

FLAP TRACKFAIRINGS

INLET/FAN/THRUSTREVERSER COWL

RIGID CARGO BARRIER(-300F/-400)

LEADING EDGE SLATAND FIXED PANELS

NACELLE STRUT FAIRING

RAKED TIP(-400 ONLY)

HORIZONTAL STABILIZERUPPER/LOWRE TRAILINGEDGE PANELSVERTICAL STABILIZER

FORWARD TORQUEBOX PANELS

HORIZONTAL STABILIZERUPPER/LOWER SKIN PANELS

INBOARD/INBOARDSPOILERS AND FLAPS

NOSE LANDINGGEAR DOORS

MAIN LANDINGGEAR DOORSAND VAPORBARRIER


TAIL SKID FAIRING

T.O. 00-105E

-9

767

767.8

CABIN CONFIGURATION-200 & -300

767-200

767-300

FWD

18 FIRST CLASS - 38 INCH PITCH 193 TOURIST - 34/33 INCH PITCH 211 PASSENGERS (24 SEATS - 33 INCH PITCH)

24 FIRST CLASS - 38 INCH PITCH 234 TOURIST - 34/33 INCH PITCH 258 PASSENGERS (33 SEATS - 33 INCH PITCH)

T.O. 00-105E

-9

767

767.9

CIVIL RESERVE AIR FLEET CABIN CONFIGURATION

LEGEND:= Power Distribution System

G = GalleyLAV = LavatoryNWS = Nurse’s Work StationO = Oxygen Management Panel

= Litter

= Emergency Exit

= Seats

2NOTE: Aircraft has capacity for 87 litters and 41 Ambulatory/Crew.

G

LAV

NWS 1

NWS 2

LAV LAV

LAV

GLAV

ICE

ICE

O2

FWDAFT

-200 SERIES AEROMEDICAL EVACUATION CONFIGURATION

T.O. 00-105E

-9

767

767.10

LEGEND:= Power Distribution System

G = GalleyLAV = LavatoryNWS = Nurse’s Work StationO = Oxygen Management Panel

= Litter

= Emergency Exit

= Seats

2NOTE: Aircraft has capacity for 111 litters and 30 Ambulatory/Crew.

CIVIL RESERVE AIR FLEET CABIN CONFIGURATION-300 SERIES AEROMEDICAL EVACUATION CONFIGURATION

G

GG

G

LAV

WINDOW EXITS

WINDOW EXITS

ICE

ICE

LAV LAV G GNWS 2

NWS 1

LAV

LAV02

FWD AFT

T.O. 00-105E

-9

767

767. CABIN CONFIGURATION-400ER

11

A ATTENDANT’S SEAT

C COAT CLOSET

L LAVATORY

W WARDROBE CLOSET

G GALLEY

VCC VIDEO CONTROL CENTER

A LL

AA

G

C G

GC

LC

A

A

CL

L

G G

A

A

A

A

L

L

LL

G G

G

G

W

W

A

AL

L

L

L

G

G

G

G

W

W

A

A

L

L

L

LG

G

G

G

W

W

AA

L

L

LL

G

CG

G

A

A

A

A

A

AA

A

VCC

A

AA

G

A

A L

G

A

A

THREE-CLASS CONFIGURATION - 243 PASSENGERS 16 FIRST CLASS 36 BUSINESS CLASS 189 ECONOMY CLASS

TWO-CLASS CONFIGURATION - 296 PASSENGERS 24 FIRST CLASS 272 ECONOMY CLASS

ONE-CLASS CONFIGURATION - 409 PASSENGERS ALL ECONOMY CLASS

777. 777T.O

. 00-105E-9


777. 777T.O

. 00-105E-9

AIRCRAFT DIMENSIONS2

777-200LR

209’ 1” (63.73 M)

67’ 0”(20.42 M)

70’ 9.5”(21.58 M)

20’ 4”(6.20 M)

31’ 6.5”(9.61 M)

141’ 7.4” (43.17 M)

84’ 11.1”(25.89 M)

141’ 7.4” (43.17 M)

20’ 4” (6.20 M)

19’ 4”(5.89 M)

206’ 6” (62.94 M)

212’ 7” (64.80 M) 70’ 7.5”(21.53 M)

13’ 0”(3.96 M)

36’ 0”(10.97 M)

SCALEMETERS

0 2 4 6 8 10 12 14

FEET0 10 20 30 40 50

60’ 10”(18.54 M)

777-300ER

242’ 4” (73.86 M)

84’ 6”(25.76 M)

88’ 2.5”(26.89 M)

20’ 4”(6.20 M)

31’ 6.5”(9.61 M)

159’ 1.4” (48.50 M)161’ 1.4” (49.11 M)

20’ 4” (6.20 M)

239’ 9” (73.08 M)

212’ 7” (64.80 M)

36’ 0”(10.97 M)

SCALEMETERS

0 2 4 6 8 10 12 14

FEET0 10 20 30 40 50

102’ 5.3” (31.22 M)19’ 4” (5.89 M)

60’ 4”(18.39 M)

70’ 7.5”(21.53 M)

13’ 0”(3.96 M)

777. 777T.O

. 00-105E-9

3 AIRCRAFT COMPOSITE MATERIALS-200A/B & -300

Colored areas indicate where the tough, light weightreinforced plastics improve damage resistance, damagetolerance, resist corrosion and fatigue. Composition is9% of structural weight. See next page for specificmaterial location. (Folding wing tips (optional) areillustrated in down position.)

INTERNAL VIEW

RUDDER

RUDDER TAB

ELEVATORS

HORIZONTAL STABILIZERTORQUE BOX SKIN/STRINGERS/SPARS

INBOARD FLAPS

OUTBOARD FLAPS

FAN COWL SUPPORTBEAM FAIRING


NOSE LANDING GEAR DOORS

VERTICAL STABILIZERTORQUE BOX SKIN/STRINGERS/SPARSOUTBOARD

AILERON

SPOILERS

FLAPERON

SPOILERS

UPPER/LOWERWING LEADINGEDGE

FORWARD AND AFTSTRUT FAIRING

ENGINE COWL -INLET, FAN,THRUST REVERSER

UPPER/LOWERWING LEADINGEDGE

HORIZONTAL STABILIZERLOWER/UPPER TRAILINGEDGE PANELS

AFT FUSELAGE SKIN PANELS

MAIN LANDINGGEAR DOORS

777. 777T.O

. 00-105E-9

AIRCRAFT COMPOSITE MATERIALS AND COMPONENT LOCATION

CARBON FIBER REINFORCED PLASTIC (CFRP)

ARAMID FIBER REINFORCED PLASTIC (AFRP)

GLASS FIBER REINFORCED PLASTIC (GFRP)

PYLON FAIRINGS

AILERON

FLAPS

FLAP TRACK FAIRINGS

SPOILERS

VERTICAL STABILIZERT/E PANELS

APRON

HORIZONTAL STABILIZER

MAIN LANDING GEAR TOP PANEL

SPOILER SHROUD TOP PANELS

L/E AND T/E BOTTOM ACCESS PANELS

LEG FAIRING DOOR

LANDING GEAR DOORS

BELLY FAIRING PANELS

RADOME

NOTE: CFRP passenger floor pan not shown.

4

777. 777T.O

. 00-105E-9

5


AIRCRAFT ENTRY -200A/B & 300


a. To open all entry/service doors: push in on red flaps to access the entry/service door handle. (left handle shown - right handle opposite)

b. Rotate handle counterclockwise 120 degrees.

c. Pull door outward.

d. Rotate entry/service door handle 180 degrees in the direction of the “open” arrow.

e. Pull door outward.

NOTES:

• Escape slide disarms automatically when door or hatch is opened from the outside.

• Flightdeck windows cannot be opened from the outside.

2. CUT-IN


MAINBATTERY

EQUIPMENTACCESS DOOR

AFTCARGODOOR

1aENTRY/SERVICEDOOR HANDLEAPU BATTERY

SURGE TANK9,300 GALS35,204 LITERS

HYDRAULIC ACCUMULATOR(LT WHEEL WELL)

HYDRAULIC RESERVOIR(RT WHEEL WELL)

OPTIONAL PASSENGEROXYGEN BOTTLES

SURGE TANK


PORTABLE OXYGEN BOTTLES

HYDRAULIC RESERVOIR(LT AND RT ENGINE STRUTS

PORTABLEOXYGENBOTTLES

OPTIONALPORTABLEOXYGENBOTTLESON FWDBLKHD FWDRT GALLEY

CREW OXYGENBOTTLE IN EECOMPARTMENTLT SIDE OFWHEEL WELL

ENGINE OILTANK FWD RT SIDE OFEACH ENGINE

APU

APU FUEL LINE

CENTER FUEL TANK 12,400 GALS 46,939 LITERS

RED FLAPSOPEN

WING TIP (UP)

777. 777T.O

. 00-105E-9

6

1. ENGINE SHUTDOWNa. Retard thrust levers, located on pilot’s center console, to RETARD position.


c. In case of engine fire, pull engine fire switches, located on pilot’s center console. Turn left or right to release agent. If not illuminated, push and hold the button under the switch to release.

d. In case of APU fire, pull APU fire switch, located on co-pilot’s overhead center console upper left side. Turn switch up or down to release agent. If not illuminated, push and hold the button under the switch to release.

e. Rotate APU control switch, located on pilot’s over head center panel, to OFF.

f. Press battery switch, located on pilot’s overhead center panel left side, to OFF.





1fBATTERY SWITCHNOTE:On symbol is removed.

1eAPU CONTROLSWITCH


1aTHRUSTLEVERS

1bFUEL CONTROLSWITCHES

1dAPU FIRESWITCH

ENGINE SHUTDOWN ANDAIRCREW EXTRACTION

777. 777T.O

. 00-105E-9

7

1. CHOP-OUT

a. Chop-out forward and aft cargo doors, located on right fuselage, to enter or exit if all other attempts fail. Chop-in or out is time consuming.

NOTE: Chop out areas are not marked on all aircraft.

EMERGENCY RESCUE ACCESS-200A/B & -300


ENTRY/SERVICE DOOR

ENTRY/SERVICEDOOR

ENTRY/SERVICEDOOR

ENTRY/SERVICE DOORS

ENTRY/SERVICEDOOR

BULK CARGO DOOR(RT SIDE) OPERATINGINSTRUCTIONS ON DOOR

ENTRY/SERVICE DOOR

AVERAGE DISTANCEFLOOR LEVEL TO GROUNDWHEELS RETRACTED: 8 FT 3 INWHEELS EXTENDED: 16 FT 6 IN

“CHOP OUT” AREASCARGO DOOR

(RT SIDE) OPERATINGINSTRUCTIONS ON DOOR



777. 777T.O

. 00-105E-9

8 CABIN CONFIGURATIONNOTE: A modular design allows airlines to move seats, galleys, and lavatories in a matter of hours to adapt to changing market conditions or for a CRAF situation. Seating configurations range from six abreast in first class to 10 abreast in economy class.

NOTE: The flightdeck is composed of two crew members only. Two observer seats are also located in the flightdeck.

6 ABREAST 7 ABREAST 9 ABREAST24 FIRST CLASS 54 BUSINESS CLASS 227 PREMIUM COACH CLASS

6 ABREAST 8 ABREAST 10 ABREAST24 FIRST CLASS 61 BUSINESS CLASS 243 PREMIUM COACH CLASS

6 ABREAST 9 ABREAST30 FIRST CLASS 345 PREMIUM COACH CLASS

777. 777T.O

. 00-105E-9 A ATTENDANT’ SEAT

G GALLEY

L LAVATORY

C CLOSET

W WARDROBE

PS PURSER STATION

-200LR (TYPICAL TWO CLASS)

9 CABIN CONFIGURATION-Continued

279 PASSENGERS 42 FIRST CLASS AT 60” PITCH 237 ECONOMY CLASS AT 34” PITCH


ACCESS TO OVERHEADPILOT CREW REST

OVERHEAD PILOTCREW REST

OVERHEADATTENDANT’SCREW REST

ACCESS TO OVERHEADATTENDANT CREW REST



OVERHEAD PILOTCREW REST


AA

L

L

G

L

G

G

C

G

WW

C

A

C

AA

L

L

L

L

G

G

G

G

W

AA A

LL

LL

G

G

GG

W

WAA

AAA

A

A

A

AAA

A

G

AL

L L

L

LAA

AA

A

A

W A

A

G

L LL

GC

CC

C

G G

777. 777T.O

. 00-105E-9

10

CABIN CONFIGURATION-Continued-200LR (TYPICAL THREE CLASS)

A ATTENDANT’ SEAT

G GALLEY

L LAVATORY

C CLOSET

W WARDROBE

PS PURSER STATION

296 PASSENGERS 6 FIRST CLASS AT 87” PITCH 42 BUSINESS CLASS AT 50” PITCH 248 ECONOMY CLASS AT 32” PITCH


OVERHEADPILOTCREW REST



AALL

GG

CG

W

C

A

L

AA L

LG

L

G

A

A A

L

LLL

G

G

G

L

A

A

A

L






AAL

L

G

GG

W

L

A

L

A

A

L

LGG

A

A A

L

LLL G

G

G

W

A

A

A

L

AA

L

GW

L A

A

G

W

777. 777T.O

. 00-105E-9

11

CABIN CONFIGURATION-Continued

A ATTENDANT’ SEAT

G GALLEY

L LAVATORY

C CLOSET

W WARDROBE

S/W STOWAGE/WARDROBE

-300ER (TYPICAL TWO CLASS)






AAL L

C

G

A

G

W

A

A

L

A AL

LG

W

G

A

AA

L

L

LLG

GGL

A

A

A

L

A

CG G

G G

G

A

WAA






A

C

L

L

CG

A

G

W

A

A

L

A

A

L

LGG

A

A C

L

L A

L

G

G

G

AA

A

AL

LC

C

GCC

G

A

C

AA

CL C

G

777. 777T.O

. 00-105E-9


A ATTENDANT’ SEAT

G GALLEY

L LAVATORY

C CLOSET

W WARDROBE

S/W STOWAGE/WARDROBE

-300ER (TYPICAL THREE CLASS)






A

L

L

G

A

G

W

A

A

LA

A

LL

GG

A

A

LL

G

L

G

G

G

A

L

A

AWL

S/W CCG

A

W

AA

CL

G G

G G A

A

L

L

L

L






AL

L

G

A

G

W

A

A

C L

A

G

A

A

GL

G

L

G

A

LA

AL

L

C

G

A

GC

CL

LG

A

AL L

C

C

AL

C C

777. 777T.O

. 00-105E-9

LOWER CARGO COMPARTMENTS13

-200LR, -300ER - CONTAINERS AND BULK CARGO

49’ 1”(14.96 M)

FORWARD CARGO COMPARTMENT


AFT CARGOCOMPARTMENT


BULK CARGOCOMPARTMENT


37’ 3”(11.35 M)

14’ 8”(4.47 M)

14’ 8”(4.47 M)

66’ 7”(20.29 M)

53’ 0”(16.15 M)

18 LD-3 CONTAINERS158 CU’ (4.5 CU M)CAPACITY EACH

14 LD-3CONTAINERS

BULK CARGO600 CU’ (17 CU M)CAPACITY


20 LD-3CONTAINERS


LD-3CONTAINER

LD-3CONTAINER

CROSS-SECTION

-200LR

-300ER

777. 777T.O

. 00-105E-9

LOWER CARGO COMPARTMENTS-Continued14

-200LR - OPTIONAL AFT LARGE CARGO DOORFORWARD CARGO COMPARTMENT







14 LD-3CONTAINERS


BULK CARGO600 CU’ (17 CU M)

8 LD-3KCONTAINERS

18 LD-3 CONTAINERS

TOTAL VOLUME 5.656 CU’ (160.2 CU M)

3 OPTIONALBODY FUEL TANKS










6-96X125” PALLETS 4-96X125” PALLETS BULK CARGO600 CU’ (17 CU M)


6-88X125” PALLETS 4-88X125” PALLETS& 2 LD-3 CONTAINERS

777. 777T.O

. 00-105E-9

LOWER CARGO COMPARTMENTS-Continued15

-300ER - OPTIONAL AFT LARGE CARGO DOOR FORWARD CARGO COMPARTMENT







20 LD-3CONTAINERS













6-96X125” PALLETS 4-96X125” PALLETS



8-88X125” PALLETS 6-88X125” PALLETS& 2 LD-3 CONTAINERS

8-96X125” PALLETS 6-96X125” PALLETS

OPTIONAL LOWERHOLD LAVATORIES

Documents

WELCOME TO TECHNICAL ORDER 00-105E-9, 1 FEBRUARY 2006, … Segment 21.pdf · 2007. 12. 18. · POINTS (2 16” PLACES) 8 ... b. Press release button on crew escape hatch, located