WELCOME TO TECHNICAL ORDER 00-105E-9, 1 FEBRUARY 2006 ... Segment 20.pdf · to go directly to the technical order, click on the continue button. ... flight deck windows open internally

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

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IN THIS SEGMENT.

THIS IS SEGMENT 20 COVERING CHAPTER 18 FROM THE 707 TO THE 737.

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 Retaining out of date rescue information can negatively affect the user’s operability and outcome of emergencies.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 20 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

707T.O

. 00-105E-9

707. AIRCRAFT PAINT SCHEME1

707T.O

. 00-105E-9

707. AIRCRAFT DIMENSIONS

Height 42’ 1” (12.83 M)

Length 152’ 11” (44.42 M)

Wing Span 145’ 9” (45.42 M)

707-320B/C

707-120B 707-320/-420

Wing Span 142’ 5” (44.42 M) Wing Span 130’ 10” (39.83 M)

Length 138’ 10” (42.32 M)

Height 41’ 8” (12.70M) Height 42’ 2” (12.85M)

Length 145’ 6” (44.35 M)

2

707T.O

. 00-105E-9

707.3 AIRCRAFT SKIN PENETRATION POINTS

AFT CARGO DOOR CENTER CARGO DOOR FWD CARGO DOOR

8”

2”

HANDLE

PENETRATIONPOINT

PENETRATIONPOINT

PENETRATIONPOINT

HANDLE

HANDLE

10”

3”

2”

2”

FWDFWDFWD

707T.O

. 00-105E-9

707.4 AIRCRAFT SKIN PENETRATION POINTS-Continued707-120B-320C TURBOFAN ENGINES

707-120B-320C TURBOFAN ENGINES

LEFT SIDE OF ENGINE

RIGHT SIDE OF ENGINE

COMMON POINT (LH & RH SIDE)


LEFT SIDE OF ENGINE


FORWARDENGINE MOUNT

213.942 AFTENGINE MOUNT MID SPAR

STRUT

COWLSPLIT COWL SPLIT

ENGINE

OUTBOARD NACELLE AND STRUT LEFT SIDE VIEW


ENGINE

MID SPAR

COWL SPLIT

COWLSPLIT

STRUT

213.942 AFTENGINE MOUNT

136.00 FORWARD ENGINE MOUNT

T/C FAIRING

FIRESEAL

FIRESEAL

707T.O

. 00-105E-9

707.5

SPECIAL TOOLS/EQUIPMENTPower Rescue Saw24 Foot Ladder35 Foot LadderFire Drill IIAIRCRAFT ENTRY-100/-200 SERIES

1. NORMAL/EMERGENCY ENTRY

a. Overwing escape hatches both sides- Push red panel, located top center of hatches, in and push hatches inward.

b. Pull handle, located left side forward and aft entry doors, outward and rotate clockwise.

c. Pull handle, located forward and aft galley doors right side, outward and rotate counterclockwise.

d. Press red handle, located on escape hatch top right forward crew compartment, and pull out.

2. CUT-IN

a. Cut along window lines as last resort.

NOTE: Some series are equipped with class one escape hatches.

CAUTION

For passenger and service doors, emergency slide will automatically deploy when doors are opened externally.

NOTE: Refer to the C-135 for more extensive information. Both airframes are identical except cargo and tanker capabilities.

434 GALS(1643 LITERS)


2283 GALS (8642 LITERS)


2333 GALS(8831LITERS)


UTILITY & AUXILIARY RESERVOIRIN AFT CARGO COMPARTMENT

PASSENGER OXYGENSYSTEM BOTTLES IN AFTCARGO COMPARTMENT

PORTABLE OXYGENBOTTLES OR NEARFLOOR LEVEL ONPARTITIONS

HYDRAULICACCUMULATORS(RIGHT WHEELWELL AREA)

FIRE EXTINGUISHERPORTS ON ENGINERIGHT COWLING(TYPICAL EACH ENGINE)

CREW OXYGEN SYSTEMBOTTLES IN FWD LOWEREDCEILING OR FWD CARGO AREA

7306 GALS(27,656 LITERS)

ENGINE OIL TANK-EACHENGINE-RIGHT SIDEPORTABLE OXYGEN BOTTLE ON

FORWARD SIDE OF BULKHEAD

BATTERIES

28” 28”38”

1cGALLEY DOOREXTERNAL HANDLE

1aPANEL

AIRCRAFT CROSS SECTION

2aCUT-IN AREAS

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

GALLEY DOOR(RT SIDE ONLY)

ON CARGOACFT ONLY

AFT ENTRY DOOR

CUT-IN AREA EACH SIDE OF ACFT (NOT MARKED ON ALL ACFT)

EMERGENCY EXITS

FWD ENTRYDOOR

GALLEY DOOR(RIGHT SIDE ONLY)

1bENTRY DOOREXTERNAL HANDLE

707T.O

. 00-105E-9

707.6 ENGINE SHUTDOWN ANDAIRCREW EXTRACTION1. ENGINE SHUTDOWN

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

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

c. Pull emergency fire T-handles, located top center above instrument panel.

d. Place engine start switches, located on pilot’s overhead panel, to OFF position.

e. In case of APU fire, pull APU fire switch, located on the upper left flight engineer’s panel, out to apply agent to APU.

f. If no APU fire, place APU master switch, located on the upper left flight engineer’s panel, to OFF position.

g. Place battery switch, located on lower right flight engineer’s panel, down to OFF position.

2. AIRCREW EXTRACTION

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

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

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

NOTE: Passenger seats are equipped with lap belts only.

APPLICABILITY: 707-100/-200 -300/-400

1cFIRE T-HANDLE

1dENGINE START SWITCHES

1gBATTERYSWITCH

1eAPU FIRE SWITCH

1fAPU MASTERSWITCH1b

START LEVERS

1aFIRE T-HANDLE

NOTE: Optional location for T-handles is on the pilot’s light shield.

707T.O

. 00-105E-9

707.7 EMERGENCY RESCUE ACCESS-100 AND -200 SERIES

CHOP OUT AREAS (NOTMARKED ON ALL AIRCRAFT)


AFT ENTRY DOOR

OVERWING ESCAPEHATCHES

FWD GALLEY DOOR

FWD ENTRY DOOR

FLIGHT DECK WINDOWSOPEN INTERNALLY

6 FEET 1/2 INCH FLOOR LEVEL TO GROUND, WHEELS RETRACTED

9 FEET 7INCH FLOOR LEVEL TO GROUND, WHEELS RETRACTED

AFTGALLEYDOOR

707T.O

. 00-105E-9

707.8

SPECIAL TOOLS/EQUIPMENTPower Rescue Saw24 Foot Ladder35 Foot LadderFire Drill IIAIRCRAFT ENTRY-300/-400 SERIES






2. CUT-IN



CAUTION





4036 GALS (15,278 LITERS)




UTILITY & AUXILIARY RESERVOIR(LEFT FILLET AREA)


PORTABLE OXYGENBOTTLES 8 PLACESON HATRACKS ORNEAR FLOOR LEVELON PARTITIONS




10,190 GALS(38,573 LITERS)

ENGINE OIL TANK-EACH ENGINE-RIGHT SIDE

PORTABLE OXYGEN BOTTLE ONFORWARD SIDE OF BULKHEAD

BATTERIES

28” 28”38”1cGALLEY DOOREXTERNAL HANDLE

1aPANEL


2aCUT-IN AREAS



ON CARGOACFT ONLY

AFT ENTRY DOOR


EMERGENCY EXITS

FWD ENTRYDOOR



APU FUELLINE

APU FWD CARGOCOMPARTMENT ON25000 SERIES

707T.O

. 00-105E-9

707.9 EMERGENCY RESCUE ACCESS-300 AND -400 SERIES



AFT ENTRY DOOR

AFTGALLEYDOOR

OVERWING ESCAPE HATCHES

FWD GALLEY DOOR

FWD ENTRYDOOR




CARGOAIRCRAFTONLY

707T.O

. 00-105E-9

707. CABIN CONFIGURATION-707-120B (PASSENGER)

10

137 PASSENGERS - MIXED CLASS (DOMESTIC)

142 PASSENGERS - MIXED CLASS (INTERNATIONAL)

ALL TOURIST ARRANGEMENT

GALLEY SERVICE DOOR 24X48” (61X121.9 CM)


MAIN ENTRY DOOR34X72” (86.4X183 CM)


32 PASSENGERS4 A BREAST AT 38”(96.4 CM) PITCH

105PASSENGERS6 A BREAST AT 34”(86.4 CM) PITCH

TYPE III EMERGENCY EXIT(LH & RH) 20X38” (51X96.5 CM)




C CLOSET

G GALLEY

L LAVATORY

S DOUBLE ATTENDANT’S SEAT C

L L G

SC C

CGG LLS

LL

G G

CS

L

L

G G C

S

L L G G

CS

L LG

S

G

C

707T.O

. 00-105E-9

707. CABIN CONFIGURATION-Continued-707-320/-320B/-420 (PASSENGER)

11

C CLOSET

G GALLEY

L LAVATORY

S DOUBLE ATTENDANT’S SEAT

ALL TOURIST ARRANGEMENT

189 PASSENGERS - 34” SEAT PITCH (86.4 CM)




18 FIRST CLASS 123 TOURIST




GGL L

S

GL L

S

GG L L

SC L

G L L

S C L

707T.O

. 00-105E-9

707. CABIN CONFIGURATION-Continued-707-320C (CARGO/PASSENGER)

12

C CLOSET

G GALLEY

L LAVATORY


ALL TOURIST - 194 PASSENGERS - 32.8” (82.5 CM) SEAT PITCH

7 PALLETS - 88X108” (274 CM) 69 PASSENGERS 34” (86.4 CM) SEAT PITCH

13 PALLETS - 88X125” (223X318 CM)

NOT INSTALLED ON -320C FREIGHTER

CARGO DOOR

CARGO DOOR

CARGO DOOR

THREE TO 10 PALLETS CAN BE ACCOMMODATED IN MIXED CARGO/PASSENGER CONFIGURATIONS.



91X134”(231X340 CM)

G G L L

SC L

GL

S

L

GL

S

GG L LS L

LL

GL

S

PASSENGERS PALLETS187 0131 3115 4103 5 87 6 69 7 57 8 33 9 29 10 0 13

717. 717T.O

. 00-105E-9

AIRCRAFT PAINT SCHEME1

717. 717T.O

. 00-105E-9

AIRCRAFT DIMENSIONS2

717-200

124’ 0”(37.8M)

77’ 11”(23.7M)

11’ 0”(3.4M) 10’ 10”

(3.3M) 52’ 8”(16.1M)

78’ 5”(23.8M)

7’ 7”(2.3M) 57’ 9”

(17.6M) 112’ 8”(34.3M)

36’ 10”(11.2M)

6’ 4”(1.9M)

16’ 0”(4.9M) 93’ 4”(28.4M)

FEET

METERS

0 10 20 30

0 5 10

717. 717T.O

. 00-105E-9

3 SKIN PENETRATION POINTSAND GENERAL INFORMATION

NOTE: The Boeing 717 is the previously named MD-95 after the design was acquired in 1997. It is the reconfigured DC-9-30.

GENERAL INFORMATION FOR ALL 717 MODELS AND VARIANTS

1. Current version is the 717-200. Available in basic and grossweight versions.

2. A proposed version is the 717-100 with 86 seats, formerly theMD-95-20.

3. Another proposed version will be the 717-100X Lite with 75seats.

4. Another proposed version will be the 717-300 for 130 seats.

SKIN PENETRATION POINTS

Fuselage (both sides)Penetrate approximately 4 inches below cabin

windows. Avoid penetrating emergency exits.

BASIC WEIGHT FUSELAGE VARIANT

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

GROSS WEIGHT FUSELAGE VARIANT

717. 717T.O

. 00-105E-9

4 ENGINE DANGER AREASJET INTAKE AND BLAST DISTANCES

NOTE:· These contours are to be used as guidelines only since the operational environment varies greatly - operational varies greatly-operated safety aspects are the responsi bility of the user/planner.

· All velocity values are statute miles per hour.

· Cross winds will have considerable effect on contours.

· Sea level static-standard day-zero ramp gradient.

AFT LIMIT OF ZONE A B C

(STATUTEWIND VELOCITY MPH) 300 100 60

TAKEOFF FEET 31 178 375 POWER METERS 11 54 114

BREAKAWAY FEET NA 35 78POWER METERS NA 11 24

FEET NA 30 50IDLE POWER METERS NA 9 15

GROUND PLANE

717. 717T.O

. 00-105E-9

5 AIRCRAFT DANGER AREAS1. EXTERIOR TAILCONE JETTISON

Jettisoning tailcone allows emergency ingress or egress. Prior to selecting jettison of tailcone, insure all personnel and equipment are clear of jettison area. Failure to clear area can cause damage to equipment and death or injury to personnel.

a. Using a ladder, proceed aft of left engine, locate jettison handle access door which is 10 feet (3 meters) above ground.

b. Push door and pull control handle. Inside lock cable must be re-installed if handle is pulled.

2. INTERIOR TAILCONE JETTISON

a. Proceed aft to rear cabin bulkhead, locate jettison handle on aircraft left wall and pull control handle.

TAILCONEJETTISON AREA

JETTISONED TAILCONE

1aEXTERIORTAILCONECONTROLS

WARNING

1aTAILCONEACCESS DOOR

2aINTERIORTAILCONECONTROLS

10 FT

717. 717T.O

. 00-105E-9

6

AIRCRAFT DANGER AREAS-ContinuedAPU ACCESS DOORS AND APU EXTERIOR CONTROLS

Use extreme caution when opening access areas where fire is evident.

1. APU ACCESS DOORS

a. Insert screw driver or similar tool into slot of cam-lock fasteners.

b. Turn fasteners to the left to open.

c. Pull down access doors.

2. APU EXTERIOR CONTROLS

a. Shut off APU by pressing the APU SHUT OFF/NORMAL switch UP.

b. If FIRE warning light is illuminated indicating APUfire, flip toggle switch cover up, select FIRE AGENT1 switch and press UP to discharge fire agent.

c. If FIRE light remains illuminated, repeat step a byselecting FIRE AGENT 2 switch. FIRE light will goout if fire is extinguished.

d. If fire is not extinguished, access APU through airintake, skin penetration, or other means available.

WARNING

APU AIR INTAKE 1aAPU ACCESS DOOR

APU FIREWARNING HORN

APU EXTERIOR CONTROLS

FIRE

APU FIRE

717. 717T.O

. 00-105E-9

AIRFRAME MATERIALSNOTE: All metal wing spars, glassfibre trailing edges on wings, ailerons, flaps, elevators, rudder, and detachable wing tips. Most of cabin floor made of balsa or Nomex core sandwich.

RADOME

COMPOSITES

ENTRANCE STAIR DOOR

WING TO BODY FAIRING

FLAP HINGE FAIRINGS

TAILCONE

ELEVATOR TABSTIP CAP

HORIZONTALSTABILIZERFAIRING

7

717. 717T.O

. 00-105E-9

8

SPECIAL TOOLS/EQUIPMENTPower Rescue Saw35 Foot LadderFire Drill II

AIRCRAFT ENTRY


a. OVERWING ESCAPE HATCHES, both sides, 4 places. To open, pull exterior handle, push inward at bottom and lift upward.

When doors are opened from outside, slide chutes automatically deploy. An opening door could injure rescue personnel.

b. LEFT FORWARD PASSENGER/SERVICE DOOR (Only left door has stair.) To open, using a ladder, (1) pull door handle out, (2) rotate counterclockwise, (3) push front door edge in, (4) pulling rear edge out and (5) swing door forward.

c. LEFT FORWARD PASSENGER/SERVICE DOOR (Deploying stairs.)(1) Pull door handle out and open slightly, (2) unlatch stair door byturning and holding battery switch “ON”, press and (3) hold “down”button until stair fully extends, and (4) open door fully.

d. RIGHT FORWARD EMERGENCY EXIT DOOR To open, pull handledown, located top center of door, and door lowers to open position.

NOTE: Doors are hinged at bottom edge.

e. PASSENGER AFT ENTRANCE DOOR AND STAIR Hold handle in“OPEN” position until stair is lowered. If aircraft hydraulic pressure is“OFF”, manually pull stair to maximum travel. Accumulator will provideinitial movement. (Rear ventral stairway is optional.)

2. CUT-IN

a. Cut 36” above any window with a cut out of 42” by 28” as a last resortto evacuate smoke and passengers.

WARNING

ESCAPEROPES

EXIT AND EVACUATIONSLIDE (2 PLACES)

LATCH

EXTERIORHANDLE

TOTAL FUEL CAPACITY:5,840 GALLONS(FUEL IN WINGS ONLY)

1aOVERWING EMERGENCY EIXT

EMERGENCY EXIT THROUGHSTAIRWAY OR THROUGH TAILCONE WHEN JETTISONED

FUEL TANKS (3) EVACUATION SLIDE

TAILCONEWALKWAYAND GUIDESTRAP

VENTRALSTAIRWAY

EXIT AND EVACUATION SLIDEOVERWING EMERGENCYEXITS (2 PLACES EACHSIDE)

28”

42”

36”

STAIR LIGHTSWITCH

RETURN TO OFF

CLOSED OFF OPEN

LOCKPINS

717. 717T.O

. 00-105E-9

9 AIRCRAFT EMERGENCY EGRESS1. CARGO COMPARTMENT DOOR

a. Push circular section of door handle inward to raise the handle.

b. Rotate door handle counterclockwise to unlatch door.

c. Push door upward into cargo compart-ment.

FLIGHTINTERPHONE(CREW)

SERVICEINTERPHONE(CABIN)

PUSH

PULL

(TYPICAL BOTH DOORS)

CARGO COMPARTMENTDOOR HANDLE

CARGO DOORS

DOOR/SLIDE

OXYGENBOTTLES

OVERWING EXITS

APU INTAKE(UNDERSIDE)

FLOORLEVEL

8 FEET

EXTERNAL POWER/COMM

BATTERY COMPARTMENT (UNDERSIDE)

APU AIRINTAKE

REAR STAIRCONTROL

APU EXTERNALSHUTDOWN

TAIL CONEJETTISON

DOOR/SLIDE

OVERWING EXITSDOOR/SLIDEAND STAIR

717. 717T.O

. 00-105E-9

10

AIRCRAFT FUEL AND APU SYSTEMS LOCATIONS

VENT BOX/OVERFLOW (UNDERSIDE)

FUEL TANKS FUEL LINES

VENT BOX/OVERFLOW (UNDERSIDE)

APU

APU

LOOKING FORWARD

FUEL LINES

717. 717T.O

. 00-105E-9

11

ENGINE/APU SHUTDOWN ANDAIRCREW EXTRACTION1. ENGINE/APU SHUTDOWN

a. Place fuel control levers, located on pilot’s centerconsole, to aft and OFF position.

b. Retard throttles, located on pilot’s center console, toIDLE CUTOFF position.

c. Place battery switch, located on center overhead panel,to OFF position.

NOTE: If engines fail to shutdown, pull emergency fire T-handles out, located on pilot’s center forward panel. Rotate handles as appropriate.

d. Place APU master switch, located on center overheadpanel, to OFF position.

e. On the APU ground control panel, located to left of APUaccess doors on the tail cone, place APU master switchto the APU shutoff position. Discharge fire agent 1 and/or 2 as applicable.


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

b. If seat tracks are not damaged during crash landing,use adjustable seat controls to retract seat to aftposition. Pilot’s controls are on right side of seat whileco-pilot’s are on the left.

c. Flight crew cabin seats are equipped with lap belts andshoulder harnesses.

d. Passenger seats are only equipped with lap belts.

BATTERY QUICKDISCONNECTS (3)

LH ENGINE RH ENGINE

FIRE T - HANDLES (PULLED OUT)

717. 717T.O

. 00-105E-9

12

EMERGENCY RESCUE ACCESS

AFT LOWER CARGOCOMPARTMENT DOOR

CHOP OUT AREAS

JETTISONABLETAILCONE

OVERWING EMERGENCY EXITS

FORWARD LOWERCARGO DOOR

FORWARD PASSENGERENTRANCE DOOR

CLEARVIEW WINDOW

AVERAGE DISTANCEFLOOR LEVEL TO GROUND

AFT BULKHEAD EMERGENCY EXIT DOOR TAILCONE

ACCESS DOOR

TAILCONEJETTISON LATCH

APU COMPARTMENTACCESS DOOR

FORWARD SERVICEENTRANCE DOOR

CLEARVIEW WINDOW -CHILL PANE WITH CO2AND BREAK WITH HEAVYFIRE AXE FOR ACCESSTO HANDLE; SLIDEWINDOW AFT

WHEELS RETRACTED: 4’WHEELS EXTENDED: 8’

2” WIDE BAND OF CONTRASTINGCOLOR INDICATING ALL DOORS,HATCHES AND WINDOWSEXTERNALLY OPERABLE.

717. 717T.O

. 00-105E-9

CABIN CONFIGURATION12

A ATTENDANT

G GALLEY

L LAVATORY

S STOWAGE

EFFECTIVITY: 717-200 TYPE III EMERGENCY EXIT(LH & RH) 20X36” (51X91.4 CM)




TYPE IMAIN ENTRY DOOR34X72” (86.4X183 CM)

TYPE IMAIN ENTRY DOOR34X72” (86.4X183 CM)

TYPE ISERVICE DOOR27X48” (69X122 CM)

TYPE ISERVICE DOOR27X48” (69X122 CM)

AFT ENTRY DOOR27.75X72” (70X183 CM)TAILCONE EMERGENCY EXIT

AFT ENTRY DOOR27.75X72” (70X183 CM)TAILCONE EMERGENCY EXIT

MIXED CLASS - 106 PASSENGERSFIRST CLASS - 8 SEATS ON 36” (91.4 CM) PITCH ECONOMY CLASS - 98 SEATS ON 32” (81.3 CM) PITCH

ALL ECONOMY CLASS - 117 PASSENGERS 5 - ABREAST ON 32” (91.3 CM) PITCH

L

G G

AA SGAA

L

L

AA

L

LS

G G

AA

720T.O

. 00-105E-9

720.1 AIRCRAFT PAINT SCHEME

720T.O

. 00-105E-9

720. AIRCRAFT DIMENSIONS2

The 720 was originally designated the 707-020 from amodified 707-120 design for medium-range operationfrom shorter runways. The aircraft is lighter and fasterthan the 707 and has a simplified wing design.

LENGTH 130’ 6” (39.78 M)

WING SPAN 130’ 10” (39.88 M)

720HEIGHT 41’ 5” (12.62 M)720BHEIGHT 41’ 2” (12.55 M)

720T.O

. 00-105E-9

720.3

AIRCRAFT SKIN PENETRATION POINTS

AFT CARGO DOOR CENTER CARGO DOOR FWD CARGO DOOR

8”

2”

HANDLE

PENETRATIONPOINT

PENETRATIONPOINT

PENETRATIONPOINT

HANDLE

HANDLE

10”

3”

2”

2”

FWDFWDFWD

720T.O

. 00-105E-9

720.4 AIRCRAFT SKIN PENETRATION POINTS-Continued720B TURBOFAN ENGINES

720B TURBOFAN ENGINES

LEFT SIDE OF ENGINE




LEFT SIDE OF ENGINE


FORWARDENGINE MOUNT

213.942 AFTENGINE MOUNT MID SPAR

STRUT

COWLSPLIT COWL SPLIT

ENGINE



ENGINE

MID SPAR

COWL SPLIT

COWLSPLIT

STRUT

213.942 AFTENGINE MOUNT

136.00 FORWARD ENGINE MOUNT

T/C FAIRING

FIRESEAL

FIRESEAL

720T.O

. 00-105E-9

720.5

SPECIAL TOOLS/EQUIPMENTPower Rescue Saw24 Foot Ladder35 Foot LadderFire Drill IIAIRCRAFT ENTRY






2. CUT-IN



CAUTION





2283 GALS (8642 LITERS)


2333 GALS(8831LITERS)


UTILITY & AUXILIARY RESERVOIRIN AFT CARGO COMPARTMENT


PORTABLE OXYGENBOTTLES OR NEARFLOOR LEVEL ONPARTITIONS





ENGINE OIL TANK-EACHENGINE-RIGHT SIDEPORTABLE OXYGEN BOTTLE ON

FORWARD SIDE OF BULKHEAD

BATTERIES

28” 28”38”

1cGALLEY DOOREXTERNAL HANDLE

1aPANEL


2aCUT-IN AREAS



ON CARGOACFT ONLY

AFT ENTRY DOOR


EMERGENCY EXITS

FWD ENTRYDOOR



720T.O

. 00-105E-9

720.6

ENGINE SHUTDOWN ANDAIRCREW EXTRACTION1. ENGINE SHUTDOWN


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

c. Pull emergency fire T-handles, located top center above instrument panel.

d. Place engine start switches, located on pilot’s overhead panel, to OFF position.

e. In case of APU fire, pull APU fire switch, located on the upper left flight engineer’s panel, out to apply agent to APU.

f. If no APU fire, place APU master switch, located on the upper left flight engineer’s panel, to OFF position.

g. Place battery switch, located on lower right flight engineer’s panel, down to OFF position.


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

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

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

NOTE: Passenger seats are equipped with lap belts only.

APPLICABILITY: 707-100/-200 -300/-400 720 & 720B

1cFIRE T-HANDLE

1dENGINE START SWITCHES

1gBATTERYSWITCH

1eAPU FIRE SWITCH

1fAPU MASTERSWITCH1b

START LEVERS

1aFIRE T-HANDLE


720T.O

. 00-105E-9

720.7 EMERGENCY RESCUE ACCESS



AFT ENTRY DOOR

OVERWING ESCAPEHATCHES

FWD GALLEY DOOR

FWD ENTRY DOOR




AFTGALLEYDOOR

720T.O

. 00-105E-9

720. CABIN CONFIGURATION8

C CLOSET

ES ESCAPE SLIDE

G GALLEY

L LAVATORY


EFFECTIVITY: 720, 720B (PASSENGER)

131 PASSENGERS - MIXED CLASS (DOMESTIC)


156* PASSENGERS - 6 A BREAST AT 34” (86.4 CM)

* ADDITIONAL PAIR OF EXITS REQUIREDFOR THIS CONFIGURATION: 149 PASSENGERSMAXIMUM ALLOWABLE WITH TWO TYPE IIIEMERGENCY EXITS.





MAIN ENTRY DOOR34X72” (86.4X183 CM) 30 PASSENGERS

4 A BREAST AT 38”(96.5 CM) PITCH


CLASS DIVIDER




C L G G

S

GLLLC

LL

LG

CSS

C LG G

C L G

SLLC

G

S

L

727. 727T.O

. 00-105E-9

AIRCRAFT PAINT SCHEME1

727. 727T.O

. 00-105E-9

AIRCRAFT DIMENSIONS2

727-100/-100C 727-200

LENGTH 116’ 2” (35.41 M)

HEIGHT 31’ 9” (9.68 M)

WING SPAN 108’ (32.92 M)

LENGTH 136’ 2” (41.50 M)

HEIGHT 31’ 7” (9.61 M)

WING SPAN 108’ (32.92 M)

727. 727T.O

. 00-105E-9

3 AIRCRAFT SKIN PENETRATION POINTS

727-200 (NOT ALL -200’S)

727-200

727-100 727-200

HANDLE

HANDLE

HANDLE

HANDLE

HANDLE

PENETRATION POINTS

PENETRATION POINTSPENETRATION POINTS

PENETRATION POINTS

PENETRATION POINTS

FWD

FWD FWD FWD

FWD

18”10” 8”

10” 10”

10”10”

17”

WING TO BODYFAIRING

727. 727T.O

. 00-105E-9

4 AIRCRAFT SKIN PENETRATION POINTS-Continued

LEFT SIDE OF ENGINE


SKIN SPLICE

COWL SPLIT

AFT COWL PANELFWD COWL PANEL

LEFT SIDE VIEWRIGHT SIDE VIEW

FWD COWLPANEL

COWLSPLIT

AFT COWLPANEL

3.75 DIAMETERCOWL VENT HOLE ATWL 209.60 AND BL 23.0 USE FOR FIREEXTINGUISHER ACCESS

COWL HINGE LINE

ENGINE

AFT MOUNT RING

NACELLE

FWD MOUNT RING

COWL SPLIT

INLET

COWL SPLIT

727-100/-200 SIDE ENGINELEFT SIDE VIEW

UP

FWD

3.75 DIAMETER COWLVENT HOLE AT NAC BL 0 USE FOR FIREEXTINGUISHER ACCESS

SKIN SPLICE727-100/-200 CENTER ENGINE

727. 727T.O

. 00-105E-9

AIRCRAFT DANGER AREAS

AXIAL DISTANCE BEHIND AIRCRAFT

DISTANCE FROMAIRCRAFT CENTERLINE

JT8D TURBOFAN ENGINE HAZARD AREASAT IDLE THRUST

INTAKE DANGER AREAS

INTAKE DANGER AREAS

18 FEET

18 FEET

4 FEET

NOSE COWLFORWARD EDGE

100 MPH(161 KMPH)

50 MPH(80 KMPH)

100 F(38 C)

200 F(93 C)

0

0

0

0

FEET

METERS

0 30 60 90 120 150

0 10 20 30 40

M30

30

20

10

0

20

10

5

0

5

10

5

F

10

727. 727T.O

. 00-105E-9

AIRCRAFT DANGER AREAS-ContinuedJT8D TURBOFAN ENGINE HAZARD AREASAT TAKEOFF THRUST

INTAKEDANGER AREAS

25 FEET

25 FEET

METERS

FEET 0 50 100 150 200 250 300

0 10 20 30 40 50 60 70 80 90 100

AXIAL DISTANCE BEHIND AIRCRAFT

DISTANCE FROMAIRCRAFT CENTERLINE

M F

30

20

10

0

10

20

10

10

5

5

0

100 F (38 C)0

150 F(65 C)

200 F(93 C)

300 F(149 C)0

0

0

0

400 MPH(644 KMPH)

300 MPH(483 KMPH)

200 MPH(322 KMPH)

150 MPH(240 KMPH)

50 MPH(80 KMPH)(TO 512 FT157M)

100 MPH(161 KMPH)

6

0

0

030

727. 727T.O

. 00-105E-9

7

AIRCRAFT COMPOSITE LOCATIONS

FIN TIP FAIRING

RAIN GUTTER

WING TO BODY FAIRING

RADOME

LEADING EDGE ACCESS PANELS

COMPOSITE LOCATIONS

727. 727T.O

. 00-105E-9

8 US MARSHALS SERVICE 727 VERSION1. US MARSHALS SERVICE 727 VERSION

Type Aircraft: 727 Saberliner used to transport prisoners.

Models involved:727-100 (93 passengers, 3 crew, and a deputy crew of 12 to 17)727-100 (95 passengers, 3 crew, and a deputy crew of 12 to 17)727-200 (configuration is similar)

Seat Positions: All seats face forward except the ones over the wingwhich face aft. A large center aisle between the seats goes from oneside to the other side where the emergency exit is over the wings.

2. PRISONER TRANSPORTATION

In 1995, the air fleets of the Marshals Service and the Immigration andNaturalization Service (INS) merged to create the Justice Prisoner andAlien Transportation System (JPATS). The merger created a moreefficient and effective system for transporting prisoners and criminalaliens. Operated by the Marshals Service, JPATS is one of the largesttransporters of prisoners in the world, handling hundreds of requestsevery day to move prisoners between judicial districts, correctionalinstitutions and foreign countries.

On average, more than 200,000 prisoner and alien movements a year arecompleted by the Marshals Service via coordinated air and groundsystems. Most of these prisoners are transported aboard Service-ownedaircraft and vehicles.

Since 1984, the Marshals Service has acquired a fleet of aircraft thatincludes three Boeing 727s, a DC-9, several smaller jets and turbopropairplanes. These planes move thousands of prisoners for the MarshalsService, Bureau of Prisons (BOP) and INS, as well as the U.S. militaryand state and local governments. Many of the airplanes were acquired atno cost through the Government Surplus Property Program and theAsset Seizure and Forfeiture Program.

The JPATS is the only government-operated, scheduled passengerairline in the nation. It serves 40 cities, and is used to move prisonersmore economically and with higher security than commercial airlines.

The U.S. Marshals Service assumes custody of individuals arrested byall federal agencies and is responsible for the housing and transportationof prisoners from the time they are brought into federal custody untilthey are either acquitted or incarcerated.

Moving thousands of prisoners and criminal aliens each year requiresextra security precautions and careful coordination. Deputy Marshals,Aviation Enforcement Officers and Aviation Safety Officers are stationedthroughout the aircraft, and prisoners wear handcuffs and leg irons in theclose confines of the aircraft cabin.

Ground security is provided by Deputy Marshals, BOP guards or INSofficers at each airport transfer point. If prisoners cannot be moved inone day, they are housed overnight at various BOP facilities. Carefulscheduling is required to ensure that each prisoner appears in court atthe designated time.

In an effort to assist state and local law enforcement agencies, theMarshals Service transports non-federal prisoners between differentjurisdictions when space is available on its aircraft.

For example, a fugitive wanted for trial in one locale may have beenapprehended in another, distant jurisdiction. However, local authoritiesare often reluctant to seek extradition of felons because of high transpor-tation and personnel costs. The Marshals Service offers state and locallaw enforcement agencies a safe and effective prisoner transportationsystem at about one-quarter of the normal cost.

727. 727T.O

. 00-105E-9

9

SPECIAL TOOLS/EQUIPMENTPower Rescue Saw24 Foot LadderFire Drill IIAIRCRAFT ENTRY

1. NORMAL ENTRY

If Forward Entry Door is used for rescue, passenger escape chute-slide will be actuated if not disconnected from inside.

a. RIGHT FORWARD ENTRY DOOR - Pull handle outward, rotate clockwise and pull door outward to open position.

2. EMERGENCY ENTRYa. PILOT’S SLIDING WINDOW - (RH & LH) Cargo and (RH only passenger aircraft.b. OVERWING ESCAPE HATCHES - Push panel in, located top center of hatches, and push hatches inward and up.c. FORWARD ENTRY DOOR - Pull external handle, located on entry door, outward, rotate clockwise and pull door out to open position.d. MID GALLEY DOOR - Pull external handle, located on galley door right forward side, outward, rotate counterclockwise and pull door out to open position.e. AFT EXIT DOORS - Pull lower end of handle, located top center of door left side of fuselage, outward, rotate clockwise and pull door outward. (Turn handle counterclockwise on doors located on right side of fuselage.)f. AIRSTAIR ENTRY DOOR - Depress latch on access door, located right side aft fuselage, and pull handle down to release stairway. (Stairway can jack aircraft up for passenger escape in a no-gear situation.)g. AFT ENTRY DOOR - Rotate handle, located on aft entry door, clockwise and push door inward.

3. CUT-INa. Cut tenth window aft from crew compartment and fifth window forward from tail section as last resort.

NOTE: Oxygen, rafts, flashlights, and fire extinguishers are located in overhead compartments.

WARNING

NOTE: Refer to the C-22 for more extensive information. Both airframes are identical except for military configurations.

AFT CARGO FUEL TANKS (OPTIONAL) 860 US GALS (FWD) 3255 LITERS 1070 US GALS (AFT) 4050 LITERS

2FWD CARGO FUEL TANKS (OPTIONAL)810 US GALS (EACH CELL)3066 LITERS 1

1

2

VENT SURGE TANK

1793 GALS6787 LITERS

PORTABLE OXYGEN BOTTLESOXYGEN BOTTLES PASSENGERAND CREW

MAIN BATTERY

PORTABLE OXYGENBOTTLES

HYD ACCUMULATOR (WHEEL WELL)APU EMER CONTROL PANEL(LEFT WHEEL WELL AREA)

ENG OIL TANK (TYPICAL)

FIRE EXT PORT(OUTBD ENG)

HYD ACCUMULATOR(AIRSTAIR PASSAGE)

HYD RESERVOIR(AIRSTAIRPASSAGE)

PORTABLEOXYGENBOTTLEAPU

(WHEELWELL)

FUEL LINES

1793 GALS6787 LITERS

4004 GALS15,155 LITERS VENT SURGE TANK

28” 28”38” AIRCRAFTCROSS-SECTION

CUT-INAREAS

2eDOORHANDLE

1a, 2cEXTERNALHANDLE

2dMID GALLEY DOOR(RT SIDE ONLY)

2eAFT EXIT DOOR

2gAFT ENTRY DOOR

2fAFT AIRSTAIR2b

EMERGENCY OVERWINGESCAPE HATCHES

2bPANEL

HYDRAULICHANDPUMP

2fAIRSTAIR DOORRELEASE HANDLE

2dEXTERNALHANDLE

2cFWD ENTRY DOOR 3a

CUT-IN

2aPILOT’SSLIDINGWINDOW

ACCESSDOOR

727. 727T.O

. 00-105E-9

10

ENGINE SHUTDOWN ANDAIRCREW EXTRACTION1. ENGINE SHUTDOWN


b. Retard engine start levers, located on pilot’s console, to CUT OFF position.

c. In case of engine fire, pull appropriate engine fire T-handles, located on center overhead instrument panel glare shield.


d. In case of APU fire, pull APU fire switch to OFF and place APU master switch to OFF, located on rear cockpit wall.

e. Lift guard and place battery switch, located on lower center flight engineer’s upper left panel, to OFF position.


a. Unlatch lap belt and remove shoulder harness from crewmembers

b. FLIGHT ENGINEER’S SEAT - Depress seat control handles and rotate seat clockwise.

c. PASSENGER’S SEATS - Passengers seats are equipped with lap belts only.

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

1cENGINE FIRE T-HANDLES 1c

ENGINE FIRE T-HANDLES

1dAPU FIRESWITCH

1dAPUMASTERSWITCH

1aTHRUSTLEVERS

1bENGINESTARTLEVERS

BULKHEAD RIGHT OFFLIGHT ENGINEER’SPANEL

727. 727T.O

. 00-105E-9

11




“CHOP OUT” AREA

CARGO DOOR (OPENS FROM INSIDE ONLY)

5 FEET 8 INCHES (FLOOR LEVEL TO GROUND, WHEELS RETRACTED)9 FEET 1 INCH (FLOOR LEVEL TO GROUND, WHEELS EXTENDED)

“CHOP OUT” AREAS

“CHOP OUT” AREA

GALLEY DOOR(MOVED FWD ON 200,REMOVED ON 200F)

FWD ENTRY DOOR

AFT ENTRY DOOR (OPENSFROM INSIDE OF THE AFTSTAIRS AREA) (AIRSTAIRMUST FIRST BE LOWERED)

AFT AIRSTAIR EXTERIORCONTROL PANEL OPERATINGINSTRUCTIONS ON ACCESSPANEL

AFT AIRSTAIR

AFT EXIT DOORS(REMOVED ON 100 AND 200F)

PILOT’S SLIDINGWINDOW

727. 727T.O

. 00-105E-9

CABIN CONFIGURATION12

EFFECTIVITY: 727-100/-100C (PASSENGER)

STOWAGE

TYPE 1 GALLEY SERVICEDOOR 33X65” (84X165 CM)

AFT ENTRY DOOR32X76 “ (81X193 CM)

WINDSCREEN

FWD ENTRY DOOR34X72 “ (97X183 CM)

TYPE IV EXIT(RH & LH) 20X38 “ (51X97 CM)TYPE III EMERGENCY

EXIT (RH & LH) 20X38 “ (51X97 CM)

106 PASSENGERS - TYPICAL MIXED CLASS (16 FIRST CLASS, 90 TOURIST)

16 PASSENGERS4 ABREAST AT 38” (97 CM) PITCH

90 PASSENGERS3 ABREAST AT 33” (84 CM) PITCH

STOWAGE34” (86 CM) TYPICAL

126 PASSENGERS - ALL TOURIST (MAXIMUM CERTIFICATED CAPACITY - 129 PASSENGERS)

C CLOSET

ES ESCAPE SLIDE

G GALLEY

L LAVATORY


C

C

G G L

L

L

L

GG ES

ESS

LS

L

727. 727T.O

. 00-105E-9

CABIN CONFIGURATION-Continued13

ES ESCAPE SLIDE

G GALLEY

L LAVATORY


EFFECTIVITY: 727-100C (PASSENGER/CARGO)

TYPE 1GALLEY SERVICE DOOR 33X65” (84X165 CM)


SMOKEBARRIER

CARGO DOOR86X34 “ (218X340 CM) SMOKE-TIGHT PARTITION

TYPE IVTYPE III

EMERGENCY EXIT (RH & LH) 20X38 “ (51X97 CM)


70 PASSENGERS

CARGO DOORCONTROL PANEL

88X108” PALLETS (122X274 CM)

88X108” PALLETS (122X274 CM)

88X108” PALLETS (122X274 CM)

56 PASSENGERS

52 PASSENGERS

G

G

S

S

S

G GL

ES

L

L

L

L

L

L

L

L

ES

ES

ES

727. 727T.O

. 00-105E-9

14

CABIN CONFIGURATION-ContinuedEFFECTIVITY: 727-100C (ALL CARGO)

CARGO DOOR86X34 “ (218X340 CM)

1 2 3 4 5 6 7 8L

L

L

L LAVATORY

CONDITIONS

HATRACKS UP

2” CLEARANCE

9 COMMERCIAL PALLETS

HIGH-PROFILE ROLLERS

PALLET VOLUME NOT INCLUDED IN CARGO VOLUME

PALLET SIZE 88X108"(223X274 CM)

88X125"(223X318 CM)

MAIN DECK

PALLET 1 359 (10.17) 401 (11.36)

PALLETS 2-8 366 (10.4) EACH2,562 (72.56)

APPROX.411 (11.6) EACH

2,877 (81.47)

LOWER DECK 890 (25.2) 890 (25.2)

TOTAL VOLUME 3,811 (107.9) 4,168 (11.8)

CARGO ENVELOPE VOLUMES IN CUBIC FEET (CUBIT METERS)

g

727. 727T.O

. 00-105E-9

15

CABIN CONFIGURATION-Continued

C CLOSET

ES ESCAPE SLIDE

G GALLEY

L LAVATORY


EFFECTIVITY: 727-200 (PASSENGER)

L L

LS

GES

ESESG G

SES

WIND SCREEN

155 PASSENGERS - TYPICAL ALL-TOURIST(MAXIMUM CERTIFICATED CAPACITY - 189 PASSENGERS)

34” (86 CM) TYPICAL

134 PASSENGERS - TYPICAL MIXED CLASS (20 FIRST CLASS, 114 TOURIST)


STOWAGE(RH & LH)

TYPE 1GALLEY SERVICE DOOR 33X65” (84X165 CM)

CLASSDIVIDER

WINDSCREEN




TYPE III EMERGENCY EXIT (RH & LH) 20X38 “ (51X97 CM)

TYPE 1SERVICE DOOR (RH & LH)30X60” (76X152 CM)

737. 737T.O

. 00-105E-9

1 AIRCRAFT PAINT SCHEME NEXT GENERATION 737-600/-700/-800/-900

737. 737T.O

. 00-105E-9

2 AIRCRAFT DIMENSIONS

737-600

67’ 9” (20.65m)62’ 9” (19.13m)

102’ 6” (21.24m)

29’ 6” (8.84m)

15’ 10” (4.83m)

12’ 4” (3.76m)

(29.79m) 97’ 9”

41’ 3” (12.57m)

(34.32m) 112’ 7”

47’ 1” (14.35m)

(2.44 m)APPROX 8’

18’ 9” (5.72m)

SCALEMETERS 0 2 4 6

FEET 0 5 10 15 20 25

36’ 10” (11.23m)13’ 5” (4.09m)

737-700

72’ 2” (22.00m)67’ 2” (20.47m)

110’ 4” (33.63m)

34’ 0” (10.36m)

15’ 10” (4.83m)

12’ 4” (3.76m)

(32.18m) 105’ 7”

41’ 3” (12.57m)

(34.32m) 112’ 7”

47’ 1” (14.35m)

(2.44 m)APPROX 8’ 18’ 9”

(5.72m)SCALE

METERS 0 2 4 6

FEET 0 5 10 15 20 25

41’ 4” (12.60m)13’ 5” (4.09m)

NOTE: 737-600s are the current smallest version of the fleet. Earlier versions i.e., -100/-200/-300/-400/-500 models are similar until the mid 1990’s upgrades when longer versions were requested by Boeing’s customers, hence the -600/-700/-800/-900 models were developed. The earlier versions will be referred to as some of these aircraft are still in service in many countries. Military versions of the T-43 and C-40A/B/C are addressed in separate files of this manual.

(737-100/-200/-300/-400/-500 prior to engine and aircraft upgrades.)

737. 737T.O

. 00-105E-9

737-800

82’ 0” (24.99m)77’ 0” (23.47m)

129’ 6” (39.47m)

43’ 10” (13.36m)

15’ 10” (4.83m)

12’ 4” (3.76m)

(38.02m) 124’ 9”

41’ 3” (12.57m)

(34.32m) 112’ 7”

47’ 1” (14.35m)

(2.44 m)APPROX 8’

18’ 9” (5.72m)

SCALEMETERS 0 2 4 6

FEET 0 5 10 15 20 25

51’ 2” (15.60m)13’ 5” (4.09m)

737-900

87’ 2” (26.57m)82’ 2” (25.05m)

138’ 2” (41.11m)

(14.73m)

15’ 10” (4.83m)

12’ 4” (3.76m)

(40.67m) 133’ 5”

41’ 3” (12.57m)

112’ 7”

47’ 1” (14.35m)

(2.44 m)APPROX 8’ 18’ 9”

(5.72m)SCALE

METERS 0 2 4 6

FEET 0 5 10 15 20 25

56’ 4” (17.17m)13’ 5” (4.09m)

AIRCRAFT DIMENSIONS-Continued3

(34.32m)

48’ 4”

737. 737T.O

. 00-105E-9


737-700 WITH WINGLETS

110’ 4” (33.63m)

34’ 0” (10.36m)

15’ 10” (4.83m)

12’ 4” (3.76m)

105’ 7” (32.18m)

(12.57m)

117’ 5”(35.79m)

47’ 1” (14.35m)

(2.44m)APPROX 8’18’ 9” (5.72m)

SCALEMETERS 0 2 4 6

FEET 0 5 10 15 20 25

41’ 4” (12.60m)13’ 5” (4.09m)

75’ 6” (23.01m)


129’ 6” (39.47m)

43’ 10” (13.36m)

15’ 10” (4.83m)

12’ 4” (3.76m)

124’ 9” (38.02m)

41’ 2” (12.55m)

117’ 5”(35.79m) 47’ 1” (14.35m)

(2.44 m)APPROX 8’18’ 9” (5.72m)

SCALEMETERS 0 2 4 6

FEET 0 5 10 15 20 25

51’ 2” (15.60m)13’ 5” (4.09m)

85’ 4” (26.01m) 41’ 3”

737. 737T.O

. 00-105E-9



138’ 2” (42.11m)

48’ 4” (14.73m)

15’ 10” (4.83m)

12’ 4” (3.76m)

133’ 5” (40.67m)

41’ 2”

117’ 5” (35.79m)47’ 1”

(2.44 m)APPROX 8’18’ 9” (5.72m)

SCALEMETERS 0 2 4 6

FEET 0 5 10 15 20 25

56’ 4” (17.17m)13’ 5” (4.09m)

90’ 6” (27.58m)

(12.55m)

(14.35m)

737. 737T.O

. 00-105E-9

6 AIRCRAFT SKIN PENETRATION POINTS

PENETRATION POINTS

PENETRATION POINTS

FWD

HANDLE

5”

C

5”

LC

8”8”

HANDLE

FWD

L

NOTE: Typical penetration areas for all models.

737. 737T.O

. 00-105E-9

7 AIRCRAFT SKIN PENETRATION POINTS-Continued

FORWARD FAIRING

C FRONT MOUNT

C AFT MOUNT

AFT STRUT FAIRINGS THRUSTREVERSERS

SIDE COWL

3.75” DIAMETER COWL VENTHOLE AT NAC BL 0.0 USE FORFIRE EXTINGUISHER ACCESS

NOSE COWL

LL LC AFT MOUNT

C FRONT MOUNTLFORWARD FAIRING

NOSE COWLSIDE COWL

3.75” DIAMETER COWL VENTHOLE AT NAC BL 0.0 USE FORFIRE EXTINGUISHER ACCESS

INBOARDENGINE NACELLE

OUTBOARD ENGINE NACELLE

ENGINE NACELLE LEFT SIDE VIEW

ENGINE NACELLERIGHT SIDE VIEW

PENETRATIONPOINT

PENETRATION POINT PENETRATION POINT

L CNACELLE

C NACELLE L

PENETRATIONPOINT

THRUST REVERSER COWL

THRUSTREVERSERCOWL

WING WING

0.6” WIDE ANNULARVENT - USE FORFIRE EXTINGUISHERACCESS TO ENGINECORE

0.6” WIDE ANNULARVENT - USE FORFIRE EXTINGUISHERACCESS TO ENGINECORE

FAN COWL

C NACELLEL

OIL TANKFILLER DOOR

C 2.5” X 9.0” COWL VENT AT BL0USE FOR FIRE EXTINGUISHERACCESS TO FAN COMPARTMENT

L2.5” X 9.0” COWL VENT AT BL0USE FOR FIRE EXTINGUISHERACCESS TO FAN COMPARTMENT

L

FAN COWL

NACELLE CL

C

737-300/-400/-500/-600/-700/-800/-900

737-100/-200

737. 737T.O

. 00-105E-9

GRAPHITE COMPOSITESEFFECTIVITY: -100/-200/-300/-400/-500

AIRFRAME MATERIALS8

LOWER WING FIXEDLEADING EDGE PANELS

FLAPTRACKFAIRINGS

NOSELANDINGGEARDOORS

LOWER WINGFIXED TRAILINGEDGE PANELS

SPOILERS

WING TRAILING EDGEMAIN FLAP ASSEMBLY

AILERONS/TABSKINAND STRUCTURE

ENGINE COWL

RADOME

NACELLESTRUTFAIRING

UPPERWINGFIXEDLEADINGEDGEPANELS

VERTICALSTABILIZER TIP

RUDDER

HORIZONTALSTABILIZERTRAILINGEDGE

UPPER WINGFIXED TRAILINGEDGE PANELS

TAILCONE ASSEMBLY

ELEVATOR TABSTRUCTURE

MAIN LANDINGGEAR DOORSAND FAIRINGS

WING TOBODYFAIRING

737. 737T.O

. 00-105E-9

GRAPHITE OR FIBERGLASS GRAPHITE COMPOSITESEFFECTIVITY: -600/-700/-800/-900

AIRFRAME MATERIALS-Continued9

WINGLETS(AS INSTALLED)



FLAP TRACKFAIRINGS



DORSALFIN SKIN

ELEVATORUPPER &LOWER SKIN


AILERONS/TAB SKINAND STRUCTURE

THRUSTREVERSER

RADOME

NACELLESTRUTFAIRING



TAILCONEASSEMBLY

RUDDER

VERTICALSTABILIZERTRAILINGEDGE


737. 737T.O

. 00-105E-9

GRAPHITE OR FIBERGLASS GRAPHITE COMPOSITESEFFECTIVITY: BOEING BUSINESS JET (BBJ)/BBJ-2

AIRFRAME MATERIALS-Continued10




FLAP TRACKFAIRINGS



DORSALFIN SKIN ELEVATOR

UPPER &LOWER SKIN


AILERONS/TAB SKINAND STRUCTURETHRUST

REVERSERRADOME

NACELLESTRUTFAIRING



TAILCONEASSEMBLY

RUDDER

VERTICALSTABILIZERTRAILINGEDGE


ELEVATOR TABSTRUCTURE

737. 737T.O

. 00-105E-9

AUXILIARY FUEL TANK CAPACITIES11

3 AFT

3 AFT/1 FWD

4 AFT 3 AFT/2 FWD 4 AFT/2 FWD 5 AFT/2 FWD

5 AFT/3 FWD

5 AFT/4 FWD

NOTE: This information includes Boeing Business Jets.

AUX FUEL GALLONS LITERS TOTAL GALLONS(ALL TANKS)

TOTALLITERS

(ALL TANKS)

3 AFT 1,485 5,685 8,360 31,710

4 AFT 2,010 7,676 8,885 33,701

3 AFT - 1 FWD 2,000 7,639 8,875 33,664

3 AFT - 2 FWD 2,530 9,647 9,405 35,672

4 AFT - 2 FWD 3,055 11,639 9,930 37,664

5 AFT - 2 FWD 3,360 12,797 10,235 38,822

5 AFT - 3 FWD 3,605 13,727 10,480 39,752

5 AFT - 4 FWD 3,850 14,656 10,725 40,681

737. 737T.O

. 00-105E-9

12

SPECIAL TOOLS/EQUIPMENTPower Rescue Saw12 Foot LadderFire Drill IIAIRCRAFT ENTRY-100/-200/-300/-400/-500 SERIES

1. NORMAL/EMERGENCY ENTRYa. Push in top center panel on overwing escape hatches, located on both fuselage sides. Push hatch inward and upward.

NOTE: Some models are equipped with stairs that can be deployed from forward and aft entry doors.

b. Pull handle on forward and aft entry doors, located left side of fuselage, outward and rotate clockwise. Pull doors outward.

NOTE: Depress button and pull handle out, rotate clockwise to extend stairway.

c. Pull handle on right forward and aft service doors, outward and rotate counterclockwise. Pull doors outward.

CAUTION

When doors are opened from outside, chutes automatically deploy.

2. CUT-IN OR CHOP OUT AREASa. Cut along window line as the last resort.

NOTE: Refer to the T-43 for more extensive information. Both airframes are identical except for military trainer capabilities.

-100/-200

-300/-400&-500

BATTERIES

E/ECOMPARTMENT ACCESS DOOR

MAINE/E DOOR-300 (OPTIONAL

FWD ENTRY DOOR

1bFWD AND AFT ENTRYDOOR EXTERNALHANDLE (LT SIDE)

AFT ENTRYDOOR

1a EMERGENCY OVERWING EXIT HATCHES PUSH PANEL (BOTH SIDES)

ENGINE OIL TANK (ONE EACH ENGINE)RT SIDE CFM-56 LT SIDE ALL OTHERS

1cFWD AND AFT SERVICE DOOREXTERNAL HANDLE (RT SIDE)

4299GALS16,273LITERS

CREW OXYGEN BOTTLE(FWD CARGO AREA)

PASSENGEROXYGEN(OPTIONAL)

PORTABLEOXYGENBOTTLE(BEHINDCO-PILOT)

1288 GALLONS4876 LITERS

VENT SURGE TANK

VENT SURGE TANK1288 GALLONS 4876 LITERS

SYSTEM A, B & STANDBYHYD RESERVOIRS INWHEEL WELL

APU OIL TANKPORTABLE OXYGEN BOTTLES(VARIEDLOCATIONS)

APU FUEL LINESAPU EMER CONTROL PANEL (RT W W)

HYD BRAKE ACCUMULATORS (IN W W)

OPTIONAL AUX FUELTANK IN LWR AFTCARGO COMPT

390/492/984 GALLONS1476/1862/3725 LITERS

1

1

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13 EMERGENCY RESCUE ACCESS


ADDITIONAL OVERWING ESCAPEHATCHES ( -400 ONLY)

CUT IN OR CHOP OUT AREAS

CUT-IN OR CHOP OUT AREAS LOCATED BETWEENWING FRONT SPAR AND ESCAPE HATCH (THREEBAYS) BELOW WINDOWS AND ABOVE FLOORS

AVERAGE DISTANCE -FLOOR LEVEL TO GROUNDWHEELS RETRACTED: 5 FTWHEELS EXTENDED: 8 FT. 6 IN.

FWD ENTRY DOOR

PILOT’S SLIDINGWINDOW

FWD SERVICE DOOR

CARGO DOOR (RT SIDE)OPERATING INSTRUCTIONSON DOOR


AFT SERVICE DOOR

AFT ENTRY DOOR

EFFECTIVITY:-100/-200/-300/-400/-500 SERIES


2” WIDE BAND OF CONTRASTINGCOLOR INDICATING ALL DOORS,HATCHES AND WINDOWSEXTERNALLY OPERABLE

CARGODOOR-200C

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14

AIRCRAFT ENTRY-ContinuedAIRCRAFT ENTRY -600/-700/-800 SERIES1. NORMAL ENTRY

NOTE: Some models are equipped with stairs that can be deployed from forward and aft entry doors.

a. Pull handle on forward and aft entry doors, located left side of fuselage, outward and rotate clockwise. Pull doors outward.

NOTE: Depress button and pull handle out, rotate clockwise to extend stairway.

b. Pull handle on right forward and aft service doors, outward and rotate counterclockwise. Pull doors outward.

c. The pilot’s sliding window can be accessed by pulling the external handle and sliding window open.

CAUTION

When doors are opened from outside, chutes automatically deploy.

BATTERY

E/E COMPARTMENTACCESS DOOR

-600/-700/-800ACCESSIBLE FROM FWDCARGO COMPARTMENT

FWD ENTRY DOOR

1aFWD AND AFT ENTRY DOOREXTERNAL HANDLE (RT SIDE)

AFT ENTRYDOOR

2aEMERGENCY OVERWING EXIT HATCHES(BOTH SIDES) (See also page 737.11)

ENGINE OIL TANK RT SIDE EACH ENGINE

1bFWD AND AFT SERVICE DOOREXTERNAL HANDLE (LT SIDE)

4299 GALS16,273 LITERS

CREW OXYGENBOTTLE (FWDCARGO AREA)

PORTABLEOXYGENBOTTLE(BEHINDCO-PILOT)

1288 GALLONS4876 LITERS

VENT SURGE TANK

1288 GALLONS 4876 LITERS

SYSTEM A, B & STANDBYHYD RESERVOIRS INWHEEL WELL

APU OIL TANK

PORTABLE OXYGEN BOTTLES(VARIEDLOCATIONS)

APU FUEL LINEAPU EMER CONTROL PANEL (RT W W)

HYD BRAKE ACCUMULATORS (IN W W)

AUXILIARYFUEL TANKLOCATIONS(BBJ ONLY)

WINGLETS (AS INSTALLED)


1cPILOTWINDOW

737. 737T.O

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AIRCRAFT ENTRY-Continued15

2. EMERGENCY ENTRYa. Push in top center on overwing escape hatches, located on both fuselage sides (see page 737.16 for hatch locations.)

3. CARGO DOOR OPERATIONa. To open cargo door 1, unlock the external door handle.

b. Verify unlocked light in ON.

c. Hold the UP TO CANOPY switch (illustrated in red) in UP position until door motion stops.

4. CUT-IN OR CHOP OUT AREASa. Cut-in or chop out areas are located between wing front spar and escape hatch (three bays) below windows and above floors. (see page 737.11)

2aEMERGENCY OVERWINGEXIT HATCHES (BOTH SIDES)

3aEXTERNAL CARGODOOR CONTROLS

4aCUT-IN AREAS

3cUP TO CANOPY SWITCH

3bCARGO DOOR LIGHTS

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16



ADDITIONAL OVERWING ESCAPEHATCHES (-800/-900 ONLY)


CUT IN OR CHOP OUT AREAS LOCATEDBETWEEN WING FRONT SPAR ANDESCAPE HATCH (THREE BAYS) BELOWWINDOWS AND ABOVE FLOORS

AVERAGE DISTANCE -FLOOR LEVEL TO GROUNDWHEELS RETRACTED: 5 FTWHEELS EXTENDED: 8 FT. 6 IN.

FWD ENTRY DOOR

PILOT’SSLIDINGWINDOW

FWD SERVICE DOOR



AFT SERVICE DOOR

AFT ENTRY DOOR

EFFECTIVITY:-600/-700/-800 SERIES

2” WIDE BAND OF CONTRASTINGCOLOR INDICATING ALL DOORS,HATCHES AND WINDOWSEXTERNALLY OPERABLE

CARGODOOR -700C


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17

ENGINE SHUTDOWN ANDAIRCREW EXTRACTION1. ENGINE SHUTDOWN (-100 thru -800 & BBJ)


b. Retard engine start levers, located on pilot’s console, to CUT OFF position.

c. In case of engine fire, pull appropriate engine fire T-handles, located on center console forward of thrust levers. Turn right or left to discharge agent. If not illuminated, push and hold the button under the switch to release.

d. In case of APU fire, pull the APU fire T-handle, located on center console forward of thrust levers. Turn right or left to discharge agent.

e. Place APU master switch up to OFF position OR OFF position. (Switch type can vary.)

f. Lift guard and place battery switch, located on pilot’s center overhead panel, to OFF position.


a. Unlatch lap belt and remove shoulder harness from crewmembers. See page T-43.5 for view of seats and associated controls.

b. FLIGHT ENGINEER’S SEAT - Depress seat control handles and rotate seat clockwise.

c. PASSENGER’S SEATS - Passengers seats are equipped with lap belts only.

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

1eAPU MASTER SWITCH

1bENGINE START LEVERS

1dAPU FIRESWITCH

1cENGINE FIRE T-HANDLES

1fBATTERYSWITCH

1aTHRUSTLEVERS

OR

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CABIN CONFIGURATIONSEFFECTIVITY: -100/-200/-300/-400/-500/-600 (NO WINGLETS) (SEE SEPARATE FILES FOR T-43 AND C-40A/B/C)

MIXED CLASS8 FIRST CLASS SEATS AT 36 - IN PITCH120 ECONOMY CLASS SEATS AT 32 - PITCH

[A] ATTENDANT [C] CLOSET [G] GALLEY [L] LAVATORY [S] STORAGE

MIXED CLASS90 BUSINESS CLASS SEATS AT 34 - IN PITCH36 ECONOMY CLASS SEATS AT 32 - PITCH

SINGLE CLASS140 ECONOMY CLASS SEATS AT 32 - IN PITCH (SHOWN)OR 148 ECONOMY CLASS SEATS AT 30 - PITCH

737. 737T.O

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CABIN CONFIGURATIONS-Continued19





EFFECTIVITY: -700 (WITH OR WITHOUT WINGLETS)

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CABIN CONFIGURATIONS-Continued20

EFFECTIVITY: -800 (WITH OR WITHOUT WINGLETS)





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CABIN CONFIGURATIONS-Continued21 EFFECTIVITY: -900 (WITH OR WITHOUT WINGLETS)


[A] ATTENDANT [C] CLOSET [G] GALLEY [L] LAVATORY

SINGLE CLASS177 ECONOMY CLASS SEATS AT 32 - IN PITCHOR 189 ECONOMY CLASS SEATS AT 31 - PITCH

Documents

WELCOME TO TECHNICAL ORDER 00-105E-9, 1 FEBRUARY 2006 ... Segment 20.pdf · to go directly to the technical order, click on the continue button. ... flight deck windows open internally