Segment 20 Covering Chapter 18 from the 707 to the 737

WELCOME TO TECHNICAL ORDER 00-105E-9, 1 FEBRUARY 2006, REVISION 11. THIS IS SEGMENT 20 COVERING CHAPTER 18 FROM THE 707 TO THE 737.

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WRITTEN CORRESPONDENCE:

HQ AFCESA/CEXF ATTN: Fire and Emergency Services Egress Manager 139 Barnes Drive Suite 1 Tyndall 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) 283-6150 DSN 523-6150

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

For technical order improvements, correcting procedures, and other inquiries, please use the above media most convenient. SEGMENT 20 INFORMATION CHANGE NOTICE This page is provided to notifiy the user of any informational changes made to Technical Order 00-105E-9 in this Segment and the current Revision. Informational changes will be referenced in the Adobe Reader’s Bookmark tool as a designator symbol illustrated as a <[C]> for quick reference to the right of the affected aircraft. The user shall insure the most current information contained in this TO is used for his operation. Retaining out of date rescue information can negatively affect the user’s operability and outcome of emergencies. If the user prints out pages his unit requires, the user shall print the affected page(s), remove and destroy the existing page(s), and insert the newly printed page(s) in the binder provided for that purpose. A Master of this TO shall be retained in the unit’s library for reference, future printing requirements and inspections.

CHAPTER AIRCRAFT PAGE EXPLANATION OF CHANGE None. TO 00-105E-9 NOTE

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

DC-3 DC-6 DC-7 DC-8 DC-9 DC-10 MD-11 MD-80 MD-90 L-1011-1 L-1011-500 707 717 720 727 737 747 757 767 777

Chapter 18 Cover 707.

T.O. 00-105E-9

1 AIRCRAFT PAINT SCHEME 707 707.

T.O. 00-105E-9 AIRCRAFT DIMENSIONS

2 707

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

707-120B 707-320/-420

Length 138’ 10” (42.32 M) Length 145’ 6” (44.35 M)

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

Height 42’ 1” (12.83 M)

707-320B/C

Length 152’ 11” (44.42 M)

Wing Span 145’ 9” (45.42 M) 707.

T.O. 00-105E-9 AIRCRAFT SKIN PENETRATION POINTS

3 707

FWD CARGO DOOR AFT CARGO DOOR CENTER CARGO DOOR

10” HANDLE 8” HANDLE 3” HANDLE 2” 2” PENETRATION PENETRATION 2” POINT POINT PENETRATION POINT

FWD FWD FWD 707.

T.O. 00-105E-9 AIRCRAFT SKIN PENETRATION POINTS-Continued

4 707 707-120B-320C TURBOFAN ENGINES FORWARD 213.942 AFT ENGINE MOUNT ENGINE MOUNT MID SPAR LEFT SIDE OF ENGINE RIGHT SIDE OF ENGINE STRUT

COMMON POINT (LH & RH SIDE)

COWL SPLIT COWL SPLIT ENGINE

OUTBOARD NACELLE AND STRUT LEFT SIDE VIEW

FIRESEAL

707-120B-320C TURBOFAN ENGINES 136.00 FORWARD 213.942 AFT ENGINE MOUNT ENGINE MOUNT MID SPAR

LEFT SIDE OF ENGINE T/C FAIRING STRUT RIGHT SIDE OF ENGINE

COMMON POINT (LH & RH SIDE)

COWL SPLIT ENGINE COWL SPLIT

OUTBOARD NACELLE AND STRUT LEFT SIDE VIEW

FIRESEAL 707.

T.O. 00-105E-9 SPECIAL TOOLS/EQUIPMENT NOTE:

5 707 Power Rescue Saw Refer to the C-135 for more 24 Foot Ladder extensive information. Both PORTABLE OXYGEN 35 Foot Ladder airframes are identical except BOTTLES OR NEAR FLOOR LEVEL ON Fire Drill II cargo and tanker capabilities. PARTITIONS AIRCRAFT ENTRY-100/-200 SERIES 434 GALS (1643 LITERS) 1. NORMAL/EMERGENCY ENTRY HYDRAULIC ACCUMULATORS 2333 GALS (RIGHT WHEEL a. Overwing escape hatches both sides- (8831 LITERS) WELL AREA) Push red panel, located top center of hatches, in and push hatches inward. FIRE EXTINGUISHER 2283 GALS PASSENGER OXYGEN PORTS ON ENGINE (8642 SYSTEM BOTTLES IN AFT b. Pull handle, located left side forward and RIGHT COWLING LITERS) CARGO COMPARTMENT (TYPICAL EACH ENGINE) aft entry doors, outward and rotate clockwise. UTILITY & AUXILIARY RESERVOIR IN AFT CARGO COMPARTMENT c. Pull handle, located forward and aft galley CREW OXYGEN SYSTEM BOTTLES IN FWD LOWERED 2283 GALS 2333 GALS doors right side, outward and rotate counter- CEILING OR FWD CARGO AREA (8642 LITERS) (8831LITERS) 434 GALS clockwise. (1643 LITERS)

d. Press red handle, located on escape hatch top right forward crew compartment, and pull out. 7306 GALS (27,656 LITERS) BATTERIES 2. CUT-IN ENGINE OIL TANK-EACH PORTABLE OXYGEN BOTTLE ON ENGINE-RIGHT SIDE a. Cut along window lines as last resort. FORWARD SIDE OF BULKHEAD 1c AIRCRAFT CROSS SECTION NOTE: GALLEY DOOR 38” 1a 28” 28” Some series are equipped with class one EXTERNAL HANDLE PANEL escape hatches. 2a CUT-IN AREAS CAUTION

For passenger and service doors, emergency NOTE: slide will automatically deploy when doors are 2 inch band of contrasting color around all doors, windows and hatches operable from opened externally. EMERGENCY EXITS ON CARGO outside the aircraft. ACFT ONLY FWD ENTRY DOOR

AFT ENTRY DOOR

GALLEY DOOR 1b GALLEY DOOR ENTRY DOOR (RIGHT SIDE ONLY) CUT-IN AREA EACH SIDE OF ACFT (RT SIDE ONLY) EXTERNAL HANDLE (NOT MARKED ON ALL ACFT) 707.

T.O. 00-105E-9 ENGINE SHUTDOWN AND APPLICABILITY: 6 707 707-100/-200 AIRCREW EXTRACTION -300/-400 1. ENGINE SHUTDOWN

a. Retard thrust levers, located on pilot’s center 1d console, to RETARD position. ENGINE START SWITCHES

b. Place engine start levers, located on pilot’s 1c center console, to CUT OFF position FIRE T-HANDLE 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. 1g NOTE: e. In case of APU fire, pull APU fire switch, BATTERY Optional location for T-handles located on the upper left flight engineer’s SWITCH is on the pilot’s light shield. panel, out to apply agent to APU.

f. If no APU fire, place APU master switch, 1a located on the upper left flight engineer’s FIRE T-HANDLE panel, to OFF position. 1e g. Place battery switch, located on lower right APU FIRE SWITCH flight engineer’s panel, down to OFF position.

2. AIRCREW EXTRACTION

a. Unlatch lap belts and remove shoulder harness 1f from crewmembers. APU MASTER SWITCH b. Depress seat control handles, located on flight 1b engineer’s seat, and rotate from left to right. START LEVERS

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. 707.

T.O. 00-105E-9

7 EMERGENCY RESCUE ACCESS 707 -100 AND -200 SERIES

AFT GALLEY DOOR

OVERWING ESCAPE HATCHES

CHOP OUT AREAS (NOT MARKED ON ALL AIRCRAFT) AFT ENTRY DOOR

CHOP OUT AREAS (NOT FWD GALLEY DOOR MARKED ON ALL AIRCRAFT)

FWD ENTRY DOOR

FLIGHT DECK WINDOWS 6 FEET 1/2 INCH FLOOR LEVEL TO GROUND, WHEELS RETRACTED OPEN INTERNALLY 9 FEET 7INCH FLOOR LEVEL TO GROUND, WHEELS RETRACTED 707.

T.O. 00-105E-9 SPECIAL TOOLS/EQUIPMENT NOTE:

8 707 Refer to the C-135 for more Power Rescue Saw PORTABLE OXYGEN 24 Foot Ladder extensive information. Both BOTTLES 8 PLACES 35 Foot Ladder airframes are identical except ON HATRACKS OR Fire Drill II cargo and tanker capabilities. NEAR FLOOR LEVEL AIRCRAFT ENTRY-300/-400 SERIES 434 GALS ON PARTITIONS (1643 LITERS) 1. NORMAL/EMERGENCY ENTRY HYDRAULIC ACCUMULATORS 2285 GALS (RIGHT WHEEL a. Overwing escape hatches both sides- (8650 LITERS) WELL AREA) Push red panel, located top center of hatches, in and push hatches inward. FIRE EXTINGUISHER 4036 GALS PASSENGER OXYGEN PORTS ON ENGINE (15,278 SYSTEM BOTTLES IN AFT b. Pull handle, located left side forward and RIGHT COWLING LITERS) CARGO COMPARTMENT (TYPICAL EACH ENGINE) aft entry doors, outward and rotate clockwise. UTILITY & AUXILIARY RESERVOIR APU FUEL (LEFT FILLET AREA) LINE c. Pull handle, located forward and aft galley CREW OXYGEN SYSTEM 4036 GALS 2285 GALS BOTTLES IN FWD LOWERED doors right side, outward and rotate counter- (15,278 LITERS) (8650 LITERS) 434 GALS CEILING OR FWD CARGO AREA clockwise. (1643 LITERS) APU FWD CARGO d. Press red handle, located on escape hatch top COMPARTMENT ON right forward crew compartment, and pull out. 25000 SERIES 10,190 GALS (38,573 LITERS)

2. CUT-IN BATTERIES ENGINE OIL TANK-EACH ENGINE- RIGHT SIDE PORTABLE OXYGEN BOTTLE ON a. Cut along window lines as last resort. FORWARD SIDE OF BULKHEAD 1c AIRCRAFT CROSS SECTION NOTE: GALLEY DOOR 38” 1a 28” 28” Some series are equipped with class one EXTERNAL HANDLE PANEL escape hatches. 2a CUT-IN AREAS CAUTION

AFT ENTRY DOOR

GALLEY DOOR 1b GALLEY DOOR ENTRY DOOR (RIGHT SIDE ONLY) CUT-IN AREA EACH SIDE OF ACFT (RT SIDE ONLY) EXTERNAL HANDLE (NOT MARKED ON ALL ACFT) 707.

T.O. 00-105E-9

9 EMERGENCY RESCUE ACCESS 707 -300 AND -400 SERIES

AFT GALLEY DOOR CARGO AIRCRAFT ONLY

AFT ENTRY DOOR

CHOP OUT AREAS (NOT MARKED ON ALL AIRCRAFT)

CHOP OUT AREAS (NOT OVERWING ESCAPE HATCHES MARKED ON ALL AIRCRAFT)

FWD GALLEY DOOR

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

FLIGHT DECK WINDOWS FWD ENTRY 10 FEET 1INCH FLOOR LEVEL TO GROUND, WHEELS RETRACTED OPEN INTERNALLY DOOR 707.

T.O. 00-105E-9

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

C CLOSET TYPE III EMERGENCY EXIT GALLEY SERVICE GALLEY SERVICE G GALLEY (LH & RH) 20X38” (51X96.5 CM) DOOR 24X48” DOOR 24X48” L LAVATORY (61X121.9 CM) (61X121.9 CM) L G S DOUBLE ATTENDANT’S L G G C L SEAT S C C SC L 32 PASSENGERS 105PASSENGERS 4 A BREAST AT 38” 6 A BREAST AT 34” (96.4 CM) PITCH MAIN ENTRY DOOR (86.4 CM) PITCH MAIN ENTRY DOOR 34X72” (86.4X183 CM) 34X72” (86.4X183 CM) 137 PASSENGERS - MIXED CLASS (DOMESTIC)

L L G G G G L S C S C L 20 PASSENGERS 122PASSENGERS 4 A BREAST AT 40” 6 A BREAST AT 34” (101.6 CM) PITCH (86.4 CM) PITCH

142 PASSENGERS - MIXED CLASS (INTERNATIONAL)

L L G G G G C L S S C L

174PASSENGERS 6 A BREAST AT 34” (86.4 CM) PITCH ALL TOURIST ARRANGEMENT 707.

T.O. 00-105E-9

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

GALLEY SERVICE C CLOSET GALLEY SERVICE TYPE III EMERGENCY EXIT DOOR 24X48” DOOR 24X48” (LH & RH) 20X38” (51X96.5 CM) (61X121.9 CM) G GALLEY (61X121.9 CM) L LAVATORY

S DOUBLE ATTENDANT’S SEAT L L G G G G L L L S C S

MAIN ENTRY DOOR 18 FIRST CLASS 123 TOURIST MAIN ENTRY DOOR 34X72” (86.4X183 CM) 34X72” (86.4X183 CM) 141 PASSENGERS - MIXED CLASS (INTERNATIONAL)

L L G G L L S S C L

189 PASSENGERS - 34” SEAT PITCH (86.4 CM) ALL TOURIST ARRANGEMENT 707.

T.O. 00-105E-9

12 CABIN CONFIGURATION-Continued 707 -707-320C (CARGO/PASSENGER) THREE TO 10 PALLETS CAN BE ACCOMMODATED IN MIXED CARGO/PASSENGER CONFIGURATIONS.

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

L LAVATORY L L G G G L L S C S L S DOUBLE ATTENDANT’S SEAT 91X134” CARGO (231X340 CM) DOOR ALL TOURIST - 194 PASSENGERS - 32.8” (82.5 CM) SEAT PITCH

L G G L G L PASSENGERS PALLETS S S L 187 0 131 3 CARGO 115 4 DOOR 103 5 87 6 69 7 7 PALLETS - 88X108” (274 CM) 69 PASSENGERS 34” (86.4 CM) SEAT PITCH 57 8 33 9 29 10 0 13 NOT INSTALLED ON -320C FREIGHTER L G L S L CARGO DOOR

13 PALLETS - 88X125” (223X318 CM) 717.

T.O. 00-105E-9

1 AIRCRAFT PAINT SCHEME 717 717.

T.O. 00-105E-9 AIRCRAFT DIMENSIONS 2 717 717-200 124’ 0” (37.8M)

77’ 11” (23.7M)

11’ 0” 10’ 10” (3.4M) (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) FEET 0 10 20 30 93’ 4” METERS 0 5 10 (28.4M) 717.

T.O. 00-105E-9 SKIN PENETRATION POINTS 3 717 AND GENERAL INFORMATION SKIN PENETRATION POINTS NOTE: The Boeing 717 is the previously named MD-95 after the design Fuselage (both sides) was acquired in 1997. It is the reconfigured DC-9-30. Penetrate approximately 4 inches below cabin windows. Avoid penetrating emergency exits. GENERAL INFORMATION FOR ALL 717 MODELS AND VARIANTS

1. Current version is the 717-200. Available in basic and gross weight versions. 2. A proposed version is the 717-100 with 86 seats, formerly the MD-95-20. 3. Another proposed version will be the 717-100X Lite with 75 seats. 4. Another proposed version will be the 717-300 for 130 seats. BASIC WEIGHT FUSELAGE VARIANT

ENGINE NACELLES (BOTH SIDES) GROSS WEIGHT FUSELAGE VARIANT PENETRATE MID-SECTION OF ENGINE BELOW ENGINE CENTERLINE 717.

T.O. 00-105E-9 ENGINE DANGER AREAS 4 717 JET INTAKE AND BLAST DISTANCES AFT LIMIT OF ZONE NOTE: A B C · These contours are to be used as guidelines only since (STATUTE the operational environment varies greatly - operational WIND VELOCITY MPH) 300 100 60 varies greatly-operated safety aspects are the responsi bility of the user/planner. TAKEOFF FEET 31 178 375 POWER METERS 11 54 114 · All velocity values are statute miles per hour. BREAKAWAY FEET NA 35 78 · Cross winds will have considerable effect on contours. POWER METERS NA 11 24

· Sea level static-standard day-zero ramp gradient. FEET NA 30 50 IDLE POWER METERS NA 9 15

GROUND PLANE 717.

T.O. 00-105E-9 AIRCRAFT DANGER AREAS

5 717 1. EXTERIOR TAILCONE JETTISON 2a WARNING INTERIOR TAILCONE Jettisoning tailcone allows emergency ingress or CONTROLS 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 TAILCONE jettison handle on aircraft left wall and pull JETTISON AREA control handle. 1a TAILCONE ACCESS DOOR

1a EXTERIOR JETTISONED TAILCONE TAILCONE CONTROLS 10 FT 717.

T.O. 00-105E-9 AIRCRAFT DANGER AREAS-Continued 717

6 APU ACCESS DOORS AND APU EXTERIOR CONTROLS

WARNING

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. APU AIR INTAKE 1a APU ACCESS DOOR 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 APU fire, flip toggle switch cover up, select FIRE AGENT 1 switch and press UP to discharge fire agent. APU EXTERIOR CONTROLS c. If FIRE light remains illuminated, repeat step a by selecting FIRE AGENT 2 switch. FIRE light will go out if fire is extinguished. APU FIRE FIRE WARNING HORN d. If fire is not extinguished, access APU through air intake, skin penetration, or other means available.

APU FIRE 717.

T.O. 00-105E-9

7 AIRFRAME MATERIALS 717 NOTE: All metal wing spars, glassfibre trailing edges on wings, ailerons, flaps, elevators, rudder, and detachable wing tips. Most of cabin floor made TIP CAP ELEVATOR TABS of balsa or Nomex core sandwich.

HORIZONTAL COMPOSITES STABILIZER FAIRING

TAILCONE

WING TO BODY FAIRING FLAP HINGE FAIRINGS

ENTRANCE STAIR DOOR

RADOME 717.

T.O. 00-105E-9 SPECIAL TOOLS/EQUIPMENT TOTAL FUEL CAPACITY: 1a 717 8 Power Rescue Saw 5,840 GALLONS OVERWING EMERGENCY EIXT 35 Foot Ladder (FUEL IN WINGS ONLY) LATCH EMERGENCY EXIT THROUGH Fire Drill II STAIRWAY OR THROUGH TAIL EXTERIOR CONE WHEN JETTISONED AIRCRAFT ENTRY HANDLE FUEL TANKS (3) EVACUATION 1. NORMAL/EMERGENCY ENTRY SLIDE TAILCONE a. OVERWING ESCAPE HATCHES, both sides, 4 places. To open, WALKWAY pull exterior handle, push inward at bottom and lift upward. LOCKPINS AND GUIDE STRAP WARNING EXIT AND EVACUATION SLIDE (2 PLACES) VENTRAL When doors are opened from outside, slide chutes automatically STAIRWAY deploy. An opening door could injure rescue personnel.

b. LEFT FORWARD PASSENGER/SERVICE DOOR (Only left door OVERWING EMERGENCY EXIT AND EVACUATION SLIDE has stair.) To open, using a ladder, (1) pull door handle out, (2) EXITS (2 PLACES EACH rotate counterclockwise, (3) push front door edge in, (4) pulling SIDE) rear edge out and (5) swing door forward. ESCAPE ROPES c. LEFT FORWARD PASSENGER/SERVICE DOOR (Deploying stairs.) (1) Pull door handle out and open slightly, (2) unlatch stair door by turning 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 handle down, located top center of door, and door lowers to open position.

NOTE: Doors are hinged at bottom edge. RETURN TO OFF CLOSED OFF OPEN 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 provide 28” initial movement. (Rear ventral stairway is optional.) 42” 2. CUT-IN

36” a. Cut 36” above any window with a cut out of 42” by 28” as a last resort STAIR LIGHT to evacuate smoke and passengers. SWITCH 717.

T.O. 00-105E-9 AIRCRAFT EMERGENCY EGRESS

9 717 1. CARGO COMPARTMENT DOOR

a. Push circular section of door handle OVERWING EXITS TAIL CONE DOOR/ inward to raise the handle. DOOR/SLIDE JETTISON AND STAIR SLIDE b. Rotate door handle counterclockwise to unlatch door.

c. Push door upward into cargo compart- APU EXTERNAL ment. SHUTDOWN EXTERNAL BATTERY COMPARTMENT APU AIR POWER/COMM (UNDERSIDE) REAR STAIR INTAKE CONTROL

OVERWING EXITS OXYGEN BOTTLES FLOOR LEVEL 8 FEET DOOR/SLIDE FLIGHT APU INTAKE INTERPHONE (UNDERSIDE) CARGO DOORS (CREW)

SERVICE INTERPHONE (CABIN)

PUSH CARGO COMPARTMENT DOOR HANDLE PULL

(TYPICAL BOTH DOORS) 717.

T.O. 00-105E-9 AIRCRAFT FUEL AND APU SYSTEMS LOCATIONS 10 717

VENT BOX/OVERFLOW (UNDERSIDE)

FUEL TANKS FUEL LINES

LOOKING FORWARD APU

FUEL LINES

VENT BOX/OVERFLOW (UNDERSIDE) APU 717.

T.O. 00-105E-9 ENGINE/APU SHUTDOWN AND

11 717 AIRCREW EXTRACTION FIRE T - HANDLES 1. ENGINE/APU SHUTDOWN (PULLED OUT)

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

b. Retard throttles, located on pilot’s center console, to IDLE 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. LH ENGINE RH ENGINE d. Place APU master switch, located on center overhead panel, to OFF position.

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

2. AIRCREW EXTRACTION

a. Unlatch lap belt and remove shoulder harness from crewmember(s). BATTERY QUICK b. If seat tracks are not damaged during crash landing, DISCONNECTS (3) use adjustable seat controls to retract seat to aft position. Pilot’s controls are on right side of seat while co-pilot’s are on the left.

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

d. Passenger seats are only equipped with lap belts. 717.

T.O. 00-105E-9

12 EMERGENCY RESCUE ACCESS 717

JETTISONABLE AFT BULKHEAD TAILCONE EMERGENCY 2” WIDE BAND OF CONTRASTING EXIT DOOR TAILCONE COLOR INDICATING ALL DOORS, ACCESS DOOR HATCHES AND WINDOWS EXTERNALLY OPERABLE. OVERWING EMERGENCY TAILCONE EXITS JETTISON LATCH

FORWARD LOWER CARGO DOOR

FORWARD SERVICE APU COMPARTMENT ENTRANCE DOOR ACCESS DOOR AFT LOWER CARGO CLEARVIEW WINDOW - COMPARTMENT DOOR CHILL PANE WITH CO2 CHOP OUT AREAS AND BREAK WITH HEAVY FIRE AXE FOR ACCESS TO HANDLE; SLIDE WINDOW AFT

FORWARD PASSENGER ENTRANCE DOOR

AVERAGE DISTANCE FLOOR LEVEL TO GROUND WHEELS RETRACTED: 4’ CLEARVIEW WINDOW WHEELS EXTENDED: 8’ 717.

T.O. 00-105E-9

12 CABIN CONFIGURATION TYPE III EMERGENCY EXIT 717 EFFECTIVITY: 717-200 TYPE I (LH & RH) 20X36” (51X91.4 CM) A ATTENDANT SERVICE DOOR 27X48” (69X122 CM) G GALLEY G G L L LAVATORY A A S STOWAGE A L SG L

TYPE I MAIN ENTRY DOOR TYPE III EMERGENCY EXIT AFT ENTRY DOOR 34X72” (86.4X183 CM) (LH & RH) 20X36” (51X91.4 CM) 27.75X72” (70X183 CM) TAILCONE EMERGENCY EXIT MIXED CLASS - 106 PASSENGERS FIRST CLASS - 8 SEATS ON 36” (91.4 CM) PITCH ECONOMY CLASS - 98 SEATS ON 32” (81.3 CM) PITCH

TYPE III EMERGENCY EXIT (LH & RH) 20X36” (51X91.4 CM) TYPE I SERVICE DOOR 27X48” (69X122 CM)

G G L A A A A S L

TYPE I MAIN ENTRY DOOR AFT ENTRY DOOR TYPE III EMERGENCY EXIT 34X72” (86.4X183 CM) 27.75X72” (70X183 CM) (LH & RH) 20X36” (51X91.4 CM) TAILCONE EMERGENCY EXIT

ALL ECONOMY CLASS - 117 PASSENGERS 5 - ABREAST ON 32” (91.3 CM) PITCH 720. T.O. 00-105E-9

1 AIRCRAFT PAINT SCHEME 720 720. T.O. 00-105E-9

2 AIRCRAFT DIMENSIONS 720 The 720 was originally designated the 707-020 from a modified 707-120 design for medium-range operation from shorter runways. The aircraft is lighter and faster than the 707 and has a simplified wing design.

WING SPAN 130’ 10” (39.88 M)

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

LENGTH 130’ 6” (39.78 M) 720. T.O. 00-105E-9 AIRCRAFT SKIN PENETRATION POINTS 720

AFT CARGO DOOR CENTER CARGO DOOR FWD CARGO DOOR

10” HANDLE 8” HANDLE 3” HANDLE 2” 2” PENETRATION PENETRATION 2” POINT POINT PENETRATION POINT

FWD FWD FWD 720. T.O. 00-105E-9 AIRCRAFT SKIN PENETRATION POINTS-Continued

4 720 720B TURBOFAN ENGINES FORWARD 213.942 AFT ENGINE MOUNT ENGINE MOUNT MID SPAR LEFT SIDE OF ENGINE RIGHT SIDE OF ENGINE STRUT

COMMON POINT (LH & RH SIDE)

COWL SPLIT COWL SPLIT ENGINE

OUTBOARD NACELLE AND STRUT LEFT SIDE VIEW

FIRESEAL

720B TURBOFAN ENGINES 136.00 FORWARD 213.942 AFT ENGINE MOUNT ENGINE MOUNT MID SPAR

LEFT SIDE OF ENGINE T/C FAIRING STRUT RIGHT SIDE OF ENGINE

COMMON POINT (LH & RH SIDE)

COWL SPLIT ENGINE COWL SPLIT

OUTBOARD NACELLE AND STRUT LEFT SIDE VIEW

FIRESEAL 720. T.O. 00-105E-9 SPECIAL TOOLS/EQUIPMENT NOTE:

5 Power Rescue Saw Refer to the C-135 for more 720 24 Foot Ladder extensive information. Both PORTABLE OXYGEN 35 Foot Ladder airframes are identical except BOTTLES OR NEAR FLOOR LEVEL ON Fire Drill II cargo and tanker capabilities. PARTITIONS AIRCRAFT ENTRY 434 GALS (1643 LITERS) 1. NORMAL/EMERGENCY ENTRY HYDRAULIC ACCUMULATORS 2333 GALS (RIGHT WHEEL a. Overwing escape hatches both sides- (8831 LITERS) WELL AREA) Push red panel, located top center of hatches, in and push hatches inward. FIRE EXTINGUISHER 2283 GALS PASSENGER OXYGEN PORTS ON ENGINE (8642 SYSTEM BOTTLES IN AFT b. Pull handle, located left side forward and RIGHT COWLING LITERS) CARGO COMPARTMENT (TYPICAL EACH ENGINE) aft entry doors, outward and rotate clockwise. UTILITY & AUXILIARY RESERVOIR IN AFT CARGO COMPARTMENT CREW OXYGEN SYSTEM c. Pull handle, located forward and aft galley 2283 GALS BOTTLES IN FWD LOWERED 2333 GALS doors right side, outward and rotate counter- CEILING OR FWD CARGO AREA (8642 LITERS) (8831LITERS) 434 GALS clockwise. (1643 LITERS)

d. Press red handle, located on escape hatch top right forward crew compartment, and pull out. 7306 GALS (27,656 LITERS) 2. CUT-IN BATTERIES ENGINE OIL TANK-EACH PORTABLE OXYGEN BOTTLE ON ENGINE-RIGHT SIDE a. Cut along window lines as last resort. FORWARD SIDE OF BULKHEAD 1c AIRCRAFT CROSS SECTION NOTE: GALLEY DOOR 38” 1a 28” 28” Some series are equipped with class one EXTERNAL HANDLE PANEL escape hatches. 2a CUT-IN AREAS CAUTION

AFT ENTRY DOOR

GALLEY DOOR 1b GALLEY DOOR ENTRY DOOR (RIGHT SIDE ONLY) CUT-IN AREA EACH SIDE OF ACFT (RT SIDE ONLY) EXTERNAL HANDLE (NOT MARKED ON ALL ACFT) 720. T.O. 00-105E-9 ENGINE SHUTDOWN AND APPLICABILITY:

6 720 707-100/-200 AIRCREW EXTRACTION -300/-400 1. ENGINE SHUTDOWN 720 & 720B

a. Retard thrust levers, located on pilot’s center 1d console, to RETARD position. ENGINE START SWITCHES

b. Place engine start levers, located on pilot’s 1c center console, to CUT OFF position FIRE T-HANDLE c. Pull emergency fire T-handles, located top center above instrument panel.

2. AIRCREW EXTRACTION

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. 720. T.O. 00-105E-9 EMERGENCY RESCUE ACCESS

7 720

AFT GALLEY DOOR

OVERWING ESCAPE HATCHES

CHOP OUT AREAS (NOT MARKED ON ALL AIRCRAFT) AFT ENTRY DOOR

CHOP OUT AREAS (NOT FWD GALLEY DOOR MARKED ON ALL AIRCRAFT)

FWD ENTRY DOOR

FLIGHT DECK WINDOWS 6 FEET 1/2 INCH FLOOR LEVEL TO GROUND, WHEELS RETRACTED OPEN INTERNALLY 9 FEET 7INCH FLOOR LEVEL TO GROUND, WHEELS RETRACTED 720. T.O. 00-105E-9 CABIN CONFIGURATION TYPE III EMERGENCY EXIT GALLEY SERVICE 8 GALLEY SERVICE 720 EFFECTIVITY: 720, 720B (PASSENGER) DOOR 24X48” (LH & RH) 20X38” (51X96.5 CM) DOOR 24X48” (61X121.9 CM) C CLOSET (61X121.9 CM)

ES ESCAPE SLIDE L G G GL C L L G GALLEY S C

L LAVATORY MAIN ENTRY DOOR MAIN ENTRY DOOR S DOUBLE ATTENDANT’S 34X72” (86.4X183 CM) 30 PASSENGERS 101PASSENGERS 34X72” (86.4X183 CM) SEAT 4 A BREAST AT 38” 6 A BREAST AT 34” (96.5 CM) PITCH (86.4 CM) PITCH

131 PASSENGERS - MIXED CLASS (DOMESTIC)

CLASS DIVIDER

L G G G L C L L S S C

18 PASSENGERS 119 PASSENGERS 4 A BREAST AT 40” 6 A BREAST AT 34” (101.6 CM) PITCH (86.4 CM) PITCH

137 PASSENGERS - MIXED CLASS (INTERNATIONAL)

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

L G C G L L L S S C

* ADDITIONAL PAIR OF EXITS REQUIRED FOR THIS CONFIGURATION: 149 PASSENGERS MAXIMUM ALLOWABLE WITH TWO TYPE III EMERGENCY EXITS.

156* PASSENGERS - 6 A BREAST AT 34” (86.4 CM) 727.

T.O. 00-105E-9

1 AIRCRAFT PAINT SCHEME 727 727.

T.O. 00-105E-9 AIRCRAFT DIMENSIONS 727

727-100/-100C 727-200

HEIGHT 31’ 9” HEIGHT 31’ 7” (9.68 M) (9.61 M)

LENGTH 116’ 2” (35.41 M) LENGTH 136’ 2” (41.50 M)

WING SPAN 108’ (32.92 M) WING SPAN 108’ (32.92 M) 727.

T.O. 00-105E-9

3 AIRCRAFT SKIN PENETRATION POINTS 727

727-200 (NOT ALL -200’S)

10” 10” HANDLE

PENETRATION POINTS

PENETRATION POINTS FWD

FWD

WING TO BODY FAIRING

727-100 727-200 727-200

HANDLE 17” 10” 8” 18” HANDLE

PENETRATION POINTS HANDLE PENETRATION POINTS PENETRATION POINTS

FWD FWD FWD 727.

T.O. 00-105E-9 AIRCRAFT SKIN PENETRATION POINTS-Continued

4 727

LEFT SIDE OF ENGINE SKIN SPLICE 727-100/-200 CENTER ENGINE RIGHT SIDE OF ENGINE

SKIN SPLICE

COWL SPLIT AFT COWL PANEL COWL SPLIT FWD COWL AFT COWL PANEL 3.75 DIAMETER PANEL FWD COWL PANEL COWL VENT HOLE AT WL 209.60 AND BL 23.0 RIGHT SIDE VIEW LEFT SIDE VIEW USE FOR FIRE EXTINGUISHER ACCESS

COWL HINGE LINE

AFT MOUNT RING INLET

NACELLE ENGINE COWL SPLIT COWL SPLIT

FWD MOUNT RING

LEFT SIDE VIEW 727-100/-200 SIDE ENGINE 3.75 DIAMETER COWL UP VENT HOLE AT NAC BL 0 USE FOR FIRE FWD EXTINGUISHER ACCESS 727.

T.O. 00-105E-9 AIRCRAFT DANGER AREAS

5 727 JT8D TURBOFAN ENGINE HAZARD AREAS AT IDLE THRUST

FEET AXIAL DISTANCE BEHIND AIRCRAFT 0 30 60 90 120 150

0 10 20 30 40

METERS INTAKE DANGER AREAS

F M 100 MPH 50 MPH 30 10 18 FEET (161 KMPH) (80 KMPH) 20 5 10 0 0 10 5 20 0 0 200 F 100 F 18 FEET 0 30 (93 0 C) (38 C) 10 INTAKE DANGER AREAS DISTANCE FROM AIRCRAFT CENTERLINE

4 FEET

NOSE COWL FORWARD EDGE 727.

T.O. 00-105E-9 AIRCRAFT DANGER AREAS-Continued 6 727 JT8D TURBOFAN ENGINE HAZARD AREAS AT TAKEOFF THRUST AXIAL DISTANCE BEHIND AIRCRAFT FEET 0 50 100 150 200 250 300

0 10 20 30 40 50 60 70 80 90 100 METERS

50 MPH (80 KMPH) F 100 MPH (TO 512 FT M 150 MPH (161 KMPH) 157M) 400 MPH 300 MPH 200 MPH 10 (644 KMPH) (483 KMPH)(322 KMPH) (240 KMPH) 30

25 FEET 20 5 10

0 0

10 5 INTAKE 20 DANGER AREAS 30 0 0 10 0 25 FEET 0 100 F (38 C) 300 0 F 200 F 150 F DISTANCE FROM 0 0 (149 0 C) (93 C) (65 C) AIRCRAFT CENTERLINE 727.

T.O. 00-105E-9 AIRCRAFT COMPOSITE LOCATIONS 727

7 COMPOSITE LOCATIONS

FIN TIP FAIRING

RAIN GUTTER

WING TO BODY FAIRING

RADOME

LEADING EDGE ACCESS PANELS 727.

T.O. 00-105E-9 US MARSHALS SERVICE 727 VERSION

8 727 1. 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 wing which face aft. A large center aisle between the seats goes from one side to the other side where the emergency exit is over the wings.

2. PRISONER TRANSPORTATION The U.S. Marshals Service assumes custody of individuals arrested by In 1995, the air fleets of the Marshals Service and the Immigration and all federal agencies and is responsible for the housing and transportation Naturalization Service (INS) merged to create the Justice Prisoner and of prisoners from the time they are brought into federal custody until Alien Transportation System (JPATS). The merger created a more they are either acquitted or incarcerated. efficient and effective system for transporting prisoners and criminal aliens. Operated by the Marshals Service, JPATS is one of the largest Moving thousands of prisoners and criminal aliens each year requires transporters of prisoners in the world, handling hundreds of requests extra security precautions and careful coordination. Deputy Marshals, every day to move prisoners between judicial districts, correctional Aviation Enforcement Officers and Aviation Safety Officers are stationed institutions and foreign countries. throughout the aircraft, and prisoners wear handcuffs and leg irons in the close confines of the aircraft cabin. On average, more than 200,000 prisoner and alien movements a year are completed by the Marshals Service via coordinated air and ground Ground security is provided by Deputy Marshals, BOP guards or INS systems. Most of these prisoners are transported aboard Service-owned officers at each airport transfer point. If prisoners cannot be moved in aircraft and vehicles. one day, they are housed overnight at various BOP facilities. Careful scheduling is required to ensure that each prisoner appears in court at Since 1984, the Marshals Service has acquired a fleet of aircraft that the designated time. includes three Boeing 727s, a DC-9, several smaller jets and turboprop airplanes. These planes move thousands of prisoners for the Marshals In an effort to assist state and local law enforcement agencies, the Service, Bureau of Prisons (BOP) and INS, as well as the U.S. military Marshals Service transports non-federal prisoners between different and state and local governments. Many of the airplanes were acquired at jurisdictions when space is available on its aircraft. no cost through the Government Surplus Property Program and the Asset Seizure and Forfeiture Program. For example, a fugitive wanted for trial in one locale may have been apprehended in another, distant jurisdiction. However, local authorities The JPATS is the only government-operated, scheduled passenger are often reluctant to seek extradition of felons because of high transpor- airline in the nation. It serves 40 cities, and is used to move prisoners tation and personnel costs. The Marshals Service offers state and local more economically and with higher security than commercial airlines. law enforcement agencies a safe and effective prisoner transportation system at about one-quarter of the normal cost. 727.

T.O. 00-105E-9 SPECIAL TOOLS/EQUIPMENT NOTE: AFT CARGO FUEL TANKS (OPTIONAL)

9 Power Rescue Saw Refer to the C-22 for more FWD CARGO FUEL TANKS (OPTIONAL) 860 US GALS (FWD) 3255 LITERS 727 810 US GALS (EACH CELL) 24 Foot Ladder extensive information. Both 2 1070 US GALS (AFT) 3066 LITERS 4050 LITERS Fire Drill II airframes are identical except 1 AIRCRAFT ENTRY for military configurations.

1. NORMAL ENTRY

WARNING HYD RESERVOIR (AIRSTAIR FUEL LINES PASSAGE) If Forward Entry Door is used for rescue, passenger escape VENT SURGE TANK PORTABLE chute-slide will be actuated if not disconnected from inside. OXYGEN APU BOTTLE 1793 GALS (WHEEL a. RIGHT FORWARD ENTRY DOOR - Pull handle outward, HYD ACCUMULATOR 6787 LITERS WELL) rotate clockwise and pull door outward to open position. (AIRSTAIR PASSAGE) FIRE EXT PORT 2 2. EMERGENCY ENTRY (OUTBD ENG) PORTABLE OXYGEN BOTTLES ENG OIL TANK (TYPICAL) a. PILOT’S SLIDING WINDOW - (RH & LH) Cargo and (RH only OXYGEN BOTTLES PASSENGER HYD ACCUMULATOR (WHEEL WELL) passenger aircraft. AND CREW APU EMER CONTROL PANEL b. OVERWING ESCAPE HATCHES - Push panel in, located (LEFT WHEEL WELL AREA) top center of hatches, and push hatches inward and up. MAIN BATTERY 1 c. FORWARD ENTRY DOOR - Pull external handle, located on entry door, outward, rotate clockwise and pull door out ACCESS 4004 GALS DOOR 15,155 LITERS 1793 GALS VENT SURGE TANK to open position. 6787 LITERS PORTABLE OXYGEN 38” 28” AIRCRAFT d. MID GALLEY DOOR - Pull external handle, located on galley 2e 28” BOTTLES CROSS- DOOR door right forward side, outward, rotate counterclockwise and SECTION pull door out to open position. HANDLE 2a 1a, 2c e. AFT EXIT DOORS - Pull lower end of handle, located top PILOT’S CUT-IN EXTERNAL AREAS center of door left side of fuselage, outward, rotate clockwise SLIDING HANDLE WINDOW and pull door outward. (Turn handle counterclockwise on doors 2d 2e located on right side of fuselage.) MID GALLEY DOOR AFT EXIT DOOR 2g (RT SIDE ONLY) f. AIRSTAIR ENTRY DOOR - Depress latch on access door, AFT ENTRY 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.) 2f g. AFT ENTRY DOOR - Rotate handle, located on aft entry door, 2c FWD ENTRY DOOR 3a 2b AFT AIRSTAIR clockwise and push door inward. CUT-IN EMERGENCY OVERWING ESCAPE HATCHES 2b 3. CUT-IN PANEL a. Cut tenth window aft from crew compartment and fifth window HYDRAULIC forward from tail section as last resort. HANDPUMP 2d 2f NOTE: EXTERNAL AIRSTAIR DOOR HANDLE RELEASE HANDLE Oxygen, rafts, flashlights, and fire extinguishers are located in overhead compartments. 727.

T.O. 00-105E-9

10 ENGINE SHUTDOWN AND 727 AIRCREW EXTRACTION 1. ENGINE SHUTDOWN 1c ENGINE FIRE T-HANDLES 1c a. Retard thrust levers, located on pilot’s center ENGINE FIRE T-HANDLES console, to RETARD position.

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. 1d NOTE: APU FIRE Optional location for T-handles is on the SWITCH pilot’s light shield. 1a d. In case of APU fire, pull APU fire switch to THRUST OFF and place APU master switch to OFF, LEVERS located on rear cockpit wall. 1d e. Lift guard and place battery switch, located on APU lower center flight engineer’s upper left panel, MASTER to OFF position. SWITCH

2. AIRCREW EXTRACTION

a. Unlatch lap belt and remove shoulder harness 1b from crewmembers ENGINE START b. FLIGHT ENGINEER’S SEAT - Depress seat LEVERS control handles and rotate seat clockwise.

c. PASSENGER’S SEATS - Passengers seats are equipped with lap belts only. BULKHEAD RIGHT OF FLIGHT ENGINEER’S NOTE: PANEL If seat tracks are not damaged during crash landing use adjustable seat control handles to retract seats to aft position. 727.

T.O. 00-105E-9

11 EMERGENCY RESCUE ACCESS 727

AFT ENTRY DOOR (OPENS FROM INSIDE OF THE AFT STAIRS AREA) (AIRSTAIR “CHOP OUT” AREAS MUST FIRST BE LOWERED)

AFT AIRSTAIR EXTERIOR CONTROL PANEL OPERATING OVERWING ESCAPE HATCHES INSTRUCTIONS ON ACCESS PANEL

“CHOP OUT” AREA AFT AIRSTAIR

GALLEY DOOR AFT EXIT DOORS (MOVED FWD ON 200, (REMOVED ON 100 AND 200F) REMOVED ON 200F)

FWD ENTRY DOOR OVERWING ESCAPE HATCHES

“CHOP OUT” AREA PILOT’S SLIDING WINDOW 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) 727.

T.O. 00-105E-9

12 CABIN CONFIGURATION 727 EFFECTIVITY: 727-100/-100C (PASSENGER) TYPE 1 GALLEY SERVICE C CLOSET DOOR 33X65” (84X165 CM) AFT ENTRY DOOR 32X76 “ (81X193 CM) ES ESCAPE SLIDE STOWAGE G GALLEY

L LAVATORY C G G L L S DOUBLE ATTENDANT’S SEAT C L

WINDSCREEN FWD ENTRY DOOR TYPE IV EXIT(RH & LH) 34X72 “ (97X183 CM) TYPE III EMERGENCY 20X38 “ (51X97 CM) EXIT (RH & LH) 16 PASSENGERS 20X38 “ (51X97 CM) 90 PASSENGERS 4 ABREAST AT 38” 3 ABREAST AT 33” (97 CM) PITCH (84 CM) PITCH

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

34” (86 CM) TYPICAL STOWAGE

ES G G L L S S ES L

126 PASSENGERS - ALL TOURIST (MAXIMUM CERTIFICATED CAPACITY - 129 PASSENGERS) 727.

T.O. 00-105E-9

13 CABIN CONFIGURATION-Continued 727 EFFECTIVITY: 727-100C (PASSENGER/CARGO) TYPE 1 EMERGENCY EXIT GALLEY SERVICE SMOKE (RH & LH) ES ESCAPE SLIDE DOOR 33X65” TYPE III TYPE IV BARRIER 20X38 “ (84X165 CM) (51X97 CM) G GALLEY

ES L LAVATORY G G L 88X108” PALLETS L S DOUBLE ATTENDANT’S (122X274 CM) S SEAT ES L

CARGO DOOR FWD ENTRY DOOR AFT ENTRY DOOR 86X34 “ (218X340 CM) SMOKE-TIGHT PARTITION 34X72 “ (97X183 CM) 32X76 “ (81X193 CM) 70 PASSENGERS

L 88X108” PALLETS L (122X274 CM) S L ES G

CARGO DOOR CONTROL PANEL 56 PASSENGERS

L L 88X108” PALLETS (122X274 CM) S L ES G

52 PASSENGERS 727.

T.O. 00-105E-9

14 CABIN CONFIGURATION-Continued 727 EFFECTIVITY: 727-100C (ALL CARGO)

L LAVATORY

CONDITIONS L L HATRACKS UP 1 2 3 4 5 6 7 8 2” CLEARANCE L

9 g COMMERCIAL PALLETS

HIGH-PROFILE ROLLERS CARGO DOOR PALLET VOLUME NOT INCLUDED 86X34 “ (218X340 CM) IN CARGO VOLUME

CARGO ENVELOPE VOLUMES IN CUBIC FEET (CUBIT METERS)

PALLET SIZE 88X108" 88X125" (223X274 CM) (223X318 CM)

MAIN DECK

PALLET 1 359 (10.17) 401 (11.36)

PALLETS 2-8 366 (10.4) EACH APPROX. 2,562 (72.56) 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) 727.

T.O. 00-105E-9

15 CABIN CONFIGURATION-Continued 727 EFFECTIVITY: 727-200 (PASSENGER) TYPE 1 AFT ENTRY DOOR GALLEY SERVICE 32X76 “ (81X193 CM) C CLOSET DOOR 33X65” CLASS (84X165 CM) ES ESCAPE SLIDE DIVIDER STOWAGE (RH & LH) G GALLEY

L LAVATORY

S DOUBLE ATTENDANT’S SEAT 38” (97 CM) 34” (86 CM) TYPE 1 TYPICAL TYPICAL SERVICE DOOR TYPE III EMERGENCY (RH & LH) EXIT (RH & LH) 30X60” (76X152 CM) 20X38 “ (51X97 CM) WIND FWD ENTRY DOOR SCREEN 34X72 “ (97X183 CM)

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

34” (86 CM) TYPICAL ES G ES G L L S S L ES ES G

WIND SCREEN

155 PASSENGERS - TYPICAL ALL-TOURIST (MAXIMUM CERTIFICATED CAPACITY - 189 PASSENGERS) 737. T.O. 00-105E-9 NEXT GENERATION 737-600/-700/-800/-900 1 AIRCRAFT PAINT SCHEME 737 737. T.O. 00-105E-9

2 AIRCRAFT DIMENSIONS 737 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.

67’ 9” (20.65m) 72’ 2” (22.00m) 62’ 9” (19.13m) 67’ 2” (20.47m)

102’ 6” (21.24m) 110’ 4” (33.63m)

29’ 6” (8.84m) 34’ 0” (10.36m)

15’ 10” 15’ 10” (4.83m) (4.83m)

12’ 4” 12’ 4” (3.76m) (3.76m)

97’ 9” 105’ 7” (29.79m) (32.18m)

41’ 3” 41’ 3” (12.57m) (12.57m)

36’ 10” (11.23m) 41’ 4” (12.60m) 13’ 5” (4.09m) 13’ 5” (4.09m) 112’ 7” 112’ 7” (34.32m) (34.32m) 47’ 1” 47’ 1” (14.35m) (14.35m)

APPROX 8’ APPROX 8’ SCALE 18’ 9” SCALE (2.44 m) 18’ 9” METERS 0 2 4 6 (2.44 m) METERS 0 2 4 6 (5.72m) (5.72m) FEET 0 5 10 15 20 25 FEET 0 5 10 15 20 25

737-600 737-700 (737-100/-200/-300/-400/-500 prior to engine and aircraft upgrades.) 737. T.O. 00-105E-9

3 AIRCRAFT DIMENSIONS-Continued 737

82’ 0” (24.99m) 87’ 2” (26.57m) 77’ 0” (23.47m) 82’ 2” (25.05m)

129’ 6” (39.47m) 138’ 2” (41.11m) 43’ 10” 48’ 4” (13.36m) (14.73m)

15’ 10” 15’ 10” (4.83m) (4.83m)

12’ 4” 12’ 4” (3.76m) (3.76m)

124’ 9” (38.02m) 133’ 5” (40.67m)

41’ 3” (12.57m) 51’ 2” (15.60m) 41’ 3” 56’ 4” (17.17m) 13’ 5” (4.09m) (12.57m) 13’ 5” (4.09m) 112’ 7” 112’ 7” (34.32m) (34.32m) 47’ 1” 47’ 1” (14.35m) (14.35m)

APPROX 8’ SCALE APPROX 8’ 18’ 9” SCALE (2.44 m) 18’ 9” METERS 0 2 4 6 (2.44 m) (5.72m) (5.72m) METERS 0 2 4 6 FEET 0 5 10 15 20 25 FEET 0 5 10 15 20 25

737-800 737-900 737. T.O. 00-105E-9 AIRCRAFT DIMENSIONS-Continued 737

110’ 4” (33.63m) 129’ 6” (39.47m)

34’ 0” 43’ 10” (10.36m) (13.36m) 15’ 10” 15’ 10” (4.83m) (4.83m)

12’ 4” 12’ 4” (3.76m) (3.76m)

105’ 7” (32.18m) 124’ 9” (38.02m) 75’ 6” (23.01m) 41’ 3” 85’ 4” (26.01m) (12.57m)

41’ 4” (12.60m) 51’ 2” (15.60m) 41’ 2” (12.55m) 13’ 5” (4.09m) 13’ 5” (4.09m) 117’ 5”(35.79m) 117’ 5”(35.79m) 47’ 1” 47’ 1” (14.35m) (14.35m)

SCALE SCALE APPROX 8’ (2.44m) METERS 0 2 4 6 APPROX 8’ (2.44 m) METERS 0 2 4 6 18’ 9” (5.72m) FEET 0 5 10 15 20 25 18’ 9” (5.72m) FEET 0 5 10 15 20 25

737-700 WITH WINGLETS 737-800 WITH WINGLETS 737. T.O. 00-105E-9 AIRCRAFT DIMENSIONS-Continued 737

138’ 2” (42.11m)

48’ 4” (14.73m)

15’ 10” (4.83m)

12’ 4” (3.76m)

133’ 5” (40.67m) 90’ 6” (27.58m)

56’ 4” (17.17m) 41’ 2” 13’ 5” (4.09m) (12.55m)

117’ 5” (35.79m) 47’ 1” (14.35m)

SCALE APPROX 8’ (2.44 m) METERS 0 2 4 6 (5.72m) 18’ 9” FEET 0 5 10 15 20 25

737-900 WITH WINGLETS 737. T.O. 00-105E-9

6 AIRCRAFT SKIN PENETRATION POINTS 737 NOTE: Typical penetration areas for all models.

5” PENETRATION 5” PENETRATION POINTS POINTS

C L CL 8” 8”

HANDLE HANDLE

FWD FWD 737. T.O. 00-105E-9 AIRCRAFT SKIN PENETRATION POINTS-Continued 7 737 737-100/-200

CL FRONT MOUNT CL FRONT MOUNT C AFT MOUNT FORWARD FAIRING L CL AFT MOUNT FORWARD FAIRING AFT STRUT FAIRINGS THRUST PENETRATION POINT REVERSERS PENETRATION POINT C CL NACELLE L NACELLE

NOSE COWL SIDE COWL SIDE COWL NOSE COWL

3.75” DIAMETER COWL VENT 3.75” DIAMETER COWL VENT OUTBOARD INBOARD HOLE AT NAC BL 0.0 USE FOR HOLE AT NAC BL 0.0 USE FOR ENGINE NACELLE ENGINE NACELLE FIRE EXTINGUISHER ACCESS FIRE EXTINGUISHER ACCESS

737-300/-400/-500/-600/-700/-800/-900 PENETRATION PENETRATION POINT POINT THRUST REVERSER COWL WING FAN COWL WING FAN COWL

NACELLE CL CL NACELLE 0.6” WIDE ANNULAR VENT - USE FOR 0.6” WIDE ANNULAR OIL TANK FIRE EXTINGUISHER VENT - USE FOR FILLER DOOR ACCESS TO ENGINE FIRE EXTINGUISHER C L CORE ACCESS TO ENGINE THRUST CL 2.5” X 9.0” COWL VENT AT BL0 2.5” X 9.0” COWL VENT AT BL0 CORE REVERSER USE FOR FIRE EXTINGUISHER USE FOR FIRE EXTINGUISHER COWL ACCESS TO FAN COMPARTMENT ACCESS TO FAN COMPARTMENT

ENGINE NACELLE ENGINE NACELLE LEFT SIDE VIEW RIGHT SIDE VIEW 737. T.O. 00-105E-9 AIRFRAME MATERIALS

8 737 GRAPHITE COMPOSITES EFFECTIVITY: -100/-200/-300/-400/-500

HORIZONTAL STABILIZER VERTICAL TRAILING STABILIZER TIP EDGE NOSE LANDING RUDDER GEAR TAILCONE ASSEMBLY DOORS UPPER UPPER WING LOWER WING FIXED ELEVATOR TAB WING FIXED TRAILING LEADING EDGE PANELS STRUCTURE FIXED EDGE PANELS LEADING EDGE PANELS LOWER WING WING TO FIXED TRAILING BODY NACELLE EDGE PANELS FAIRING STRUT FAIRING WING TRAILING EDGE MAIN FLAP ASSEMBLY SPOILERS AILERONS/ TABSKIN MAIN LANDING AND STRUCTURE GEAR DOORS AND FAIRINGS FLAP TRACK FAIRINGS ENGINE COWL RADOME 737. T.O. 00-105E-9 AIRFRAME MATERIALS-Continued

9 737 GRAPHITE OR FIBERGLASS GRAPHITE COMPOSITES EFFECTIVITY: -600/-700/-800/-900

VERTICAL WINGLETS VERTICAL STABILIZER (AS INSTALLED) STABILIZER TIP TRAILING EDGE UPPER WING UPPER WING RUDDER LOWER WING FIXED FIXED FIXED TRAILING LEADING EDGE PANELS LEADING EDGE PANELS TAILCONE EDGE ASSEMBLY PANELS

LOWER WING DORSAL ELEVATOR FIXED TRAILING NACELLE FIN SKIN UPPER & EDGE PANELS NOSE STRUT LOWER SKIN LANDING FAIRING WING TRAILING EDGE GEAR MAIN FLAP ASSEMBLY DOORS

WINGLETS (AS INSTALLED) FLAP TRACK THRUST AILERONS/TAB SKIN FAIRINGS REVERSER AND STRUCTURE

RADOME 737. T.O. 00-105E-9 AIRFRAME MATERIALS-Continued

10 737 GRAPHITE OR FIBERGLASS GRAPHITE COMPOSITES EFFECTIVITY: BOEING BUSINESS JET (BBJ)/BBJ-2

VERTICAL WINGLETS VERTICAL STABILIZER TIP (AS INSTALLED) STABILIZER TRAILING RUDDER EDGE TAILCONE UPPER UPPER WING ASSEMBLY LOWER WING FIXED WING FIXED TRAILING LEADING EDGE PANELS FIXED ELEVATOR TAB EDGE PANELS LEADING STRUCTURE EDGE PANELS

LOWER WING DORSAL ELEVATOR FIXED TRAILING FIN SKIN NOSE UPPER & EDGE PANELS NACELLE LANDING LOWER SKIN STRUT GEAR FAIRING WING TRAILING EDGE DOORS MAIN FLAP ASSEMBLY

WINGLETS (AS INSTALLED) FLAP TRACK AILERONS/TAB SKIN FAIRINGS THRUST AND STRUCTURE REVERSER RADOME 737. T.O. 00-105E-9

11 AUXILIARY FUEL TANK CAPACITIES 737 NOTE: This information includes Boeing Business Jets.

AUX FUEL GALLONS LITERS TOTAL TOTAL GALLONS LITERS (ALL TANKS) (ALL TANKS)

3 AFT 3 AFT 1,485 5,685 8,360 31,710 5 AFT/4 FWD 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

5 AFT/3 FWD

3 AFT/1 FWD

5 AFT/2 FWD 4 AFT 3 AFT/2 FWD 4 AFT/2 FWD 737. T.O. 00-105E-9 SPECIAL TOOLS/EQUIPMENT NOTE: OPTIONAL AUX FUEL

12 737 Power Rescue Saw Refer to the T-43 for more 1 TANK IN LWR AFT 12 Foot Ladder extensive information. Both CARGO COMPT Fire Drill II airframes are identical except 390/492/984 GALLONS AIRCRAFT ENTRY-100/-200/-300/-400/-500 SERIES for military trainer capabilities. 1476/1862/3725 LITERS

1. NORMAL/EMERGENCY ENTRY VENT SURGE TANK a. Push in top center panel on overwing escape hatches, located on both fuselage sides. Push SYSTEM A, B & STANDBY 1288 GALLONS hatch inward and upward. HYD RESERVOIRS IN APU OIL TANK 4876 LITERS WHEEL WELL PORTABLE OXYGEN BOTTLES NOTE: (VARIEDLOCATIONS) Some models are equipped with stairs that can 1 APU FUEL LINES be deployed from forward and aft entry doors. CREW OXYGEN BOTTLE (FWD CARGO AREA) APU EMER CONTROL PANEL (RT W W) HYD BRAKE ACCUMULATORS (IN W W) b. Pull handle on forward and aft entry doors, located PASSENGER left side of fuselage, outward and rotate clock- OXYGEN 1288 GALLONS 4876 LITERS wise. Pull doors outward. (OPTIONAL) VENT SURGE TANK PORTABLE NOTE: 4299 OXYGEN ENGINE OIL TANK (ONE EACH ENGINE) Depress button and pull handle out, rotate GALS BOTTLE RT SIDE CFM-56 LT SIDE ALL OTHERS clockwise to extend stairway. (BEHIND 16,273 CO-PILOT) LITERS 1a c. Pull handle on right forward and aft service doors, EMERGENCY OVERWING EXIT HATCHES outward and rotate counterclockwise. Pull doors PUSH PANEL (BOTH SIDES) outward. 1c FWD AND AFT SERVICE DOOR CAUTION EXTERNAL HANDLE (RT SIDE)

When doors are opened from outside, chutes automatically deploy.

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

-100/-200 BATTERIES AFT ENTRY FWD ENTRY DOOR DOOR

1b -300/-400 FWD AND AFT ENTRY MAIN &-500 DOOR EXTERNAL E/E E/E DOOR HANDLE (LT SIDE) COMPARTMENT ACCESS DOOR -300 (OPTIONAL 737. T.O. 00-105E-9

13 EMERGENCY RESCUE ACCESS 737 EFFECTIVITY:-100/-200/-300/-400/-500 SERIES

2” WIDE BAND OF CONTRASTING COLOR INDICATING ALL DOORS, HATCHES AND WINDOWS EXTERNALLY OPERABLE

AFT SERVICE DOOR

CARGO DOOR (RT SIDE) OPERATING INSTRUCTIONS ON DOOR

AFT ENTRY DOOR OVERWING ESCAPE HATCHES

CUT IN OR CHOP OUT AREAS ADDITIONAL OVERWING ESCAPE HATCHES ( -400 ONLY) CUT IN OR CHOP OUT AREAS CARGO DOOR (RT SIDE) OPERATING INSTRUCTIONS ON DOOR FWD SERVICE DOOR

CARGO DOOR -200C CUT-IN OR CHOP OUT AREAS LOCATED BETWEEN PILOT’S SLIDING WING FRONT SPAR AND ESCAPE HATCH (THREE WINDOW BAYS) BELOW WINDOWS AND ABOVE FLOORS AVERAGE DISTANCE - FLOOR LEVEL TO GROUND FWD ENTRY DOOR WHEELS RETRACTED: 5 FT WHEELS EXTENDED: 8 FT. 6 IN. 737. T.O. 00-105E-9 AIRCRAFT ENTRY-Continued 14 AUXILIARY 737 AIRCRAFT ENTRY -600/-700/-800 SERIES FUEL TANK 1. NORMAL ENTRY LOCATIONS WINGLETS (AS INSTALLED) (BBJ ONLY) NOTE: Some models are equipped with stairs that can VENT SURGE TANK APU OIL TANK be deployed from forward and aft entry doors. SYSTEM A, B & STANDBY HYD RESERVOIRS IN 1288 GALLONS a. Pull handle on forward and aft entry doors, WHEEL WELL located left side of fuselage, outward and 4876 LITERS PORTABLE OXYGEN BOTTLES rotate clockwise. Pull doors outward. (VARIEDLOCATIONS) CREW OXYGEN APU FUEL LINE NOTE: BOTTLE (FWD APU EMER CONTROL PANEL (RT W W) Depress button and pull handle out, rotate CARGO AREA) clockwise to extend stairway. HYD BRAKE ACCUMULATORS (IN W W)

1288 GALLONS 4876 LITERS b. Pull handle on right forward and aft service PORTABLE doors, outward and rotate counterclockwise. OXYGEN WINGLETS Pull doors outward. BOTTLE (AS INSTALLED) (BEHIND 4299 GALS c. The pilot’s sliding window can be accessed by CO-PILOT) 16,273 LITERS pulling the external handle and sliding window ENGINE OIL TANK RT SIDE EACH ENGINE open. 1b CAUTION FWD AND AFT SERVICE DOOR EXTERNAL HANDLE (LT SIDE) When doors are opened from outside, chutes automatically deploy. 2a 1c EMERGENCY OVERWING EXIT HATCHES PILOT (BOTH SIDES) (See also page 737.11) WINDOW

BATTERY

AFT ENTRY FWD ENTRY DOOR DOOR -600/-700/-800 1a E/E COMPARTMENT ACCESSIBLE FROM FWD FWD AND AFT ENTRY DOOR ACCESS DOOR CARGO COMPARTMENT EXTERNAL HANDLE (RT SIDE) 737. T.O. 00-105E-9

15 AIRCRAFT ENTRY-Continued 737 2. EMERGENCY ENTRY a. Push in top center on overwing escape hatches, located on both fuselage sides (see page 737.16 for hatch locations.)

3. CARGO DOOR OPERATION a. To open cargo door 1, unlock the external door 2a handle. EMERGENCY OVERWING EXIT HATCHES (BOTH SIDES) b. Verify unlocked light in ON.

c. Hold the UP TO CANOPY switch (illustrated in red) in UP position until door motion stops. 3a 4. CUT-IN OR CHOP OUT AREAS EXTERNAL CARGO a. Cut-in or chop out areas are located between wing DOOR CONTROLS front spar and escape hatch (three bays) below windows and above floors. (see page 737.11)

3b CARGO DOOR LIGHTS 3c UP TO CANOPY SWITCH

4a CUT-IN AREAS 737. T.O. 00-105E-9

16 EMERGENCY RESCUE ACCESS 737 EFFECTIVITY:-600/-700/-800 SERIES

2” WIDE BAND OF CONTRASTING COLOR INDICATING ALL DOORS, HATCHES AND WINDOWS EXTERNALLY OPERABLE

AFT SERVICE DOOR

OVERWING ESCAPE HATCHES CARGO DOOR (RT SIDE) OPERATING INSTRUCTIONS ON DOOR ADDITIONAL OVERWING ESCAPE HATCHES (-800/-900 ONLY)

AFT ENTRY DOOR CUT IN OR CHOP OUT AREAS CARGO DOOR (RT SIDE) OPERATING INSTRUCTIONS CUT IN OR CHOP OUT AREAS ON DOOR

FWD SERVICE DOOR

CARGO DOOR -700C PILOT’S CUT IN OR CHOP OUT AREAS LOCATED SLIDING AVERAGE DISTANCE - BETWEEN WING FRONT SPAR AND WINDOW FLOOR LEVEL TO GROUND ESCAPE HATCH (THREE BAYS) BELOW FWD ENTRY DOOR WHEELS RETRACTED: 5 FT WINDOWS AND ABOVE FLOORS WHEELS EXTENDED: 8 FT. 6 IN. 737. T.O. 00-105E-9

17 ENGINE SHUTDOWN AND 737 AIRCREW EXTRACTION 1. ENGINE SHUTDOWN (-100 thru -800 & BBJ)

a. Retard thrust levers, located on pilot’s center console, to RETARD position. OR b. Retard engine start levers, located on pilot’s console, to CUT OFF position. 1f c. In case of engine fire, pull appropriate engine BATTERY fire T-handles, located on center console 1e SWITCH forward of thrust levers. Turn right or left to APU MASTER SWITCH discharge agent. If not illuminated, push and hold the button under the switch to release. 1a d. In case of APU fire, pull the APU fire T-handle, THRUST located on center console forward of thrust levers. LEVERS Turn right or left to discharge agent.

e. Place APU master switch up to OFF position 1d OR OFF position. (Switch type can vary.) APU FIRE SWITCH f. Lift guard and place battery switch, located on pilot’s center overhead panel, to OFF position.

2. AIRCREW EXTRACTION

a. Unlatch lap belt and remove shoulder harness from crewmembers. See page T-43.5 for view 1b of seats and associated controls. ENGINE START LEVERS

b. FLIGHT ENGINEER’S SEAT - Depress seat 1c control handles and rotate seat clockwise. ENGINE FIRE T-HANDLES

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. 737. T.O. 00-105E-9 CABIN CONFIGURATIONS 18 737 EFFECTIVITY: -100/-200/-300/-400/-500/-600 (NO WINGLETS) (SEE SEPARATE FILES FOR T-43 AND C-40A/B/C)

MIXED CLASS 8 FIRST CLASS SEATS AT 36 - IN PITCH 120 ECONOMY CLASS SEATS AT 32 - PITCH

MIXED CLASS 90 BUSINESS CLASS SEATS AT 34 - IN PITCH 36 ECONOMY CLASS SEATS AT 32 - PITCH

SINGLE CLASS 140 ECONOMY CLASS SEATS AT 32 - IN PITCH (SHOWN) OR 148 ECONOMY CLASS SEATS AT 30 - PITCH

[A] ATTENDANT [C] CLOSET [G] GALLEY [L] LAVATORY [S] STORAGE 737. T.O. 00-105E-9

19 CABIN CONFIGURATIONS-Continued 737 EFFECTIVITY: -700 (WITH OR WITHOUT WINGLETS)

MIXED CLASS 8 FIRST CLASS SEATS AT 36 - IN PITCH 120 ECONOMY CLASS SEATS AT 32 - PITCH

MIXED CLASS 90 BUSINESS CLASS SEATS AT 34 - IN PITCH 36 ECONOMY CLASS SEATS AT 32 - PITCH

SINGLE CLASS 140 ECONOMY CLASS SEATS AT 32 - IN PITCH (SHOWN) OR 148 ECONOMY CLASS SEATS AT 30 - PITCH

[A] ATTENDANT [C] CLOSET [G] GALLEY [L] LAVATORY [S] STORAGE 737. T.O. 00-105E-9

20 CABIN CONFIGURATIONS-Continued 737 EFFECTIVITY: -800 (WITH OR WITHOUT WINGLETS)

MIXED CLASS 8 FIRST CLASS SEATS AT 36 - IN PITCH 120 ECONOMY CLASS SEATS AT 32 - PITCH

MIXED CLASS 90 BUSINESS CLASS SEATS AT 34 - IN PITCH 36 ECONOMY CLASS SEATS AT 32 - PITCH

SINGLE CLASS 140 ECONOMY CLASS SEATS AT 32 - IN PITCH (SHOWN) OR 148 ECONOMY CLASS SEATS AT 30 - PITCH

[A] ATTENDANT [C] CLOSET [G] GALLEY [L] LAVATORY [S] STORAGE 737. T.O. 00-105E-9 CABIN CONFIGURATIONS-Continued

21 737 EFFECTIVITY: -900 (WITH OR WITHOUT WINGLETS)

MIXED CLASS 12 FIRST CLASS SEATS AT 36 - IN PITCH 165 ECONOMY CLASS SEATS AT 32 - PITCH

SINGLE CLASS 177 ECONOMY CLASS SEATS AT 32 - IN PITCH OR 189 ECONOMY CLASS SEATS AT 31 - PITCH

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