WELCOME TO TECHNICAL ORDER 00-105E-9, 1 FEBRUARY 2006 ... Segment 18.pdf · mishap response...

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IN THIS SEGMENT.

THIS IS SEGMENT 18 COVERING CHAPTER 18 TO THE DC-10.

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 Retaining out of date rescue information can negatively affect the user’s operability and outcome of emergencies.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 18 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

T.O. 00-105E-9

18-1. INTRODUCTION AND USE.

18-2. This section contains emergency rescue andmishap response information illustrations in alpha-numerical order relative to type and model of aircraft.This arrangement of illustrations is maintained fromChapter 4 throughout the remainder of the publica-tion.

18-3. GENERAL ARRANGEMENT.

18-4. Aircraft type designation has been positionedin the upper right corner of the horizontal illustrationfor rapid identification. Additional aids to rapid orien-tation are:

a. Recent technological advances in avia-tion have caused concern for the modern firefighter.Aircraft hazards, cabin configurations, airframe ma-terials, and any other information that would be help-ful in fighting fires, the locating and rescue of per-sonnel will be added as the information becomes avail-able.

b. Suggested special tools/equipment arelisted in the upper left corner, on the Aircraft/Entrypage of each listed aircraft.

c. Procedural steps covering emergency/normal entrances, cut-ins, engine/APU shutdown,safetying ejection/escape systems, and aircrew ex-traction are outlined on the left side of each page withcoordinated illustrations on the right.

d. Illustrations located on right side of pagesare coordinated with text by numerals and small let-ters depicting both paragraph and subparagraph onthe page.

e. Each illustration is consistently coloredand/or pattern keyed to highlight essential emergencyrescue information.

f. Details are pulled directly from the illustra-tion to highlight an area, thus eliminating unneces-sary searching for desired information.

CHAPTER 18

COMMERCIAL/CIVIL RESERVE AIRFLEET(CRAF)

AEROSPACE EMERGENCY RESCUEAND MISHAP RESPONSE INFORMATION

18-1

18-5. CIVIL RESERVE AIR FLEET (CRAF)

Major US carriers represented in CRAF are man-aged by AMC, Scott AFB, IL in the Civil Air Director-ate for Operations. Short and long range aircraft areused based on a particular task. Nearly 20 milliontons capacity can be moved on any given day. 536aircraft are currently committed.

Commercial aircraft used as US strategic airlifters havepromised, under the CRAF program, to make up morethan 90 percent of the Air Force’s long-range passen-ger-carrying capability and 30 percent of its cargo-hauling capability. As of 1995, commitments for the747 aircraft designated by the USAF as the C-19, arefor 136 passenger and 110 cargo equivalents. Thesefigures are based on current European-based sce-narios. This affects long-range international routes.

The 747 “classic” or -100/200 model can be convertedfrom a passenger to a freighter configuration in a mat-ter of hours. The main entrance is main deck cargocapability where the side cargo door is modified forthis conversion when needed. Passenger seats areremoved or reduced in number and the main deck isconverted to accept pallets.

Aeromedical evacuation aircraft or flying hospitalconfigurations are also part of CRAF. Air Forcekits converting aircraft into flying medical facilitiesfit only Boeing 767s. See the 767 segment for thisinformation. 44 aircraft are needed to fulfill require-ments. 19 are committed.

There are three stages in a call-up emergency:

Stage I: Can be set in motion by the head of the USTransportation Command. The use of a few aircraftfrom any one carrier resulting in a minimal impact onnormal civilian business.

Stage II: Activated only at the Secretary of Defenselevel. Impact is necessarily more serious. Airlinesshould be able to maintain normal operations.

Stage III: Must be authorized by an emergency dec-laration from the US President or Congress. Wouldlikely cause a serious impact on US civilian transpor-tation schedules.

FAA Part 139.315 - Index Categories Based on Aircraft Length ICAO Annex 14 - RFFS Categories Based on Aircraft Length & Fuselage Width (aircraft overall length; maximum fuselage width)

Index A - < 90' Category 1 - < 9m (29.5'); 2m (6.6') Category 6 - 28m (91.9') - < 39m (128.0'); 5m (16.4")Index B - 90' - <126' Category 2 - 9m (29.5') - <12m (39.4'); 2m (6.6') Category 7 - 39m (128.0') -<49m (160.8'); 5m (16.4")Index C - 126' - <159' Category 3 - 12m (39.4') - <18m (59.1'); 3m (9.8') Category 8 - 49m (160.8') - <61m (200.1'); 7m (23.0')Index D - 159' - <200' Category 4 - 18m (59.1') - <24m (78.7'); 4m (13.1') Category 9 - 61m (200.1') - <76m (249.3'); 7m (23.0')Index E - 200' or greater Category 5 - 24m (78.7') - <28m (91.9'); 4m (13.1') Category 10 - 76m (249.3') - <90m (295.3'); 8m (26.3')

FAA ARFF (Aircraft Rescue & Fire Fighting) Index ICAO RFFS (Rescue Fire Fighting Service) Category*Aircraft A B C D E Aircraft 6 7 8 9 10707 (all) X 707 (all) X717-200 X 717-200 X720 X 720 X727-100 X 727-100 X727-200 X 727-200 X737-100 X 737-100 X737-200 X 737-200 X737-300 X 737-300 X737-400 X 737-400 X737-500 X 737-500 X737-600 X 737-600 X737-700 X 737-700 X737-800 X 737-800 X737-900 X 737-900 XBBJ X BBJ XBBJ2 X BBJ2 X747SP X 747SP X747-100,200,300 X 747-100,200,300 X 747-400, 400ER X 747-400, 400ER X 757-200 X 757-200 X757-300 X 757-300 X767-200 X 767-200 X767-300 X 767-300 X767-400 X 767-400 X 777-200, 200LR X 777-200, 200LR X 777-300, 300ER X 777-300, 300ER X DC-8-43,55 X DC-8-43,55 XDC-8-61,71 X DC-8-61,71 XDC-8-62,72 X DC-8-62,72 XDC-8-63,73 X DC-8-63,73 XDC-9-15 X DC-9-15 XDC-9-21 X DC-9-21 XDC-9-32 X DC-9-32 XDC-9-41 X DC-9-41 XDC-9-51 X DC-9-51 XDC-10-10 X DC-10-10 XDC-10-30,40 X DC-10-30,40 XMD-11 X MD-11 X MD-81,82,83,88 X MD-81,82,83,88 XMD-87 X MD-87 XMD-90-30 X MD-90-30 X

* No Boeing Commercial Jet Aircraft In Categories 1 - 5 or 10

Boeing Commercial Aircraft - Rescue & Fire Fighting Categories (FAA & ICAO)

10/11/02Airport Technology

Boeing Commercial Airplanes

DC-3

DC

-3.

T.O. 00-105E

-9

AIRCRAFT PAINT SCHEME

1

DC-3

C-47

DC-3

DC

-3.

T.O. 00-105E

-9

AIRCRAFT DIMENSIONS

2

HEIGHT 16’ 11”(5.18 M)

LENGTH63’ 9” (19.43 M)

WING SPAN95’ 6 “ (29.20 M)

DC-3

DC

-3.

T.O. 00-105E

-9

3

FLAMMABLE MATERIALS AND ENTRY/EXIT LOCATIONS

HYDRAULIC FLUID TANK

FUELTANKS804 GAL(3043 L)

EMERGENCY EXITS

CARGO DOOR

MAIN CABIN ENTRANCE DOOR

ENGINEOIL TANK

ENGINE OIL TANK

BATTERIES

PILOT’S ENTRY DOOR

OXYGEN BOTTLE

DEICER FLUIDTANK

OVERHEAD EMERGENCY EXIT

A 2” WIDE BAND OF CONTRASTINGCOLOR INDICATING ALL EMERGENCYEXITS AND FORCED ACCESS AREAS

DC-3

DC

-3.

T.O. 00-105E

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4

SPECIAL TOOLS/EQUIPMENTPower Rescue SawFire Drill II

AIRCRAFT ENTRY

1. EMERGENCY ENTRY - DC-3/C-47

a. Pull emergency exit external handle, located on emergency exit aft of wing, each side of fuselage, to unlock and pull emergency exit hatch outward.

b. Rotate overhead crew escape hatch handle, located forward top center of fuselage, clockwise then pull hatch up and aft.

2. NORMAL ENTRY

a. Rotate main cabin entry handle, located on main cabin entry door, clockwise, then open door outward.

b. Pull pilot’s cargo door handle, located on fuselage forward right side on pilot’s cargo door, down. Open door outward.

3. CUT-IN

a. Cut-in areas are located at normal and emergency entrance points and at crew windows, left and right side of flightdeck.

NOTE: Crew size: 2 to 3. Passengers: 27 to 28.

FIRE CONTROLBOX (AC-47D)

400 GAL

400 GAL

204

204

200

200

385 385

PORTABLEOXYGENBOTTLES

BATTERIES

FLARE LAUNCHER

AMMUNITION

GUN POSITIONS (AC-47D)

OXYGEN CYLINDERS

1bOVERHEAD CREWEMERGENCY EXIT3aCUT-IN

1aEMERGENCY EXITS3aCUT-IN

2aMAIN CABINENTRY DOOR

3aCUT-IN

2bCREW ENTRY DOOR3aCUT-IN

3aFLIGHTDECKWINDOWSCUT-IN

DC-3

DC

-3.

T.O. 00-105E

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5

ENGINE SHUTDOWN ANDAIRCREW EXTRACTION1. ENGINE EMERGENCY SHUTDOWN

a. Pull firewall shutoff valve handle, located on engine fire extinguisher control panel, to the OUT position.

b. Turn master ignition switch, located on center overhead panel, to OFF position.

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

2. ENGINE NORMAL SHUTDOWN

a. Retard throttle control levers, located between pilot’s and co-pilot’s seats, to full CLOSE position.

b. Place mixture control levers, located between pilot’s and co-pilot’s seats, to the aft CUT-OFF position.

c. Turn master ignition switch, located on center overhead switch panel, to OFF position.

d. Turn battery switch, located on overhead switch panel, to OFF position.

3. AIRCREW EXTRACTION

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

NOTE: If seat tracks are not damaged during crash landing, use adjustable seat control to retract seats to aft position in removing crewmember(s).

2aTHROTTLECONTROLLEVERS

2bMIXTURECONTROLLEVERS

1b, 2cMASTERIGNITIONSWITCHES

ENGINE FIRE EXTINGUISHER CONTROL PANEL

1c, 2dBATTERY SWITCH

1aFIREWALL SHUTOFFVALVE HANDLES

DC-6

DC

-6.

T.O. 00-105E

-9


1

DC-6

USAF: C-118 USN: R6D “LIFTMASTER”VC-118 “The Independence” AND VIP

DC-6 FIREBOMBER

DC-6 FIREBOMBER“Still in service.”

DC-6

DC

-6.

T.O. 00-105E

-9

AIRCRAFT DIMENSIONS

2

WINGSPAN 117' 6" (35.8 M)

HEIGHT 28' 8" (8.7 M)

LENGTH 105' 7" (32.1 M)

DC-6

DC

-6.

T.O. 00-105E

-9

3

FLAMMABLE MATERIALS AND ENTRY/EXIT LOCATIONSA 2” WIDE BAND OF CONTRASTINGCOLOR INDICATING ALL EMERGENCYEXITS AND FORCED ACCESS AREAS

HYDRAULIC FLUID TANK

FUEL TANK2,702 GAL(10,228 L)

FORCEDACCESSAREAS

CARGO DOOR (DC-6A ONLY)

MAIN CABIN ENTRANCE DOOR

ENGINEOIL TANKS

ENGINE OIL TANK

BATTERIESCARGO DOOR(DC-6A ONLY)

OXYGEN BOTTLE

DEICERFLUIDTANK

PILOT’S ENTRANCE DOOR AUXILIARY OIL TANKS

FUEL TANK2,702 GAL(10,228 L)

FORCEDACCESSAREAS

DC-6

DC

-6.

T.O. 00-105E

-9

4


AIRCRAFT ENTRY - DC-6/C-118

1. NORMAL ENTRY

a. Rotate external control handle, located on main cabin entry door aft left side of fuselage, UP to open door.

b. Rotate external control handle, located on crew entry door forward right side of fuselage, UP to open door.

2. EMERGENCY ENTRY

a. Pull handle on emergency exits, located over each wing, OUT and pull exit hatch outward.

3. CUT-IN

a. Cut-in areas (marked in red) are located at normal and emergency entries and at cargo compartment windows and doors.

FUEL TANKS

MAIN CABINENTRY DOOR

3aCUT-IN

2aEMERGENCYEXITS

CREWENTRYDOOR

BATTERIES

OXYGEN BOTTLES(C-118 ONLY)

695

526

719

695

526

719762

762

1bCREW ENTRYEXTERNALCONTROLHANDLE

1aPASSENGER ENTRYEXTERNAL CONTROL HANDLE

CARGO DOOR (C-118 ONLY)

AFT CARGODOOR (C-118 ONLY)

DC-6

DC

-6.

T.O. 00-105E

-9

5

ENGINE SHUTDOWN ANDAIRCREW EXTRACTION1. ENGINE SHUTDOWN

a. Retard throttle control levers, located on control pedestal, to the CLOSED position.

b. Place mixture control levers, located on the control pedestal, to the CLOSED position.

c. Place ignition switches, located on forward overhead panel, to the OFF position.

d. Place master battery/generator switches cutoff bar, located on forward overhead panel, to the OFF position.

NOTE: If engines fail to shutdown, pull engine emergency T-handles, located on the main fire control panel, to the FULL-OUT position.




1dMASTER BATTERY/GENERATORSWITCHES CUTOFF BAR

FORWARD OVERHEAD PANEL

1cIGNITIONSWITCHES

ENGINE EMERGENCY T-HANDLES

1aTHROTTLES

CONTROL PEDESTAL


DC-7

DC

-7.

T.O. 00-105E

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1

DC-7

C-74 GLOBEMASTER I

DC-7

DC

-7.

T.O. 00-105E

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2

AIRCRAFT DIMENSIONS

WINGSPAN 117' 6" (35.8 M)

HEIGHT 28' 7" (8.7 M)

LENGTH 108' 11" (33.2 M)

C-74

DC-7

DC

-7.

T.O. 00-105E

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3

FLAMMABLE MATERIALS AND ENTRY/EXIT LOCATIONSDC-7/DC-7B SERIES

FUEL TANK 2,756 GAL (10,433 L)

ENGINE OIL TANKS

ENGINE OIL TANKS

BATTERIES

FIRE ACCESS


FIRE EXTINGUISHER BOTTLES

PORTABLE OXYGEN BOTTLES

FLARES


AUXILIARY ENGINE OIL TANK ON SOME ACFT

DC-7

DC

-7.

T.O. 00-105E

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4

FLAMMABLE MATERIALS AND ENTRY/EXIT LOCATIONS-ContinuedDC-7C SERIES


ENGINE OIL TANKS

ENGINE OIL TANKS

BATTERIES

FIRE ACCESS


FIRE EXTINGUISHER BOTTLES AUXILIARY ENGINE OIL TANK ON SOME ACFT

FLARES


DC-7

DC

-7.

T.O. 00-105E

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5

MAIN CABIN DOOR

1aMAIN CABIN DOOR

2a EMERGENCYEXIT DOOR

TYPICAL ESCAPE HATCHES

1aCREW AND CARGO DOOR

CHOP OUT AREAS

CHOP OUT AREAS

TYPICAL FIRE ACCESS


AIRCRAFT ENTRY - DC-7 SERIES

1. NORMAL ENTRY- CREW AND MAIN DOORS

a. Rotate handle counterclockwise.

b. Pull door outward.

2. EMERGENCY EXIT DOORS

a. Pull handle out.

b Push door inward.

3. ESCAPE HATCHES

a. Pull handle out.

b. Rotate handle counterclockwise.

c. Pull hatch out.

4. CHOP OUT/CUT-IN AREAS


1aCREW, MAIN ANDCARGO DOOR HANDLE

2aEMERGENCY EXIT DOOREXTERNAL HANDLE

4aCHOP OUT/CUT-IN

AIRCRAFT CROSS SECTION

3aESCAPE HATCHEXTERNAL HANDLE

DC-7

DC

-7.

T.O. 00-105E

-9

FLAMMABLE MATERIALS AND ENTRY/EXIT LOCATIONS-ContinuedDC-7C CARGO6


ENGINE OIL TANKS

ENGINE OIL TANKS

BATTERIES

FIRE ACCESS


FIRE EXTINGUISHER BOTTLES AUXILIARY ENGINE OIL TANK ON SOME ACFT

FLARES


DC-7

DC

-7.

T.O. 00-105E

-9

7


AIRCRAFT ENTRY - DC-7C CARGO

1. NORMAL ENTRY- CREW AND MAIN DOORS

a. Rotate handle counterclockwise.

b. Pull door outward.

2. EMERGENCY EXIT DOORS

a. Pull handle out.

b Push door inward.

3. ESCAPE HATCHES

a. Pull handle out.

b. Rotate handle counterclockwise.

c. Pull hatch out.

4. CHOP OUT/CUT-IN AREAS


1aCREW, MAIN ANDCARGO DOOR HANDLE

2aEMERGENCY EXIT DOOREXTERNAL HANDLE

4aCHOP OUT/CUT-IN


3aESCAPE HATCHEXTERNAL HANDLE

1aMAINCABINDOOR

2aEMERGENCYEXIT DOOR

TYPICALESCAPEHATCHES

1aCREW ANDCARGO DOOR

CHOP OUTAREAS

CHOP OUTAREAS

TYPICAL FIRE ACCESS

FWDCARGO DOOR

AFTCARGO DOOR

FLARES

FIREEXTINGUISHER BOTTLES

SIDEWINDOW(2 EACH)

OXYGEN BOTTLE(2 EACH)

DC-7

DC

-7.

T.O. 00-105E

-9

ENGINE SHUTDOWN ANDAIRCREW EXTRACTION

7

1. ENGINE SHUTDOWN

a. Retard throttle control levers, located on control pedestal, to the CLOSED position.

b. Place mixture control levers, located on the control pedestal, to the CLOSED position.

c. Place ignition switches, located on forward overhead panel, to the OFF position.

d. Place master battery/generator switches cutoff bar, located on forward overhead panel, to the OFF position.

NOTE: If engines fail to shutdown, pull engine emergency T-handles, located on the main fire control panel, to the FULL-OUT position.




1dMASTER BATTERY/GENERATORSWITCHES CUTOFF BAR

FORWARD OVERHEAD PANEL

1cIGNITIONSWITCHES

ENGINE EMERGENCY T-HANDLES

1aTHROTTLES

CONTROL PEDESTAL


DC

-8. DC-8T.O

. 00-105E-9


1

DC

-8. DC-8T.O

. 00-105E-9

AIRCRAFT DIMENSIONS

2

150.7’(45.93 M)

12.25’ (3.73 M)

13.55’ (4.13 M)

15.9’ (4.85 M)

57.5’ (17.53 M)

146.25’ (44.58 M) 47.5’

(14.48 M)

20.8’ (6.34 M) 142.4’

(43.40 M)

SCALE

5 10 15 M

0 10 20 30 40 50 FT

NOTE:HEIGHT VARIANCE

DC-8-4343’ 5.2” (13.24 M) MAXIMUM42’ 1.7” (12.84 M) MINIMUM

DC-8-43

SEE NOTE

DC

-8. DC-8T.O

. 00-105E-9

DC-8-55, 55F

AIRCRAFT DIMENSIONS-Continued

3

150.7’(45.93 M)

12.25’ (3.73 M)

13.55’ (4.13 M)

15.9’ (4.85 M)

57.5’ (17.53 M)

146.25’ (44.58 M) 47.5’

(14.48 M)

20.8’ (6.34 M) 142.4’

(43.40 M)

SCALE

5 10 15 M

0 10 20 30 40 50 FT

SEE NOTE


DC-8-55:43’ 6.7” (13.28 M) MAXIMUM42’ 1.7” (12.85 M) MINIMUM

DC-8-55F:43’ 8.9” (13.33 M) MAXIMUM42’ 1.3” (12.84 M) MINIMUM

DC

-8. DC-8T.O

. 00-105E-9

DC-8-62, -62F, -72, -72F


4

157.5’(48.01 M)

12.25’ (3.73 M)

13.55’ (4.13 M)

15.9’ (4.85 M)

60.8’ (18.53 M) 152.9’

(46.60 M) 47.5’ (14.48 M)

20.8’ (6.34 M) 148.4’

(45.23 M)

SCALE

5 10 15 M

0 10 20 30 40 50 FT

SEE NOTE


DC-8-62, -72:43’ 3.0” (13.18 M) MAXIMUM42’ 3.6” (12.89 M) MINIMUM

DC-8-62F, -72F:43’ 3.8” (13.20 M) MAXIMUM42’ 3.0” (12.88 M) MINIMUM

DC

-8. DC-8T.O

. 00-105E-9


DC-8-61, -7143’ 2.7” (13.17 M) MAXIMUM41’ 11.7” (12.79 M) MINIMUM


DC-8-63, -73:43’ 0” (13.11 M) MAXIMUM42’ 1.4” (12.84 M) MINIMUM


DC-8-61, -61F, -63, 63F, -73, -73F

5


187.4’(57.12 M)

12.25’ (3.73 M)

13.55’ (4.13 M)

15.9’ (4.85 M)

77.50’ (23.62 M) 182.9’

(55.75 M) 47.5’ (14.48 M)

20.8’ (6.34 M) 142.4’

(43.40 M)

SCALE

5 10 15 M

0 10 20 30 40 50 FT

SEE NOTE

DC

-8. DC-8T.O

. 00-105E-9

BATTERY(LOCATED IN RTWHEEL WELL)

CREWOXYGENSYSTEMBOTTLE

PASSENGEROXYGEN CYLINDERS

FUEL TANK8,950 GALS(33,879 L)

HYDRAULIC SUMPLOCATED IN LTWHEEL WELL


HYDRAULICACCUMULATORSLOCATED IN RTWHEEL WELL


HYDRAULIC ACCUMULATORSLOCATED IN NOSE WHEEL WELL

ENGINE OIL TANKS

HYDRAULICACCUMULATORLOCATED IN LTWING ROOT

HYDRAULIC ACCUMULATORSLOCATED IN LT WHEEL WELL

HYDRAULIC FLUID TANKSLOCATED IN LT WING ROOT

SPECIAL TOOLS/EQUIPMENTPower Rescue Saw35 Foot LadderFire Drill II

AIRCRAFT ENTRY-DC-8

1. NORMAL/EMERGENCY ENTRY

a. PASSENGER AND SERVICE DOORS - To open door, pull handle from recess, rotate handle forward, and pull door open.

b. EMERGENCY EXIT - To open door, hold handle, push release plate (handle on some aircraft only). Doors are hinged at bottom edge.

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

2. CUT-IN

a. Cut along window line as a last resort.

WARNING


2aCUT-IN AREAS

1aPASSENGER AND SERVICE DOORS

1bEMERGENCY EXIT

6

DC

-8. DC-8T.O

. 00-105E-9

EMERGENCY RESCUE ACCESS

BREAK GLASS FOR ACCESS TOHANDLE AND SLIDE WINDOW AFT

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

AFT PASSENGERENTRY DOOR

TYPICAL EMERGENCY EXITS

AVERAGE DISTANCEFLOOR LEVEL TO GROUNDWHEELS RETRACTED: 9 FTWHEELS EXTENDED: 13 FT

CUT-IN/CHOP OUT AREAS

AFT SERVICEENTRY DOOR

FWD PASSENGERENTRY DOOR

FWD SERVICEENTRY DOOR

ACCESS TO ACCESSORYCOMPARTMENT

7

NOTE:1. Observe markings on all doors for operability. Donot attempt to open doors which are banded ormarked inoperable.

2. Do not stand in front of passenger service oremergency exit doors when opening. Escape slidewill inflate automatically when door is opened anddrop over lowered door.

DC

-8. DC-8T.O

. 00-105E-9

8

1. ENGINE SHUTDOWN - ALL MODELS

a. Retard fuel control levers, located on center console, to full aft OFF position.

b. Retard throttles, located on center console, to IDLE START position.

c. Place battery switch, located on upper left corner of flight engineer’s panel, to OFF position.

NOTE: If engines fail to shutdown, pull emergency fire T-handles, located on center overhead panel.

This type aircraft is not equipped with an APU.


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

b. Passenger seats are equipped with lap belts only.

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

AGENTDISCHARGEHANDLES

EMERGENCYFIRET-HANDLES(4 EACH)

FUEL, AIRHYDRAULICOFFPOSITION

AGENTSELECTPOSITION

1cBATTERY SWITCH

1bTHROTTLES

1aFUELCONTROLLEVERS

FLIGHT DECK LOOKING FORWARD

FLIGHT ENGINEER PANEL

ENGINE SHUTDOWN ANDAIRCREW EXTRACTION

DC

-8. DC-8T.O

. 00-105E-9

9










ENGINE OIL TANKS



HYDRAULIC FLUID TANKSLOCATED IN LT WING ROOT


AIRCRAFT ENTRY-DC-8F





2. CUT-IN


WARNING


2aCUT-IN AREAS


1bEMERGENCY EXIT

DC

-8. DC-8T.O

. 00-105E-9












10

REMOVAL OF DOOR IS RESTRICTEDON SOME AIRCRAFT FWD CARGO

COMPARTMENT DOORS

CARGO LOADINGDOOR

AFT CARGOCOMPARTMENT DOORS



DC

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11


OXYGENBOTTLES








ENGINE OIL TANKS



HYDRAULIC FLUID TANKS LOCATEDIN LT WING ROOT


AIRCRAFT ENTRY-DC-8-61




c. EMERGENCY EXIT DOORS - To open door, pull handle from recess, rotate handle forward, and pull door open.


2. CUT-IN


WARNING


2aCUT-IN AREAS


1bEMERGENCY EXIT

1cEMERGENCY EXIT DOORS

DC

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12

GALLEY SERVICE DOOR

FWD CARGOCOMPARTMENT DOORS


OVERWING EMERGENCY EXITS

CUT-IN/CHOP OUTAREAS

TYPICAL EMERGENCY EXIT DOORS



DC

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13





TYPICALHYDRAULICPUMP





ENGINE OIL TANKS

HYDRAULIC SUMPS

HYDRAULIC SUMP LOCATEDIN LT WHEEL WELL

HYDRAULIC ACCUMULATORLOCATED IN LT WING ROOT







2. CUT-IN


WARNING


2aCUT-IN AREAS


1bEMERGENCY EXIT

SURGE DAMPERLOCATED IN LTWING ROOT

MAIN HYDRAULIC RESERVOIRLOCATED IN LT WING ROOT

DC

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14 NOTE:1. Observe markings on all doors for operability. Donot attempt to open doors which are banded ormarked inoperable.


DC

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15


OXYGENBOTTLES



HYDRAULICPUMP





ENGINE OIL TANKS

HYDRAULICSUMPS


HYDRAULIC FLUID TANKS LOCATEDIN LT WING ROOT







d. FORWARD UPPER CARGO DOOR EXTERNAL CONTROL PANEL - To open door, push lockpin handle down and hold. Insert wrench in hex end of door handle shaft and rotate counterclockwise to unlatch. Attach sling to door and hoist door open.

2. CUT-IN


WARNING


2aCUT-IN AREAS


1bEMERGENCY EXIT


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

1dFWD UPPER CARGODOOR EXTERNALCONTROL PANEL

SURGE DAMPERLOCATED IN LT WING ROOT

SURGE DAMPER

HYDRAULIC SUMP LOCATEDIN LT WHEEL WELL

DC

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16


CLEARVIEW WINDOWEXTERIOR ACCESS



EMERGENCY EXIT DOORS ON SOME AIRCRAFT




FWD PASSENGER ENTRY DOOR


ACCESS TO ACCESSORY COMPARTMENT

GALLEY SERVICE DOOR






EXTERIOR CONTROLPANEL

FWD UPPER CARGO DOOR



DC

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17

BATTERYOXYGENBOTTLES



SPOILER RESERVOIRLOCATED IN RTWHEEL WELL





ENGINE OIL TANKS

OPTIONALAPU

HYDRAULIC ACCUMULATORLOCATED IN LT WHEEL WELL

HYDRAULIC RESERVOIR LOCATEDIN LT WING ROOT








2. CUT-IN


WARNING


2aCUT-IN AREAS


1bEMERGENCY EXIT




AUXILIARYHYDRAULICPUMP

HYDRAULICACCUMULATOR

HYDRAULIC RUDDER RESERVOIRLOCATED IN LT WHEEL WELL

DC

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18












GALLEY SERVICE DOOR










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19




TYPICALHYDRAULICPUMP





ENGINE OIL TANKSOPTIONAL APU










2. CUT-IN


WARNING


2aCUT-IN AREAS


1bEMERGENCY EXIT




HYDRAULICRESERVOIR



DC

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20



















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21




SPOILER RESERVOIRLOCATED IN RTWHEEL WELL





ENGINE OIL TANKSOPTIONAL APU










2. CUT-IN


WARNING


2aCUT-IN AREAS


1bEMERGENCY EXIT




AUXILIARYHYDRAULICPUMP



TYPICAL HYDRAULICPUMP IN 4 PLACES

DC

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22












GALLEY SERVICE DOORON SOME AIRCRAFT










DC

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CABIN CONFIGURATION

23 DC-8-43

177 PASSENGERS 6 ABREAST SEATING129 SEATS ON 31” (78.7 CM) PITCH 24 SEATS ON 34” (86.4 CM) PITCH 12 SEATS ON 36” (91.4 CM) PITCH 6 SEATS ON 33” (91.4 CM) PITCH 6 SEATS ON 37” (94.0 CM) PITCH

GALLEYS

CREWSTORAGE

ATTENDANT’SDOUBLE SEAT

LAVATORIES

LAVATORIES

WINDSCREENMAIN ENTRY DOOR (B)34.5X72” (87.6X182.9 CM)

EMERGENCY EXIT TYPE III20X38” (50.86X96.5 CM)


AFT SERVICE DOOR (C)33.5X64” (85.1X162.6 CM)

AFT ENTRY DOOR (D)34.5X72” (87.6X182.9 CM)

GALLEY

SERVICE DOOR (A)33.5X64” (85.1X162.6 CM)

DC-8-55

189 PASSENGERS 6 ABREAST SEATING 66 SEATS ON 31” (78.7 CM) PITCH 66 SEATS ON 32” (81.3 CM) PITCH 39 SEATS ON 29” (99.1 CM) PITCH 18 SEATS ON 40” (101.6 CM) PITCH 6 SEATS ON 37” (94.0 CM) PITCH

GALLEY


LAVATORY

LAVATORIES

MAIN ENTRY DOOR (B)34.5X72” (87.6X182.9 CM)



AFT SERVICE DOOR (C)33.5X64” (85.1X162.6 CM)


GALLEYS


GALLEY

DC

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CABIN CONFIGURATION-Continued

24 DC-8-62, -72

189 PASSENGERS 6 ABREAST SEATING189 SEATS ON 34” (86.4 CM) PITCH

GALLEY

CREWSTORAGE


LAVATORIES

LAVATORIES

WINDSCREEN




AFT SERVICE DOOR (C)34X64” (86.4X162.6 CM)


GALLEYS


DC-8-61, -63, -71, -73

259 PASSENGERS 6 ABREAST SEATING177 SEATS ON 32” (81.3 CM) PITCH 24 SEATS ON 38” (96.5 CM) PITCH 58 SEATS ON 31” (78.7 CM) PITCH

1 AND 2GALLEY

ATTENDANT’S DOUBLE SEAT

LAVATORIES

LAVATORY




AFT SERVICE DOOR (C)34X64” (86.4X162.6 CM)


SERVICE DOOR (A) 33.5X64” (85.1X162.6 CM)

3 AND 4GALLEY


ATTENDANTSEAT

EMERGENCY EXIT TYPE I 24X56” (61X142.2 CM)

EMERGENCY EXIT TYPE I24X56” (61X142.2 CM)





DC

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CARGO CONFIGURATION

25 DC-8-55F

PALLETS 1 THROUGH 12 5543.2 CU ‘ (154. CU M)PALLET 13 460 CU’ (13.03 CU M)LOWER DECK CARGO 1390 CU’ (39.4 CU M)TOTAL CARGO 7293.2 CU’ (206.63 CU M)

BARRIER NET

CREW GALLEY

LAVATORY

FWD ENTRY DOOR34.5X72” (87.6X182.9 CM)

SERVICE DOOR34X64” (86.4X162.6 CM)


1 2 3 4 5 6 7 8 9 10 11 12 13

CARGO DOOR85X140” (215.9.6X355.6 CM)

CARGO PALLET (13 PLACES) 88X125” (224X318 CM)

SERVICE DOOR33.5X64” (85.1X162.6 CM)

DC-8-62F, -72F

PALLETS 1 THROUGH 13 5896.8 CU ‘ (154. CU M)PALLET 14 460 CU’ (13.03 CU M)LOWER DECK CARGO 1615 CU’ (45.74 CU M)TOTAL CARGO 7971.8 CU’ (225.77 CU M)

BARRIER NET

CREWGALLEY

LAVATORY




1 2 3 4 5 6 7 8 9 10 11 12 13 14

CARGO DOOR85X140” (215.9.6X355.6 CM)

CARGO PALLET (14 PLACES)88X125” (224X318 CM)


DC-8-61F, -63F, -71F, -73F

PALLETS 1 THROUGH 17 7711.2 CU ‘ (218.4 CU M)PALLET 18 460 CU’ (13.03 CU M)LOWER DECK CARGO 2500 CU’ (70.8 CU M)TOTAL CARGO 10671.2 CU’ (302.23 CU M)

CREW GALLEY

LAVATORY



AFT ENTRY DOOR34.5X72” (87.6X182.9 CM)

1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18

MAIN CARGO DOOR85X140” (215.9.6X355.6 CM)

CARGO PALLET (18 PLACES) 88X125” (224X318 CM)


BARRIER NET

DC

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. 00-105E-9


1

DC

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AIRCRAFT DIMENSIONS

2

104’ 4.8”(31.82 M)

SCALE

5 10M

0 10 20 30 40’

8’ 10.5”(2.70 M)

11’ 0”(3.35 M)DOOR (A)

DOOR (B)

SEENOTE

11’ 10.0”(3.61 M)

43’ 8.4”(13.32 M)

92’ 1.2”(28.07 M) 36’ 10.8”

(11.25 M) 7’ 7.2”(2.32 M)

16’ 4.8”(5.00 M)

89’ 4.8”(27.25 M)

DC-9-15

NOTE: DC-9-15 MAX - 27’ 7.0” (8.4 M) - MIN - 27’ 5.0” (8.4 M) DC-9-21 MAX - 27’ 5.0” (8.4 M) - MIN - 27’ 5.0” (8.4 M)

104’ 4.8”(31.82 M)

SCALE

5 10M

0 10 20 30 40’

8’ 10.5”(2.70 M)

11’ 0”(3.35 M)DOOR (A)

DOOR (B)

SEENOTE

11’ 10.0”(3.61 M)

43’ 8.4”(13.32 M)

92’ 1.2”(28.07 M)

36’ 10.8”(11.25 M)

7’ 7.2”(2.32 M)

16’ 4.8”(5.00 M)

DC-9-21

93’ 3.6”(28.44 M)

DC

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3

DC-9-32

119’ 3.6”(36.36 M)

SCALE

5 10M

0 10 20 30 40’

8’ 10.5”(2.70 M)

11’ 0”(3.35 M)DOOR (A)

DOOR (B)

11’ 10.0”(3.61 M)

53’ 2.4”(16.22 M) 107’ 0”

(32.61 M)

36’ 10.8”(11.25 M)

7’ 7.2”(2.32 M)

16’ 4.8”(5.00 M)

93’ 3.6”(27.25 M)

NOTE: DC-9-32 MAX - 27’ 9.0” (8.5 M) - MIN - 27’ 6.0” (8.4 M) DC-9-41 MAX - 28’ 5.0” (8.7 M) - MIN - 27’ 0” (8.5 M)

SEENOTE

DC-9-41

125’ 7.2”(38.28 M)

SCALE

5 10M

0 10 20 30 40’

8’ 10.5”(2.70 M)

11’ 0”(3.35 M)DOOR (A)

DOOR (B)

11’ 10.0”(3.61 M)

56’ 1.2”(17.10 M)

113’ 3.6”(34.53 M)

36’ 10.8”(11.25 M)

7’ 7.2”(2.32 M)

16’ 4.8”(5.00 M)

93’ 3.6”(27.25 M)

SEENOTE

DC

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4

DC-9-41

133’ 7”(40.72 M)

SCALE

5 10M

0 10 20 30 40’

8’ 10.5”(2.70 M)

11’ 0”(3.35 M)DOOR (A)

DOOR (B)

11’ 10.0”(3.61 M)

60’ 11”(18.57 M) 121’ 3”

(36.96 M)

36’ 10.8”(11.25 M)

7’ 7.2”(2.32 M)

16’ 0”(4.88 M) 93’ 4.2”

(28.45 M)

SEENOTE

DC-9-51

SEENOTE

NOTE: DC-9-51 MAX - 28’ 9.0” (8.8 M) - MIN - 28’ 3.0” (8.6 M)

DC

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5

AIRCRAFT SKIN PENETRATION POINTS

FUSELAGE (BOTH SIDES)PENETRATE APPROXIMATELY 4 INCHESBELOW CABIN WINDOWS. AVOIDPENETRATING EMERGENCY EXITS.

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

DC

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6

ENGINE DANGER AREAS

DIS

TA

NC

E F

RO

M A

IRC

RA

FT

C L40

20

0

20

40

10

5

5

10

10

5

5

10

40

20

0

20

40

25 FT ENGINE INTAKE DANGER AREA

FEET METERS 100 200 300 400 500 600 700

30 60 90 120 150 180 210

IDLE POWER

AXIL DISTANCE BEHIND AIRCRAFT

TAKEOFFPOWER

Jet Intake and Blast Distances

@ 35 MPH

@ 45 MPH

@ 60 MPH

@ 75 MPH

@ 100 MPH

@ 150 MPH

@ 200 MPH

ENGINE BLAST DANGER AREAS

FEET

METERS

DC

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7

AIRCRAFT DANGER AREAS

WARNING

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

1. APU ACCESS DOORS

a. Insert screwdriver or similar tool into slot of camlock fasteners.

b. Turn fasteners to the left to open.

c. Pull down access doors.

2. ENGINE NACELLE LOWER COWL DOOR

a. Release four (4) latches on upper cowl door.

b. Push in safety latch release while holding door up with one hand.

c. Lower door to full open position.

1cAPU GROUNDCONTROL PANELACCESS DOOR

1a, 1bCAMLOCK SLOTHEAD LATCH

1cAPU ACCESS DOOR

2aUPPER COWL DOOR LATCH

2bSAFETY LATCH RELEASE

2cLOWER COWL DOOR

2aCOWL LATCHES(TYPICAL 4 PLACES)

APU ACCESS DOORS AND ENGINE NACELLELOWER COWL DOOR

DC

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AIRCRAFT FLAMMABLE MATERIAL LOCATIONS

OPTIONAL AUXILIARY FUEL TANK

OPTIONAL AUXILIARY FUEL TANK

FUEL VENT BOX

FUEL VENT BOX

FUEL OVERFLOWSTAND PIPE

FUEL OVERFLOWSTAND PIPE

1386 GALS(5247 LITRES)



HYDRAULIC ACCUMULATORS

HYDRAULIC ACCUMULATORS

FIRE EXTINGUISHER AGENT CONTAINERS

APU GROUND CONTROLPANEL ON FUSELAGE

PORTABLE OXYGEN BOTTLE

CREW OXYGENSYSTEM BOTTLES

RAIN REPELLENTCONTAINERS

PORTABLE OXYGENSYSTEM BOTTLE

CREW OXYGENSYSTEM BOTTLES

BATTERIES QUICKDISCONNECTSBATTERIES

ENGINE OIL TANKS

APU EXHAUST DUCTON RT SIDE ONLY

HYDRAULIC FLUIDRESERVOIR 1 PLACE INEACH WHEEL WELL

1

1

2

2

780/1000 GALS(2953/3785 LITRES)

580/780/1000/1250 GALS(2196/2953/3785/4732 LITRES)

8

DC

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9


AIRCRAFT ENTRY

1. NORMAL ENTRY

CAUTION

When doors are opened from outside, slide chutes automatically deploy.

a. Pull handle, located on left forward entry door, out, rotate counterclockwise and pull door outward.

b. Pull stairway handle, located forward left bottom side of fuselage, outward, press the open button to extend stairway.

c. Pull handle, located on right forward service door, out, rotate clockwise and pull door outward.

2. EMERGENCY ENTRY

Caution must be exercised when releasing tail cone. Keep personnel clear. Tail cone free falls when released from aircraft.

a. Push in jettisonable tail cone T-handle door, located on left fuselage forward of tail cone, pull T-handle to jettison tail cone. Jettison door is approximately 8.5 feet high.

b. Open rear stairway control panel, located on aft left exterior fuselage, push control handle to forward OPEN position to release stairway.

CAUTION

Stairway free falls to down position.

c. Push overwing exit door handle release, two doors are located over each wing, pull handle to unlatch door, push in and lift up forcibly.

WARNING

2cEMERGENCY OVERWING EXIT(BOTH SIDES)

2aTAIL CONEJETTISONHANDLE

2bCONTROL HANDLE

AFT ENTRANCE STAIRWAYCONTROL PANEL

OPEN BUTTON

1bFORWARDPASSENGERSTAIRWAYHANDLE

1cFORWARD SERVICEENTRANCE DOORHANDLE

1aPASSENGERDOORHANDLE

DC

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10

AIRCRAFT EMERGENCY EXITSAFT PASSENGER DOOR STAIRWAY INTERIORAND EXTERIOR CONTROLS

NOTE:· For manual stairway operation, hold interior or exterior control handle in open position. Stairway will free fall open.

· Interior control handle is removed on some aircraftmaking the stairway inoperable from the inside.

PASSENGER AFT ENTRANCESTAIRWAY EXTERIOR CONTROL PANEL

EMERGENCY EXIT

ON SOME AIRCRAFT

STAIR OPERATING HANDLE INSIDE

CONTROL HANDLE

OPEN DOOR FORACCESS STAIR CONTROL

PASSENGER AFT ENTRANCESTAIRWAY INTERIOR CONTROL PANEL

OPEN CLOSE

DC

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11

AIRCRAFT EMERGENCY EXITS-ContinuedPRESSURE BULKHEAD EMERGENCY EXIT, TAILCONE JETTISON,AND MAIN CARGO DOOR OPERATION

MAIN CARGO DOOR (IF APPLICABLE)

NOTE: Use only when all other exits are blocked and time permits.

MANUAL LATCH CONTROLS

a. If installed, turn vent door handle to the UNLOCKED position.b. Turn lockpin handle to UNLOCK and hold.c. Insert pipe in latch fitting and move to UNLOCK.d. Release spring loaded lockpin handle.

HOIST BAR

PLACE CABLE LOOP OR HOOKTHROUGH HERE TO MANUALLY HOIST DOOR OPEN

LATCHACTUATINGSOCKET

LOCKPIN HANDLE(Spring loaded to thelocked position.)

PIPE

VENT DOOR(SOME AIRCRAFT)

INSERT PIPE HERE TOMANUALLY UNLOCK ORLOCK DOOR

CARGO AIRCRAFT ONLY

AFT PRESSUREBULKHEAD

HANDLE IN TAIL SECTIONON PRESSURE BULKHEADDOOR (PULL TO UNLOCK PUSH DOOR IN)

HANDLE ON PRESSURE BULKHEAD DOOR (LIFT TO UNLOCK PULL DOOR IN)

ON SOMEAIRCRAFT

VIEWINGWINDOW

OPEN

INTERIOR VIEW

DC

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12

AIRCRAFT EMERGENCY EXITS1. CLEARVIEW WINDOW FOR CARGO AIRCRAFT ONLY

a. Push in both access doors.

b. Push window handle aft, then down.

c. Push window aft.

2. LOWER CARGO COMPARTMENT DOORS

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

b. Rotate door handle counterclockwise to unlatch door.

c. Push door upward into cargo compartment.

3. ELECTRICAL/ELECTRONIC COMPARTMENT DOOR

a. Push right side of handle inward and pull left side of handledown to unlatch door.

b. Push door inward and to the left to open.

EXTERIOR ACCESS(KNOCKOUT PANELS)

CARGOAIRCRAFTONLY

1b

1c

1a

CLEARVIEW WINDOW

2a

2b

(TYPICAL BOTH DOORS)

LOWER CARGOCOMPARTMENT DOORS

ELECTRICAL/ELECTRONICSCOMPARTMENT DOOR

PUSH PULL3a

DC

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13

CLEARVIEW WINDOW - EXTERIORACCESS KNOCKOUT PANEL ONCARGO AIRCRAFT


AFT PASSENGER ENTRY DOOR

PRESSURE BULKHEAD EMERGENCY EXIT


PASSSENGER AFT ENTRANCESTAIRWAY INTERIOR CONTROLPANEL ON SOME AIRCRAFT

APU COMPARTMENT ACCESS DOOR


FWD SERVICE ENTRY DOOR

TAIL CONE ACCESS DOOR

MAIN CARGO DOORAND EXTERNAL CONTROL PANELON CARGO AIRCRAFT ONLY

ENGINE NACELLE LOWER COWL DOOR


CLEARVIEW WINDOW -CHILL PANE WITH CO2 ANDBREAK WITH HEAVY FIRE AXEFOR ACCESS TO HANDLE;SLIDE WINDOW AFT


JETTISONABLE TAIL CONE

AFT LOWER CARGO DOOR

TAIL CONE JETTISON LATCH

FWD LOWER CARGO DOOR

DC

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14

ENGINE/APU SHUTDOWN ANDAIRCREW EXTRACTION

1. ENGINE/APU SHUTDOWN

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 IDLECUTOFF position.

c. Place battery switch, located on center over-head panel, toOFF position.

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

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 tailcone, open door by pushing twolatches. Place APU master switch to the APU shutoff (up)position. If “Fire” light is illuminated ...place discharge fireswitch (up) position to release fire agent 1. Wait 10seconds to use fire agent 2, if applicable.


a. Unlatch lap belt and remove shoulder harness fromcrewmember.

b. If seat tracks are not damaged during crash landing, useadjustable seat controls to retract seat to aft position.Pilot’s controls are on right side of seat while co-pilot’s areon the left.

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

d. Passenger seats are only equipped with lap belts.

CENTER OVERHEAD PANELPILOT’S STATION (TYPICAL)

1dAPUMASTERSWITCH

1cBATTERY SWITCH

1bTHROTTLES

LOW AGENT INDICATING LIGHTS

LEFTENGINE

RIGHTENGINE

EMERGENCY FIRE T-HANDLES CENTER OVERHEAD PANEL

1aFUEL CONTROL LEVERS

FIREWARNINGHORN

DOOR

APU GROUNDCONTROLSAND FIREEXTINGUISHERS

LATCHES

1eAPUSHUTOFF

1eFIREAGENT DISCHARGE SWITCHES

APU GROUND CONTROL PANEL

DC

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CABIN CONFIGURATION

15 DC-9-15,-21

90 PASSENGERS 5 ABREAST SEATING50 SEATS ON 32” (81.3 CM) PITCH40 SEATS ON 31” (78.7 CM) PITCH

NOTE: Maximum of 90 passengers, 5-abreast seating available.

DC-9-32

115 PASSENGERS 5 ABREAST SEATING 55 SEATS ON 33” (83.8 CM) PITCH 10 SEATS ON 36” (91.4 CM) PITCH 50 SEATS ON 31” (78.7 CM) PITCH


GALLEY


LAVATORY

CREWSTORAGE


EMERGENCY EXIT TYPE III 20X36” (51X91 CM)

SERVICE DOOR (A)27X48” (69X122 CM)

SCALE

0 2 4 6 METERS

0 10 20 FEET

LAVATORY



SCALE

0 2 4 6 METERS

0 10 20 FEET

GALLEY


LAVATORY

CREWSTORAGE




LAVATORY



DC

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16 DC-9-41

125 PASSENGERS 5 ABREAST SEATING66 SEATS ON 34” (86.4 CM) PITCH 5 SEATS ON 33” (83.8 CM) PITCH30 SEATS ON 32” (81.3 CM) PITCH25 SEATS ON 31” (78.7 CM) PITCH


DC-9-51

135 PASSENGERS 5 ABREAST SEATING 5 SEATS ON 35” (88.9 CM) PITCH 5 SEATS ON 34” (86.4 CM) PITCH 66 SEATS ON 33” (83.8 CM) PITCH 60 SEATS ON 32” (81.3 CM) PITCH


GALLEY


LAVATORY

CREWSTORAGE

MAIN ENTRY DOOR (B)34X72” (86X183 CM) EMERGENCY EXIT TYPE III

20X36” (51X91 CM)


SCALE

0 2 4 6 METERS

0 10 20 FEET

LAVATORY



SCALE

0 2 4 6 METERS

0 10 20 FEET

GALLEY


LAVATORY

CREWSTORAGE

MAIN ENTRY DOOR (B)34X72” (86X183 CM)



LAVATORY



DC

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CARGO CONFIGURATION

17 DC-9-15F

DC-9-32F

LAVATORY

FWD ENTRY DOOR (B)34X72” (86.4X182.9 CM)TYPE 2

SERVICE DOOR (A)27X48” (68.6X121.9 CM)

SCALE

0 2 4 6 METERS

0 10 20 FEET

LAVATORY

SCALE

0 2 4 6 METERS

0 10 20 FEET

GALLEY

CARGO PALLET1 PLACE167 FT (4.7 M )

FWD CARGOBARRIER NET

CARGO DOOR (C)81X136” (205.7X345.4 CM)

CARGO PALLETS6 PLACES360 FT(10.2 M )

SERVICE DOOR (A)27X48” (69X122 CM)TYPE I LAVATORY

33

LAVATORYFWD ENTRY DOOR (B)34X72” (86.2X182.9 CM)TYPE I

CARGO VOLUMES

PALLET SIZE #1 THRU 6 88X108” (224X274 CM)

PALLETS 1 THRU 6 2161 FT (61.2 M )LOWER DECK CARGO 600 FT (17.0 M )TOTAL CARGO 2761 FT (78.2 M )

3 33 33 3

FWD CARGOBARRIER NET

1 2 3 4 5 6

CARGO VOLUMES

PALLET SIZES #1 and 10 54X88” (137X224 CM) #2 THRU 9 88X108” (224X274 CM)

PALLET 1 174 FT (4.9 M )PALLETS 2 THRU 9 2959 FT (83.8 M )PALLET 10 167 FT (4.7 M )LOWER DECK CARGO 895 FT (25.3 M )TOTAL CARGO 4195 FT (118.8 M )

3

3

3

3

3

3 3

1 2 3 4 5 6 7 8 9 10CARGO PALLETS1 PLACE174 FT(4.9 M )

33

33

CARGO PALLETS8 PLACES370 FT(10.5 M )

CARGO DOOR (C)81X136” (205.7X345.4 CM)

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1

DC-10T.O

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-10.

AIRCRAFT DIMENSIONS

DC-10 SERIES 10 (LOWER GALLEY) DC-10 SERIES 10 AND 10CF (UPPER GALLEY)

182’ 3.1”(55.55 M)

70”X66”(177.8CM X 167.6CM)

19’ 9”(6.02 M)

26’ 10”(8.18 M)

27’ 10.5”(8.50 M)

19’ 9”(6.02 M)

72’ 5”(22.07 M)

170’ 6”(51.97 M)

SEENOTE

155’ 4”(47.35 M)

71’ 2”(21.69 M)

35’ 0”(10.67 M)

SCALE

0 2 4 6 M

0 10 20 FT

NOTE: Height, depending on load varies from 57’ 4” (17.48M) to 58’ 5” (17.81M).

182’ 3.1”(55.55 M)

104”X66”(164.2CM X 167.6CM)

19’ 9”(6.02 M)

26’ 10”(8.18 M)

27’ 10.5”(8.50 M)

19’ 9”(6.02 M)

170’ 6”(51.97 M)

SEENOTE

155’ 4”(47.35 M)

71’ 2”(21.69 M)

35’ 0”(10.67 M)

SCALE

72’ 5”(22.07 M)

0 2 4 6 M

0 10 20 FT

CARGO DOOR 10CF ONLY

2

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-10.


3

DC-10 SERIES 30 AND 30CF (LOWER GALLEY)

181’ 7.2”(55.35 M)

19’ 9”(6.02 M)

26’ 10”(8.18 M)

27’ 10.5”(8.50 M)

19’ 9”(6.02 M)

170’ 6”(51.97 M)

SEENOTE

165’ 4”(50.39 M)

71’ 2”(21.69 M)

35’ 0”(10.67 M)

SCALE

72’ 5”(22.07 M)

0 2 4 6 M

0 10 20 FT


DC-10 SERIES 30 AND 30CF (UPPER GALLEY)

181’ 7.2”(56.35 M)

19’ 9”(6.02 M)

26’ 10”(8.18 M)

27’ 10.5”(8.50 M)

19’ 9”(6.02 M)

170’ 6”(51.97 M)

SEENOTE

165’ 4”(50.39 M)

71’ 2”(21.69 M)

35’ 0”(10.67 M)

SCALE

72’ 5”(22.07 M)

0 2 4 6 M

0 10 20 FT



70”X66”(177.8CM X 167.6CM)

104”X66”(164.2CM X 167.6CM)

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-10.


DC-10 SERIES 40 AND 40CF (LOWER GALLEY)

182’ 2.6”(55.54 M)

19’ 9”(6.02 M)

26’ 10”(8.18 M)

27’ 10.5”(8.50 M)

19’ 9”(6.02 M)

170’ 6”(51.97 M)

SEENOTE

165’ 4”(50.39 M)

71’ 2”(21.69 M)

35’ 0”(10.67 M)

SCALE

72’ 5”(22.07 M)

0 2 4 6 M

0 10 20 FT


DC-10 SERIES 40 AND 40CF (UPPER GALLEY)

182’ 3.1”(55.55 M)

104”X66”(164.2CM X 167.6CM)

19’ 9”(6.02 M)

26’ 10”(8.18 M)

27’ 10.5”(8.50 M)

19’ 9”(6.02 M)

170’ 6”(51.97 M)

SEENOTE

165’ 4”(50.39 M)

71’ 2”(21.69 M)

35’ 0”(10.67 M)

SCALE

72’ 5”(22.07 M)

0 2 4 6 M

0 10 20 FT



70”X66”(177.8CM X 167.6CM)

4

DC-10T.O

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DC

-10.5 JET INTAKE AND BLAST DISTANCES

NOTE: Crosswinds will have considerable effect on contours.

5 FEET

35 MPH EXHAUST CURVE (TAKEOFF POWER)

35 MPH EXHAUST CURVE (IDLE POWER)

215 FEET

1,500 FEET

A

B

A 20 FOOT RADIUS

B 30 FOOT RADIUS

VIEW LOOKING UP FROM BOTTOM OF AIRCRAFT

ENGINE DANGER AREAS

INTAKE DANGER AREA

IDLE DANGER AREA

TAKE OFF EXHAUST DANGER AREA

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-10.6

AIRCRAFT EVACUATION ROUTESAND CLEARVIEW WINDOW ENTRY1. CLEARVIEW WINDOW ENTRY To gain access into flight compartment:

a. Chill clearview window pane with CO2.

b. Break window pane with heavy fire ax or suitable device.

c. Depress lock lever and push lever aft.

d. Push crank handle outboard and turn clockwise to move window aft.

AFT

1cLOCK LEVER 1a, 1b

CLEARVIEW WINDOW

RAMPWITHSLIDE

ESCAPEROPES

1dCRANK HANDLE

DOUBLE TRACK EVACUATION SLIDES (BOTH SIDES)

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DC

-10.7

ENGINE NACELLE DOORS ANDFAN COWL ACCESS DOORS1. ENGINE NACELLE DOORS To open fan reverser:

a. Open fan and core cowl doors.

b. Open blowout and lower latch access panel doors on bottom of reverser.

c. Release forward mounting ring latches on each side of reverser.

d. Press trigger on door tension latch handle to release handle.

e. Pull handle to fully unlatched position.

f. Disengage latch hook from u-bolt.

g. Insert speed handle or nut runner into flex- shaft socket and crank reverser half open.

2. TO OPEN FAN AND CORE COWL DOORS

a. Press trigger on door tension latch handle to release handle.

b. Pull handle to fully unlatched position.

c. Disengage latch hook from u-bolt.

d. Raise door to open position and engage hold-open rods with engine fittings.

FAN REVERSER

1a, 2dFAN COWL DOORS (2)

1bACCESS DOORS

1e, 2bLATCH HANDLE

1d, 2aTRIGGER

1f, 2cLATCH HOOK

1cRING LATCHES(3 PLACES EACHDOOR)

COMPARTMENTCOOLING AIR EXIT

ENGINE OIL TANKSERVICING DOOR CSD SERVICING

DOOR

PRESSURE RELIEF DOOR GENERATORCOOLINGAIR EXIT

GEARBOXBREATHEROUTLET

COMPARTMENTCOOLING AIRINLET COMPARTMENT

COOLING AIR EXIT

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AIRCRAFT ACCESS DOORS

8 1. CENTER ACCESSORY COMPARTMENT DOOR

a. Pull down external handle and rotate in direction indicated by placarding on door.b. Stow handle and slide door to right side of fuselage.

2. APU ACCESS DOOR

a. Press trigger to release handle.b. Support door after unlatching.c. Door opens down.

3. APU GROUND CONTROL PANEL COMPARTMENT DOOR

a. Press three (3) triggers on door to release three handles.b. Door opens down.

1aEXTERNALHANDLE

CENTER ACCESSORYCOMPARTMENTACCESS DOOR

APU COMPARTMENTACCESS DOOR

2aHANDLE

2aTRIGGER

3aTRIGGER

3aHANDLE(TYPICAL)

ON ACFT WITHLOWER GALLEYONLY

APUCONTROLPANEL

FIREWARNINGHORN

APU CONTROL PANELCOMPARTMENT DOOR

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DC

-10.9

FUEL VENT BOX (TYPICAL BOTH WINGS)OVERBOARD OUTLET (TYPICAL BOTH WINGS)

FUEL TANK #3 6000 GAL. (APPROX.)PRESSURE REFUELING/DEFUELING ADAPTORS(INSIDE ACCESS DOOR, TYPICAL BOTH WINGS)

ENGINE #3 FUEL FIRE SHUTOFF VALVEENGINE #3 HYDRAULIC FIRE SHUTOFF VALVEPORTABLE OXYGEN BOTTLES (CTR PARTITION)

FIRE EXT AGENT CONTAINERS (800 PSI, ENG #3)ENGINE #3

FUEL TANK #2 (CONTINUES OPPOSITE WING 9700 GAL. APPROX.)

AUXILIARY FUEL TANK (14,600 GAL. APPROX.)CUT-IN AREA (TYPICAL ENGINES #1 & #3)

ENGINE OIL TANK (TYPICAL ENGINES #1 & #3)PORTABLE OXYGEN BOTTLE (FWD PARTITION- TYPICAL 6 ATTENDANT’S STATIONS)WATER FIRE EXT (RT ATTENDANT’S STATION)

DRY CHEMICAL FIRE EXT (LT ATTENDANT’S STATION)

DRY CHEMICAL FIRE EXT

PASSENGER DOOR PNUEMATIC BOTTLE (1500 PSI, TYPICAL ALL PASSENGER DOORS)

PORTABLE OXYGEN BOTTLES (FWD)

EMERGENCY LIGHTING BATTERY POWER SUPPLY

RAIN REPELLENT CONTAINER (90 PSI)

CLEARVIEW WINDOW (BOTH WINDOWS TYPICAL-CHOP IN AREA)

EMERGENCY LIGHTS CONTROL SWITCH(OVERHEAD SWITCH PANEL)

ENGINE FIRE CONTROL HANDLES

CREW PORTABLE OXYGEN BOTTLE (CREW COATROOM PARTITION)

AVIONICS COMPARTMENT LOWER DOORINERTIAL NAVIGATION SYSTEM BATTERIES (IF INSTALLED) CREW FIXED OXYGEN

BOTTLE (1850 PSI)OXYGENOVERFLOWVENT

ENGINE #1LOWER CARGO FIRE EXT CONTAINER INSTALLATION

EMERGENCY LIGHTING BATTERY POWER SUPPLYPASSENGER DOOR (42 X 76 INCHES, TYPICAL 6 PLACES)

FORWARD CARGO DOORUPPER CARGO DOOR (CONVERTIBLE FREIGHTER AIRCRAFT ONLY)

EMERGENCY LIGHTS CONTROL SWITCH (FWD LT ATTENDANT STATION)PASSENGER DOOR (32 X 76 INCHES, OPPOSITE DOOR TYPICAL)ESCAPE SLIDE PNEUMATIC BOTTLE (3000 PSI-INSIDE ESCAPE SLIDE-TYPICALALL PASSENGER DOORS)AVIONICS COMPARTMENT AFT DOOR

CARBON DIOXIDE AND WATER FIRE EXTINGUISHERS (FLIGHT COMPARTMENT ONCOATROOM PARTITION) FUEL TANK #1 (6000 GAL. APPROX.)

FUEL DUMP OUTLET (TYPICAL OPPOSITE WING)PORTABLE OXYGEN BOTTLES (4 1/4 OR 11 CU FT- AFT PARTITION)

EMERGENCYLIGHTING BATTERYPOWER SUPPLY

APU FUEL FIRE SHUTOFF VALVE

EMERGENCY LIGHTING BATTERYPOWER SUPPLY

CENTER CARGO DOOR

ENGINE #2ENGINE OIL TANKENGINE #2 HYDRAULICFIRE SHUTOFF VALVEFIRE EXT AGENT CONTAINERS (800 PSI-AFTACC COMP, FOR ENGINE #2 & APU AREA)HYDRAULIC FLUID RESERVOIR (AFTACCESSORY COMPARTMENTAFT ACCESSORY COMPARTMENT

APU EXHAUST DUCT (RT SIDE ONLY)APU COMPARTMENT DOORAPU FUEL FIRE SHUTOFF VALVEPRESSURE BULKHEAD (AFT END OFPASSENGER COMPARTMENT)HORIZONTAL STABILIZER JACK SCREWS &MOTORS ACCESS DDORWATER FIRE EXT (RT SIDE AFT DIVIDERPARTITION)AFT CARGO DOOR

CUT-IN AREA (SKIN 0.071 INCH, LONGERONS0.050 TO 0.063 INCH - TYPICAL 8 AREAS)

HYD ACCUMULATORS (1000 PSI, WHEELWELL, TYPICAL BOTH WHEELS)HYD FLUID RESERVOIR (WHEEL WELL,OPPOSITE SIDE TYPICAL)

FIRESEALS (TYPICAL ALL ENGINES)

APU GRD CONTROL PANEL (AFT OF WHEELWELL, LT SIDE)ENGINE #2 FWD FUEL SHUTOFF VALVEAPU FUEL FIRE SHUTOFF VALVEENGINE #1 FUEL FIRE SHUTOFF VALVE

WATER FIRE EXT (RT ATTENDANT STATION)DRY CHEMICAL FIRE EXT (LT ATT. STATION)ENGINE #1 HYDRAULIC FIRE SHUTOFFVALVE

CENTER ACCESSORY COMPARTMENT DOORMAIN BATTERIES (CTR ACC COMP.)

FIRE EXT AGENT CONTAINERS ( 800 PSIFOR ENGINE #1)

ENGINE #1 OIL TANK

AIRCRAFT FLAMMABLE MATERIAL LOCATIONS

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DC

-10.10

SPECIAL TOOLS/EQUIPMENTPower Rescue Saw35 Foot Ladder¼ Inch Drive ToolFire Drill IIAIRCRAFT ENTRY

When emergency mode is used to open any passenger door, door will automatically move to full open position.

1. OPERATION OF ALL 8 DOORS WITH NON PUSH BUTTON TYPE: NORMAL MODE-ELECTRICALa. Pull door control handle out of recess.b. Move handle to open position and hold.c. When door is fully open, return handle to neutral detent.

IF DOOR DOES NOT OPEN:2. EMERGENCY MODE-PNUEMATIC (ALL 8 DOORS)a. Hold door control handle at open position.b. Depress and hold emergency opening button, or if emergency override lever is installed, rotate from safe to emergency and hold.c. Move door control handle to emergency position (see dotted PULL handle).

IF DOOR STILL DOES NOT OPEN:d. Push door inward as far as possible and hold. For forward doors, push in area of window.e. Use any available means to pry door upward.

Door with slide attached is very heavy. Required lifting force may exceed 400 pounds.

3. AUXILIARY MODE USING 1/4-INCH DRIVE FITTING (Applicable for forward left fuselage door only.)a. Hold door control handle at open position.b. Insert 1/4-inch drive tool in manual drive fitting and turn counterclockwise until door is open.

Torque applied in excess of 100 inch pounds or 500 RMPs may result in damage.

c. Return door control handle to neutral detent and push inward to stow.

WARNING

WARNING

CAUTION

CLOSE OPEN

FWD MID OVERWING AFT

LEFT FWD DOOR ONLY (SOME AIRCRAFT)

EMERGENCY OPENING BUTTON

AUXILIARY HANDLE

DOOR CONTROL HANDLE

MANUAL DRIVE(LEFT FWD DOORONLY SOME ACFT)

NEUTRALDETENT

POSITIVE STOP AT OPENPOSITION DURINGNORMAL OPERATION

POSITIVE STOP ATCLOSE POSITION

EMERGENCY

OPEN

CLOSE

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-10.11

AIRCRAFT ENTRY-ContinuedWARNING

When emergency mode is used to open any passenger door, door will automatically move to full open position.

4. OPERATION OF ALL 8 DOORS WITH PUSH BUTTON TYPE: NORMAL MODE-ELECTRICALa. Pull door control handle out of recess to disarm escape slide.b. Move door control switch to open and hold.c. When door is fully open, release switch.

IF DOOR DOES NOT OPEN:5. EMERGENCY MODE-PNUEMATIC (ALL 8 DOORS)a. Pull door control handle out of fuselage.b. Rotate emergency override lever from safe position to emergency position and hold.c. Rotate door control handle to emergency position (see dotted PULL handle).

IF DOOR STILL DOES NOT OPEN:d. Push door inward as far as possible and hold. For forward doors, push in area of window.e. Use any available means to pry door upward.

Door with slide attached is very heavy. Required lifting force may exceed 400 pounds.

6. AUXILIARY MODE USING 1/4-INCH DRIVE FITTING (Applicable for forward left fuselage door only.)a. Pull handle out, rotate to free fall position and hold.b. Insert 1/4-inch drive into socket and rotate as indicated until door is open.

Torque applied in excess of 100 inch pounds or 500 RMPs may result in damage.

c. Release door control handle to neutral position.

CAUTION

WARNING

CLOSE OPEN

MID OVERWING AFTFWD

LEFT FWD DOOR ONLYPASSENGER DOORS (8)

EMERGENCYOVERRIDELEVER

EMERGENCY

SAFE

AUXILIARY HANDLE

DOORCONTROLSWITCH

FREE FALL

EMERGENCY

DOOR OPEN

CLOSED

NOTE: When moved to emergency position and held, allows door control handle to be moved to emergency for emergency opening of the door when electrical power is not available.

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DC

-10.12 7. FLIGHT COMPARTMENT ENTRY THROUGH THE AVIONICS COMPARTMENT

a. To open the avionics compartment lower access door, pull down and turn external handle counterclockwise.

b. Stow handle and slide door forward.

c. To open avionics compartment aft access door, turn handle up (clockwise) and push door.

d. To open avionics compartment emergency access door, push to open into flight compartment.

e. Use aft access door from passenger compartment to access flight compartment. Rotate handle up to unlock aft access door.

AIRCRAFT ENTRY-Continued

7cAFT ACCESSDOOR HANDLE

7bLOWERACCESSEXTERNALHANDLE

7aLOWERACCESS DOOR

FLIGHT COMPARTMENT

7eAFT ACCESSDOOR

7dEMERGENCYACCESS DOOR7d

AVIONICSCOMPARTMENT

7eAFT ACCESSDOOR HANDLE

VIEW LOOKING FORWARD

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DC

-10.13

AIRCRAFT ENTRY-Continued8. EXTERNAL CARGO DOOR OPERATION WITH POWER AVAILABLE

a. Press trigger to release handle.b. Pull handle out and up.c. Place door power switch on.d. Place door switch to open.

To prevent door from springing open, manually crank door actuator to the fully closed position prior to manually unlatching.

9. EXTERNAL CARGO DOOR OPERATION WITH MANUAL MODE-NO POWER

a. Press trigger to release handle.b. Pull handle out and up.c. Insert drive tool in latch manual drive fitting and turn drive tool toward unlock position until latches are open.d. Insert drive tool in door manual drive fitting and turn clockwise until door is open.

WARNING

CARGO DOOR

9dDOORSWITCH

9cPOWERSWITCH

LATCHVIEWINGPORT

VENT DOOR

9bDOOR HANDLE

9aTRIGGER

9c3/8 INCH LATCHMANUAL DRIVEFITTING RECEPTACLE

9d3/8 INCH LATCHMANUAL DRIVEFITTING RECEPTACLE

MANUAL OPERATION

LOCK PIN ENGAGEDSYSTEM SAFE

LOCK PINNOT ENGAGEDSYSTEM UNSAFE

CAUTION

BE SURE LOCKPINS ENGAGED

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DC

-10.14

AIRCRAFT ENTRY-Continued10. UPPER CARGO DOOR INTERNAL OPERATION CONVERTIBLE FREIGHTER AIRCRAFT ONLY

NOTE: If installed, pip pin must be removed from locktube to allow unlocking of lockpin handle.

a. To open manually, rotate vent door handle to unlock position.

b. Pull lockpin handle up to unlock position and hold.

c. Insert pipe or hydraulic hand pump handle in latch actuating socket and push down to unlatched position.

d. Release lockpin handle and remove pipe or hand pump handle from latch actuating socket.

e. Place cable loop or hook through latch actuating socket to manually hoist door open.

UNLOCK AND HOLD OPEN WHILE UNLOCKING LATCH MECHANISM

10b, 10dLOCK PINHANDLE

10eLATCHACTUATINGSOCKET

10cLATCH AND HYDRAULICHAND PUMP HANDLE(INSTALLED)

VIEWINGPORT

10aVENTDOOR

UNLOCK

LOCK

PUSH

LATCHED

UNLATCHED

LOCK PIN ENGAGEDSYSTEM SAFE

LOCK PIN NOTENGAGEDSYSTEM UNSAFE

CARGO DOOR VENT

OPEN PRIOR TO OPENING CARGO DOOR

CLOSE AND LOCK PRIOR TO FLIGHT

IF CARGO DOOR WILL NOT OPEN:

ROTATE DOOR CONTROL HANDLE TO “CLOSE” AND RELEASE

OPEN VENT DOOR

CARGO DOOR VENTUNLOCKED LOCKED

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15

CLEARVIEW WINDOW -CUTIN/CHOP OUT


HORIZONTAL STABILIZER JACKSCREWS AND MOTORS ACCESSDOOR



FWD SERVICE ENTRY DOOR

APU COMPARTMENT DOOR

UPPER CARGO DOOR ON CONVERTIBLE FREIGHTER AIRCRAFT ONLY

CENTER CARGO DOOR

PASSENGER ANDSERVICE DOORS


AFT ACCESSORYCOMPARTMENT DOOR

PRESSURE BULKHEAD

FWD CARGO DOOR


AFT CARGO DOOR

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DC

-10.16

ENGINE/APU SHUTDOWN AND AIRCREW EXTRACTION1. ENGINE SHUTDOWN

a. Retard throttles, located on pilot’s console, full aft position.

b. Place fuel control levers, located on pilot’s center console, aft and down to full detent.

c. Place APU fire control switch, located on flight engineer’s left panel to OFF position.

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

e. If engines fail to shutdown: Lift “ENG/FIRE” handle guards, push emergency fire T-handles, located on pilot’s overhead panel, down and forward.

f. In case of engine fire: While holding forward pressure on handle, turn handle clockwise and hold. After 10 seconds, turn handle counterclockwise.

2. APU SHUTDOWN

a. Place the APU master switch, located on flight engineer’s upper forward panel or exterior panel down to the OFF position.

b. In case of APU light illumination: Place APU off and agent arm switch to agent arm UP position. Place CYL 1 to DISCHARGE up position. After 10 seconds place CYL 2 to DISCHARGE up position.


a. Rotate quick release knob on lap belt and remove shoulder harness.

b. Pull seat manual release handle to adjust seat to a recline position in removing crewmembers.

c. Passenger seats are equipped with lap belts only.

1eEMERGENCYT-HANDLES

CENTER OVERHEAD SWITCH PANEL

1aTHROTTLES

1bFUEL CONTROL LEVERS

1dBATTERY SWITCH

1cAPUSWITCH

APU EXTERIOR PANEL

APU FIRE

1cAPU FIRECONTROL SWITCH

UPPERFORWARD PANEL

FLIGHTENGINEERPOSITION

PILOT/COPILOT POSITION (FACING FORWARD)

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-10.

CABIN CONFIGURATION

17

GALLEY

LAVATORY

LAVATORY

ATTENDANT SEAT

ENTRY DOOR 4R42X76” (107X193 CM)

CLOSET

LAVATORY

LAVATORY

ATTENDANT SEAT

ATTENDANT SEAT

CLOSET

ATTENDANT SEAT ATTENDANT SEAT

CLOSET

ATTENDANT SEAT

ATTENDANT SEAT

ATTENDANT SEAT

GALLEY


ENTRY DOOR 3L42X76” (107X193 CM)



ENTRY DOOR 1L32X76” (81X193 CM) ENTRY DOOR 2L

42X76” (107X193 CM)ENTRY DOOR 4L42X76” (107X193 CM)

DC-10 SERIES 10, 30, 30CF, 40 AND 40CFMIXED CLASS (LOWER GALLEY)

270 PASSENGERS222 8-ABREAST SEATING AT 34” (86 CM) PITCH 48 6-ABREAST SEATING AT 38” (97 CM) PITCH

NOTE: All entry doors are emergency exits.

SCALE

0 2 4 6 METERS

0 10 20 FEET

DC-10 SERIES 10, 30, 30CF, 40 AND 40CFALL ECONOMYCLASS

399 PASSENGERSALL ECONOMY 10-ABREAST SEATING AT 34”, 32”, 31”, 30”, AND 29” PITCH


SCALE

0 2 4 6 METERS

0 10 20 FEET

LAVATORY

LAVATORY

LAVATORY

LAVATORY

ATTENDANT SEAT

ATTENDANT SEAT

ENTRYDOOR 1R 32X76”(81X193 CM)

ENTRY DOOR 1L 32X76” (81X193 CM)

ATTENDANT SEAT

ATTENDANT SEAT

CLOSETCLOSET

ATTENDANT SEAT

ATTENDANT SEAT

GALLEYGALLEY

ATTENDANT SEAT

ENTRY DOOR 2R 42X76” (107X193 CM)


ATTENDANT SEAT





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DC

-10.


18

LAVATORY

LAVATORYATTENDANT SEAT

CLOSET

LAVATORY

LAVATORY

ATTENDANT SEAT

ATTENDANT SEAT

ATTENDANT SEAT

CLOSET

ATTENDANT SEAT




DC-10 SERIES 10, 30, 30CF, 40 AND 40CFMIXED CLASS (UPPER GALLEY)

277 PASSENGERS255 9-ABREAST SEATING AT 34” (86 CM) PITCH 22 6-ABREAST SEATING AT 34” (86 CM) PITCH


SCALE

0 2 4 6 METERS

0 10 20 FEET

DC-10 SERIES 10, 30, 30CF, 40 AND 40CFMIXED CLASS (MAIN DECK BAGGAGE)

215 PASSENGERS199 9-ABREAST SEATING AT 34” (86 CM) PITCH 22 6-ABREAST SEATING AT 42” (107 CM)


SCALE

0 2 4 6 METERS

0 10 20 FEET

LAVATORY

LAVATORIES

LAVATORY

LAVATORY

ATTENDANT SEAT

ATTENDANT SEAT

ENTRYDOOR 1R 32X76”(81X193 CM)


ATTENDANT SEAT

ATTENDANT SEAT

CLOSET

CLOSET

ATTENDANT SEAT

ATTENDANT SEAT

MAIN DECK BAGGAGE



ATTENDANT SEAT





ATTENDANT SEAT

LAVATORY

ENTRY DOOR 3R 42X76” (107X193 CM) ENTRY

DOOR 4R 42X76” (107X193 CM)

LAVATORY

ENTRY DOOR 2R 42X76” (107X193 CM) ENTRY

DOOR 1R 32X76”(81X193 CM)

ATTENDANT SEAT


LAVATORY

LAVATORY

LAVATORY

ATTENDANT SEAT

LAVATORY

DC-10T.O

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DC

-10.

CARGO CONFIGURATION

19

DC-10 SERIES 10CF, 30CF, AND 40CFMAIN CABIN CARGO

9 g BARRIER NET

MAIN CARGO COMPARTMENT LENGTH=120 FT 11 INFLAT FLOOR AREA= 2200 SQ FTBULK VOLUME* = 16,760 CU FT

1R 2R 3R 4R 5R 6R 7R 8R 9R 10R 11R 12R 13R 14R 15R

* BULK VOLUME IS WATER VOLUME OF CABINBETWEEN STATIONS NOTED.

STA 495 STA 1946

DC-10 SERIES 10CF, 30CF, AND 40CFMAIN CABIN CARGO (88X108” PALLETS)

1L 2L 3L 4L 5L 6L 7L 8L 9L 10L 11L 12L 13L 14L 15L

MAIN CABIN CARGO VOLUME 30 - 88”X108” PALLETS12,248 CU FT (346.81 CU M)

DC-10 SERIES 10CF, 30CF, AND 40CFMAIN CABIN CARGO (88X125” PALLETS)

MAIN CABIN CARGO VOLUME 22 - 88”X125” PALLETS10,874 CU FT (307.95 CU M)

1R 2R 3R 4R 5R 6R 7R 8R 9R 10R 11R

1L 2L 3L 4L 5L 6L 7L 8L 9L 10L 11L

DC-10 SERIES TYPICAL CARGO SECTION

FULL OPEN=165

PARTIAL OPEN=165

0

0

CEILING AND HEIGHT 88” AT 2NDAND 3RD PASSENGER DOORS

84” FWD AND AFT DROP CEILINGS

CONSTANT SECTION 118.5” RADIUS

GROUNDLINE

102” OPENING

95” BASIC CEILING HEIGHT

66”

193.6 - 188.2”

FULL OPEN

42.4” FOR 70X66” DOOR17.6” FOR 104X66” DOOR

115.7 - 105.0” 125.5”164”

18’ 2”

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DC

-10.20

CARGO CONFIGURATION-ContinuedDC-10 SERIES 10, 30, 30CF, 40 AND 40CFSTANDARD CENTER CARGO COMPARTMENT (LOWER GALLEY)

DC-10 SERIES 30, 30CF, 40 AND 40CFEXTENDED CENTER CARGO COMPARTMENT (UPPER GALLEY)

DC-10 SERIES 10, 10CF, 30, 30CF, 40 AND 40CFSTANDARD CENTER CARGO COMPARTMENT (UPPER GALLEY)

DC-10 SERIES 10, 10CF, 30, 30CF, 40 AND 40CF - CONTAINERS/PALLETSSTANDARD CENTER CARGO COMPARTMENT (UPPER GALLEY)

66X70”CARGO DOORRT SIDE ONLY(6 CONTAINERS)


BULK CARGODOOR LTSIDE ONLY

NOTE: Aircraft may also have extended center compartment. 14 LD3 containers used.

BULKCARGO

66X70” OR 66X104”CARGO DOORRT SIDE ONLY(16 CONTAINERS)


66X70” OR 66X104”CARGO DOORRT SIDE ONLY(16 CONTAINERS)



66X104”CARGO DOORRT SIDE ONLY(5 PALLETS)



NOTE: 5 Pallets and 8 LD3 containers used.

NOTE: 24 LD3 containers used.

NOTE: 26 LD3 containers used.

WELCOME TO TECHNICAL ORDER 00-105E-9, 1 FEBRUARY 2006 ... Segment 18.pdf · mishap response...

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Transcript of WELCOME TO TECHNICAL ORDER 00-105E-9, 1 FEBRUARY 2006 ... Segment 18.pdf · mishap response...