aircraft rescue info

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

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THIS IS SEGMENT 26 COVERING CHAPTERS 26 and 27.

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 Retaining out of date rescue information can negatively affect the user’s operability and outcome of emergencies.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 26 INFORMATION CHANGE NOTICE

None.

TO 00-105E-9

Chapter 26 Cover

NOTE

Chapter 26 contains emergency rescue andmishap response information for the following NATO aircraft:

BEL, FRA, PRT, GEU ALPHA JETITA AMX*

ESP, USA AV-8A/BGBR HARRIER GR MK7GBR HARRIER T-8*GBR HARRIER T-10*GBR SEA HARRIER FA2FRA JAGUAR EGBR JAGUAR GR1GBR JAGUAR GR1A*GBR JAGUAR GR1B*FRA JAGUAR MK 1AGBR JAGUAR T2FRA MIRAGE IV

FRA, ESP MIRAGE FI CT/F-1/C-14FRA MIRAGE F1BFRA MIRAGE 2000 B/N/DFRA MIRAGE 2000C

GEU, ITA TORNADO ADV/IDS*GBR TORNADO F3

GEU, ITA, GBR TORNADO GR MK 1AGBR TORNADO GR4*

* Aircraft information pending

T.O. 00-105E-9

26-1. INTRODUCTION AND USE.

26-2. 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.

26-3. GENERAL ARRANGEMENT.

26-4. Aircraft type designation has been positionedin the upper right corner of the horizontal illustrationfor rapid identification. Additional aids to rapid orien-tation are:

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

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

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

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

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

f. Details are pulled directly from the illus-tration to highlight an area, thus eliminating unnec-essary searching for desired information.

CHAPTER 26

NATO

ATTACK

AEROSPACE EMERGENCY RESCUEAND MISHAP RESPONSE INFORMATION

26-1

ALPHA JETT.O

. 00-105E-9

ALP

HA

JET.

1

AIRCRAFT HAZARDS

ARMAMENTSTATIONS

ARMAMENTSTATIONS

ARMAMENTSTATIONS

27 MMGUN POD

27 MMGUN POD

INTAKEINGESTIONDANGER

HOT ENGINEEXHAUST ANDTURBULENCE

ARMAMENT CONSISTS OF:

TWO UNDER EACH WING FOR UP TO5,510 LB OF STORES.

4 CLUSTER BOMBS.

BOMBS AND ROCKET PACKS OPTIONAL.

OTHER HAZARDS:

POLYTETRAFLUOROETHYLENEACID BATTERIESHYDRAULIC OIL - H-515ENGINE OIL - O-156HIGH PRESSURE GASES - NITROGENEJECTION SEATS WITH CARTRIDGE ASSISTED EQUIPMENTCANOPY SYSTEM HAS MINATURE DETONATING CORD (MDC)

ALPHA JETT.O

. 00-105E-9

ALP

HA

JET.

AIRCRAFT COMPOSITES

2

COMPOSITE MATERIAL: MAN MADEMINERIAL FIBRES

ALPHA JETT.O

. 00-105E-9

ALP

HA

JET.

SPECIAL TOOLS/EQUIPMENTPower Rescue Saw

AIRCRAFT ENTRY

1. NORMAL ENTRY

a. Push on release of external locking lever, located on left side of fuselage below windshield and turn handle clockwise to STOP position.

b. Access to the aft canopy must be gained over the left intake. Push on release of external locking lever and turn lever clockwise to STOP position.

c. Lift up canopy to TOP position.

2. EMERGENCY ENTRY

a. The release mechanism of the minature detonating cord or “MDC” unit is located on both sides of the fuselage in front of intake.

b. Break glass and remove handle.

c. Pull fwd or aft canopy jettison handle to full length to shatter corresponding canopy.

NOTE: The draw cord is very short. Fire MDC with averted face.

3. CUT-IN

a. Cut canopy along canopy frame on all sides.

3

OXYGEN

LITHIUMBATTERIES

FUEL DROP TANK

MAIN FUEL TANKS

FUEL DROP TANKS82 OR 119 GALLONS310 OR 450 LITRESFUEL TYPE: JP-8

DIMENSIONS:WING SPAN - 29’ 10.75”HEIGHT - 13’ 9”LENGTH - 43’ 5”

2cAFTCANOPYJETTISONHANDLE

2cFWDCANOPYJETTISONHANDLE

2aEMERGENCYRELEASEMECHANISM

1aEXTERNALLOCKINGHANDLE

3cCUT-IN

ALPHA JETT.O

. 00-105E-9

ALP

HA

JET.

4

ENGINE SHUTDOWN

1aTHROTTLES

1aIDLE DETENTLEVERS

1bFUELSHUTOFFSWITCHES

BATTERYSWITCH

1cCRASH BAR

1. ENGINE SHUTDOWN

a. Lift idle detent stops, located on left console in the fwd cockpit.

b. Place throttles aft to OFF position.

c. Lift covers of the fuel shutoff switches, located on left console behind the throttles, and place switches to OFF position.

d. Depress crash bar, located above the right console in the fwd cockpit. Crash bar is marked yellow and black and disconnects electrical system.

ALPHA JETT.O

. 00-105E-9

ALP

HA

JET.

5

EJECTION SEAT FAMILIARIZATION1. EJECTION SEAT FAMILIARIZATION

NOTE: The Alpha Jet uses a Martin Baker ejection seat. There may be some variations to safetying the seat. The graphic identifies critical components and safety pin locations for safetying and crew extraction.

a. Safety pins are pip pin type.

b. Safety pins are clip type.

c. Lap belt buckle secures crew member by lap belt and shoulder harness.

d. Uncovered handle is a leg restraint release handle.

e. Orange handle is a central harness quick release for the release of all restraints.

NOTE: Emergency harness release handles can be located on the right hand side of the seat, are colored orange, and also release all restraints when pulled up to the STOP position. These handles may incorporate an explosive charge to sever the parachute line at the guillotine device.

1aFACE CURTAINSAFETY PIN

1cLAP BELT BUCKLE

1aLOWER EJECTION(D RING) HANDLEAND SAFETY PIN

1bTOP CHARGE MECHANISMSAFETY PIN (PIN IS ROUTEDTHROUGH SEAR)

1aDROGUE GUN MECHANISMSAFETY PIN (PIN IS ROUTEDTHROUGH SEAR)

1bCANOPYFRAGILIZATIONSAFETY PIN

1eORANGEHANDLEFOR CREWRELEASE

1dUNCOVERED HANDLEFOR CREW RELEASE

FR VARIATION

ALPHA JETT.O

. 00-105E-9

ALP

HA

JET.

6

EJECTION SEAT SAFETYINGAND AIRCREW EXTRACTION

1bRIMMEDRELEASEBUTTONAND1dGROUNDSAFETYLEVER

1. EJECTION SEAT SAFETYING

a. Install canopy fragilization safety pins in three locations.

b. Pulled rimmed release button in the ground safety lever, located on the right side of the seat, out to STOP position.

c. If applicable, install safety pin in lower ejection handle.

d. Lift ground safety lever up to level position until release buttton engages.

2. AIRCREW EXTRACTION

a. Pull yellow snap from harness quick release box, rotate outer assembly 1/4 turn clockwise to STOP position and strike firmly to open.

b. Press locking device, located in the emergency release handle lower right side of the seat and life emergency release handle up to STOP position.

c. Squeeze restraint release device, located on pilot’s left thigh, to disconnect the dinghy line.

d. Disconnect personnel leads.

2cDINGHYRELEASECONTROL

2bYELLOW SNAP

2bEMERGENCYRELEASEHANDLE

1aCANOPYFRAGILIZATIONSAFETY POINTS

2aHARNESSQUICKRELEASEBOX

2cLOWEREJECTIONHANDLE

2cRESTRAINTRELEASECONTROL

2dPERSONNEL LEADSDISCONNECT FOR OXYGEN,RADIO, ANTI-G SYSTEMS,AND SURVIVAL PACK

BE VARIATION

GE, PO VARIATION

AMXT.O

. 00-105E-9

AM

X. 1

The aircraft information is pending release.

AV-8BT.O

. 00-105E-9

AV

-8B.1

The aircraft information is located in Chapter 20 containing US Navy aircraft.

HARRIER GR7T.O

. 00-105E-9

HA

RR

IER

GR

7.

AIRCRAFT DIMENSIONS

WING SPAN 25’ 3” (7.70M)

HEIGHT12’ 2”(3.71M)

LENGTH 46’ 6”(14.17M)

1

TYPICAL HARRIER

HARRIER GR7T.O

. 00-105E-9

HA

RR

IER

GR

7. 2

AIRCRAFT HAZARDS

SIDEWINDERMISSLE

EXTERNALFUEL TANK

GUNPODS

CENTERPYLON

FUEL ANDWEAPONSPYLONS

FUEL ANDWEAPONS PYLONS

CHAFF AND FLAREDISPENSERS

A variety of weapons or stores may be carried externallyon pylons.

Weapons or stores may be: Fuel tanks, bombs, rockets,gunpods or missles.

NOTE: Sidewinder AIM-9L Missle (up to 6 may be carried). Do not look directly at AOTD windows: - Energy beam - Liquid nitrogen - Mercury thallium

All forward areas in danger of weapons firing and all weapons should be considered loaded and armed.

OTHER HAZARDS:Battery acidAssisted escape systemBeryllium +beryllium oxidesCartridge operated equipmentComposite materials - man made mineral fibresCoolanolDimethylformamide (Strobe power pack)Ejector release unitsMercury (Temperature bulbs)Miniature Detonating Cord (MDC)Niemonic steel (Heat shields)PolytetrafluoroethyleneSonar locator beacon(s) (1-Lithium battery)ThalliumThorium fluorideZinc selenide (GR7/T10 only)Fuel: AvturHydraulic oil: OM-15High pressure gases: Nitrogen/AirEngine oil: OX-38Oxygen: Molecular sieve concentration system

WARNING

HARRIER GR7T.O

. 00-105E-9

HA

RR

IER

GR

7.3

RCN RCN

RCN

ENGINE JETEFFLUX MAYBE IN ANYDIRECTION

OXYGENENGINEAIRINTAKE

ENGINEOIL TANK

EXTERNALFUEL TANK

FUEL TANKS

CANOPYMDC BATTERY

FLARES

RCN

FUEL TANKS

HYDRAULIC FLUID RESERVOIRS

AIRCRAFT HAZARDS-Continued

RCNs (Reaction Control Nozzles) may be dangerously hot.

Aircraft structure (nose and wings) contain carbon fibre which causes toxic fumes in fire.

Microwave hazard from various equipment.

Strobe lights are intense.

Exhaust nozzles may move.

High voltage electrical systems.

NOTE: Up to four external fuel tanks may be carried.

WARNING

HARRIER GR7T.O

. 00-105E-9

HA

RR

IER

GR

7. 4

SPECIAL TOOLS/EQUIPMENTPower Rescue SawCrash AxLadder

AIRCRAFT ENTRY

1. NORMAL ENTRY

NOTE: Normal entry controls are located on the right side fuselage forward of intake.

a. Press thumb release button and pull normal control handle forward.

b. Pull down on footstep to gain access to cockpit, if ladder is not used, and push buttons to release steps.

2. EMERGENCY ENTRY

NOTE: Emergency controls are located on both sides of the fuselage forward of intakes.

a. Depress thumb plate.

b. Grasp wire loop operating handle, located inside thumb plate.

c. Face away from aircraft.

d. Step away from aircraft and take up cable slack.

e. Pull wire loop operating handle sharply forward to shatter canopy.

3. CUT-IN

a. Canopy is made of acrylic plastic and may be cut with a power rescue saw or crash ax. Cut along the canopy frame.

SAFETY PINSTOWAGE

FIRE ACCESSBOTHSIDES

1bFUSELAGESTEPS

KEEP CLEAROF ENGINEAIR INTAKE

1bFOOTSTEP

1aNORMAL ENTRYHANDLE WITHTHUMB RELEASEBUTTON

2aTHUMBPLATE

2bWIRE LOOPOPERATINGHANDLE(STOWEDPOSITION)

2eWIRE LOOPOPERATINGHANDLE

2aTHUMBPLATERELEASEBUTTON

HARRIER GR7T.O

. 00-105E-9

HA

RR

IER

GR

7.5

ENGINE SHUTDOWN1. ENGINE SHUTDOWN

a. Move throttle manual fuel, located on left console, back to OFF.

b. Move LP fuel manual shutoff lever, located on lower left console, back to OFF.

c. Move battery master switch, located on upper right console, to OFF.

1cBATTERYMASTERSWITCH1a

THROTTLE MANUAL FUEL

NOZZLE CONTROLFUEL PUMPS

OXYGENSHUTOFF

1bLP FUELMANUALSHUTOFFLEVER

INTERNAL MDCHANDLE

JETTISONSWITCH

MASTERARMAMENTSAFETYSWITCH

LATE ARMSWITCH

FIREWARNINGLIGHTS

ECM SWITCHES

CANOPY UNLOCK HANDLE

SAFETY PINSTOWAGE

HARRIER GR7T.O

. 00-105E-9

HA

RR

IER

GR

7.6

SEAT SAFETYING ANDAIRCREW EXTRACTION1. SEAT SAFETYING

a. Insert main gun sear safety pin.

b. Put Safe/Arm handle to SAFE by turning handle fully up.


a. Remove face mask.

b. Release PEC by pressing trigger and pulling up to free from seat.

c. Release PSP by pressing plungers on each side and lay aside.

d. Release leg restraint lines by pulling leg restraint lever to rear.

e. Release QRF by turning quick release button and pressing, then pull out lugs.

f. Remove crewmember.

g. Fit remaining pins to render ejection seat safe.

1a

1b

2a

2g

2f

2g

2b

2c

2d

2g

EMERGENCYOXYGENCYLINDER

2e

HARRIER T8T.O

. 00-105E-9

HA

RR

IER

T8.


1

HARRIER T10T.O

. 00-105E-9

HA

RR

IER

T10.


1

SEA HARRIER FA2T.O

. 00-105E-9

SE

A H

AR

RIE

R FA

2.

AIRCRAFT PAINT SCHEME

1

SEA HARRIER FA2T.O

. 00-105E-9

SE

A H

AR

RIE

R FA

2.2

AIRCRAFT DIMENSIONS

LENGTH 45.6’ (14.17 M)

HEIGHT 11’ 10”(3.62M)

WING SPAN 25.3’ (7.7 M)

NOTE: The Sea Harrier FA2 is a modified Harrier GR 7 and US version AV-8B Harrier II and having 1 crewmember.

SEA HARRIER FA2T.O

. 00-105E-9

SE

A H

AR

RIE

R FA

2.

1. HAZARDS

The Sea HarrierFA2 and Harrier GR7 have morehazards than any other fixed-wing aircraft. Apart fromall normal dangers there are a number of reactioncontrol-ducts and control surfaces which constitutedanger at all times.

A Reaction control ducting nozzles in nose, tail andboth wing tips. Movement on the control columncauses shutters to open, close and rotation of nozzlesresulting in emission of extremely hot air. Beware ofthe danger to fingers from these shutters.

B Never approach this aircraft from the rear, alwaysapproach within full view of the pilot within the safearea shown in the graphic.

C Beware of all intakes and exhausts.

D Assisted Escape Systems - Mild detonating cordcanopy and various explosive jettison mechanisms.

E Beware of external armaments fitted, high energyignition units and radiation hazards.

2. OTHER HAZARDOUS AREAS

a. Oil Breather Fins are extremely sharp fins projectingfrom under the starboard side of the aircraft fuselageand can cause injury to personnel.

b. The complete Flying Tail plane pivots and when in theflying attitude, there is a hole through the fuselage.Should the tail plane be depressed, it acts as aguillotine through this hole. Keep away from this area.

c. Nose Wheel Doors will close automatically with grea force on start up. Keep clear of this area during startup.

AIRCRAFT HAZARDS

WARNING

3

D

A

CE

E A

A

BA

LEFT ROLL NOZZLES

YAW NOZZLES

AFT PITCH NOZZLES

RIGHT ROLL NOZZLES

FORWARD PITCH NOZZLES

SEA HARRIER FA2T.O

. 00-105E-9

SE

A H

AR

RIE

R FA

2. 4

AIRCRAFT HAZARDS-Continued2. OTHER HAZARDOUS AREAS

d. Armament. This aircraft is capable of carrying avariety of weapons and a combination of differentweaponry at the same time. Normal armamentprocedures and safety rules must therefore beadhered to, unless it is specifically stated that theaircraft is not armed.

e. Miniature Detonating Cord (MDC). The cockpitcanopy is fitted with an MDC which is a potentialhazard to the unwary. The safety pin is stowed inthe unit casing at the rear of the canopy. (Refer toRAF document AP 101B-4801-12B Part 1Chapter 8or equivalent.)

f. Assisted Escape System and associated explosive-operated jettison mechanisms fitted to aircraft are apotential source of lethal injury to personnel anddamage to aircraft. Safety devices in the form ofsafety pins, levers and switches are provided whenthe aircraft is on the ground to safeguard againstthe many dangers.

g. Cockpit precautions are to be fully observed beforeentering a cockpit or starting work on an aircraft, itis the responsibility of the individual to ensure that:(1) All safety devices are correctly fitted. (2) Nounits or switches with which the individual in notconversant are touched. (3) Prior to removing theanchorage pins of the BTRU and/or drogue gun, theunits must be unloaded.

h. LOX is a potential hazard on deck if not treatedcorrectly (N/A to GR7).

i. Canopy opening is on the left or port side of thefuselage and is of the push-latch pull-out type.

80’ (24.6M)

125’ (38.1M)

150’ (45.7M)

40’ (12.3M)

A

B

A: TEMPERATURE DROPS TO 50 DEGREES CENTIGRADE

SAFE AREA. This area may be occupiedwith caution for starting and for adjustmentswhen ground idling only (nozzles aft).

50’ (15.24M)

80’ (24.6M)

NOZZLES FROM 45 DEGREE DOWNWARDS

NOZZLES DOWN50’ (15.24M)

NOTE:Personnel should avoid being out of thepilot’s view during vertical takeoff. Verticallanding or hovering unless they are fixed.

WARNING

This aircraft is more dangerousthan conventional fixed-wingaircraft because the exhaustsystem can be rotated.

SEA HARRIER FA2T.O

. 00-105E-9

SE

A H

AR

RIE

R FA

2.

HAZARD TYPE ITEM QUANTITY LOCATION

Acid - Sulphuric Batteries 2 Between FR's 38-39

Aircraft Assisted Escape Systems Egress System 1 Cockpit

AL 36 Windscreen Wash Fluid Tank 4.45 L Nose Area

Amorphous silica On Aircraft

Asbestos 3+ trace Heat Shields on Tail PitchYaw Nozzle Bay

Engine Heat ShieldsWater Tanks Muffs (FR 29)

Trace in Engine Seals

Avcat - FS 11 NATO F-44 Fuel 2875 L Internal3136 L External

Fuel System

Avtur F-34 FuelFuel 2875 L Internal

3136 L ExternalFuel System

Beryllium - Beriliua (Beryllium Oxides) 2 (traces) Rear Equipment Bay (FR 33-37)Receiver/Processor

Rear Fin Total Temperature Probe

Cadmium and Cadmium Oxide Traces All Electronic Components

Chaff Dispenser 1 FR's 36-38 ALE40 Panel Undersideof A/C

Coolanol Approx. 2 L Reservoir at FR33B(S) Piping DownStarboard Side to Nose Cone

Ejector Release Units (ERJs) 7 Maximum 7 on Fuselage & Wing Pylons5 on CBLS on Sea Eagle Launches

Flare Dispenser 1 FRs 36-38 ALE 40 Panel Undersideof A/C

Gaseous Tritium Light Sources Lights 4 Beta Lights on Mass Flag (cockpit)Yaw Vane (nose)

Emergency Light Switch (cockpit)Nose Cone Locking Handle

AIRCRAFT DATA AND HAZARD LISTHAZARD LISTAIRCRAFT DATA

VSTOL Fighter Attack Aircraft One Rolls-Royce Pegasus Mk.104/106 vectored thrust turbofan Military: 1 crew Aircraft Weight: 13,862 lbs. (6,287 Kgs)

Fires resulting from this type of aircraft crash may produce toxic fumes which are hazardous to health.

Personal Protective Equipment (recommendations made by the GRB RAF Royal Navy to be worn at crash site):

Standard No. 3 (combat) dress. Civil Emergency Services normal uniform with appropriate weather protection. Safety helmet (as required).

5

WARNING

SEA HARRIER FA2T.O

. 00-105E-9

SE

A H

AR

RIE

R FA

2.

AIRCRAFT DATA AND HAZARD LIST-ContinuedHAZARD LIST

Glass Reinforced Plastics Numerous Throughout A/C

Liquid Oxygen (LOX) 5 L Oxygen System Bottle Aft of MainU/C if fitted

Lithium (Non Rechargeable Batteries) Batteries 2 x 'AA' in EachLocation

Rear Equipment Bay Inside BCLUand in RWR PLU in Cockpit

Mecury Thallium 4 x Trace Aquisition Sidewinder andSidewinder Heads

Minature Detonating Cord (MDC) Canopy 1 Canopy Jettison System

Nimonic Steels Heat Shields

Nitrogen Compressed 8 up to 3300 PSI 6 x Accumulators + 2 x Blow DownBottles

OM-15 Hydraulic Oil 30 L Hydraulic Oil System

OX-38 Engine Oil 20 to 31.75 Pts Engine Oil System

Oxygen Compressed Gas 2100 L Oxyen System Bottle aft of main U/Cif fitted

Polytetrafluoroethylene (PTFE) Trace All A/C Various Seals

Sonar Locator Beacon(s) Sonor Beacon 1 Lithium Battery FRs 1-2S

Weapon Load (if fitted) Weapon(s) Mission Variable Wings + Fuselage Stations andFuselage Gun Pods

6

SEA HARRIER FA2T.O

. 00-105E-9

SE

A H

AR

RIE

R FA

2.7

AIRCRAFT HAZARDS

SIDEWINDERMISSLE

EXTERNALFUEL TANK

GUNPODS

CENTERPYLON

FUEL ANDWEAPONSPYLONS

FUEL ANDWEAPONS PYLONS

CHAFF AND FLAREDISPENSERS


Weapons or stores may be: Fuel tanks, bombs, rockets,gunpods or missles.

NOTE: Sidewinder AIM-9L Missle (up to 6 may be carried). Do not look directly at AOTD windows: - Energy beam - Liquid nitrogen - Mercury thallium


OTHER HAZARDS:Battery acidAssisted escape systemBeryllium +beryllium oxidesCartridge operated equipmentComposite materials - man made mineral fibresCoolanolDimethylformamide (Strobe power pack)Ejector release unitsMercury (Temperature bulbs)Miniature Detonating Cord (MDC)Niemonic steel (Heat shields)PolytetrafluoroethyleneSonar locator beacon(s) (1-Lithium battery)ThalliumThorium fluorideZinc selenide (GR7/T10 only)Fuel: AvturHydraulic oil: OM-15High pressure gases: Nitrogen/AirEngine oil: OX-38Oxygen: Molecular sieve concentration system

WARNING

SEA HARRIER FA2T.O

. 00-105E-9

SE

A H

AR

RIE

R FA

2.8

RCN RCN

RCNENGINE JETEFFLUX MAYBE IN ANYDIRECTION

OXYGENENGINEAIRINTAKE

ENGINEOIL TANK

EXTERNALFUEL TANK

FUEL TANKS

CANOPYMDC BATTERY

FLARES

RCN

FUEL TANKS



RCNs (Reaction Control Nozzles) may be dangerously hot.

Aircraft structure (nose and wings) contain carbon fibre which causes toxic fumes in fire.

Microwave hazard from various equipment.

Strobe lights are intense.

Exhaust nozzles may move.

High voltage electrical systems.

NOTE: Up to four external fuel tanks may be carried.

WARNING

SEA HARRIER FA2T.O

. 00-105E-9

SE

A H

AR

RIE

R FA

2.


FIRE ACCESS

TAIL UNDERSIDE

CHAFF/FL

ARE

APU

EXHAUST

INTAKE

9

AIRCRAFT SPINE

RIGHTSIDE

SEA HARRIER FA2T.O

. 00-105E-9

SE

A H

AR

RIE

R FA

2.10


AIRCRAFT ENTRY

1. NORMAL ENTRY

NOTE: Normal entry controls are located on the right side

fuselage forward of intake.

a. Press thumb release button and pull normal controlhandle forward.

b. Pull down on footstep to gain access to cockpit, if ladderis not used, and push buttons to release steps.

2. EMERGENCY ENTRY (SEA HARRIER vs. GR7)

NOTE:Although the Harrier GR7 rescue procedure is similiar tothe Sea Harrier, insure rescue crews are fully aware onspecific differences. Emergency controls are located onboth sides of the fuselage forward of intakes.

a. Depress thumb plate.

b. To detonate the miniature detonating cord (MDC), pullthe handle on either side of the cockpit canopy. (Thejettison cord is 10 feet long [Harrier GR7 is 3 feetminimum].

c. Grasp wire loop operating handle, located inside thumbplate and face away from aircraft to prevent injury fromshattering pieces of the canopy.

d. Step away from aircraft and take up cable slack.

e. Pull wire loop operating handle sharply forward to shattercanopy.

SAFETY PINSTOWAGE

FIRE ACCESSBOTHSIDES

1bFUSELAGESTEPS

KEEP CLEAROF ENGINE AIRINTAKE

1bFOOTSTEP

1aNORMAL ENTRYHANDLE WITHTHUMB RELEASEBUTTON

2aTHUMBPLATE

2bWIRE LOOPOPERATINGHANDLE(STOWEDPOSITION)

2eWIRE LOOPOPERATINGHANDLE

2aTHUMBPLATERELEASEBUTTON

SEA HARRIER FA2T.O

. 00-105E-9

SE

A H

AR

RIE

R FA

2.

EMERGENCY ENTRY-Continued

NORMAL CANOPY OPENING

MDC OPENING

MDC OPENING

2. EMERGENCY ENTRY-Continued

NOTE: See applicable graphics for normal canopyopening and MDC locations.

3. CUT-IN

a. Canopy is made of acrylic plastic and may be cut with a power rescue saw or crash ax. Cut along the canopy frame.

11

MDC

SEA HARRIER FA2T.O

. 00-105E-9

SE

A H

AR

RIE

R FA

2.

MDC PATTERN(EDGE OF TRANSPARENCY AND OVERHEAD)

CANOPY MDC SYSTEM SAFETY PIN(FLIGHT STOWAGE POSITION)

SAFETY PIN(SERVICING POSITION)

FIRING UNIT

SEAT/MDC INTERCONNECTION(SEAT STRIKER HITS LEVER)

MDC OPERATINGCABLE CONDUITS

INTERNAL FIRING HANDLE(AND SAFETY PIN)

EXTERNAL FIRING HANDLEACCESS (LT SHOWN; RT SIMILAR)

HINGED DOOR

EXTERNAL FIRING HANDLE

STOWED CABLE

DOOR LATCH RELEASE THUMB BUTTON

12

SEA HARRIER FA2T.O

. 00-105E-9

SE

A H

AR

RIE

R FA

2.13

COCKPIT EQUIPMENTMDC FIRING HANDLE (AND SAFETY PIN)

SAFETY PIN STOWAGE

SAFETY PIN STOWAGE

SEAT HEIGHTADJUSTMENT SWITCH

PEC SEAT PORTIONDUST COVER STOWAGE

SEAT FIRINGHANDLE PIN

MDC FIRINGHANDLE PIN

MANUAL SEPARATION PIN

ROCKET INITIATION PINEJECTION GUN PIN

(ANY ORDER)

CANOPY MANUALUNLOCK HANDLE

FIRE WARNING LIGHTS

SEA HARRIER FA2T.O

. 00-105E-9

SE

A H

AR

RIE

R FA

2.14

MASTER ARMAMENT SAFETY SWITCH

UNDERVOLT/OVERLOADTEST BUTTON AND LIGHT

GTS MODESELECTOR

ENGINE & APU STARTERBUTTON & COVER FLAP

VOLTMETERAC RESET BUTTON

BATTERYTEST/EXTERNAL POWER SWITCH

ELECTRICAL PANEL

1cBATTERY MASTERSWITCHES

1aHP COCK/THROTTLE LEVER

THROTTLE FRICTION DAMPER

AFTS POINTER

ADJUSTABLE FULL THROTTLE STOP (AFTS) CONTROL

HP COCK OFF TRIGGER

LIMITERS SWITCH STRIKER

SPRINGLOADEDFULLTHROTTLESTOP

LIMITERSSWITCH

THROTTLE QUADRANT

MANUAL RELIGHT BUTTON

ENGINE SHUTDOWN

1bLP FUELMANUALSHUTOFFLEVER

1. ENGINE SHUTDOWNa. Move HP cock/throttle lever, located on left console, aft to

OFF. Friction damper may have to be loosened.

b. Move LP fuel manual shutoff lever, located on lower leftconsole, aft to OFF.

c. Move battery master switches, located on upper rightconsole, to OFF.

SEA HARRIER FA2T.O

. 00-105E-9

SE

A H

AR

RIE

R FA

2.15

THRO

TTLE

ENGINE SHUTDOWN-Continued

BATT

ERY

MAS

TERS

PEC

LP F

UE

L C

OC

K

MASTE

R ARMAM

ENT

SEA HARRIER FA2T.O

. 00-105E-9

SE

A H

AR

RIE

R FA

2.16


a. Make the ejection seat safe by insertingthe safety pin under the seat firing handlelocated at the front lower portion of theseat.

b. Make the ejection seat safe by placing thesafety pin in the main gun sear located atthe top center of the seat.

c. Make the ejection seat safe by placingthe safety pin in the rocket initiator searlocated on the upper left side of the seat.

d. Install safety pin in the manual separationsear located on the lower right side of theseat.

e. Release the pilot’s oxygen mask; do notremove helmet.

f. Release the dinghy clip on the pilot’s leftthigh (Martin-Baker type clip).

g. Release the pilot’s Personal EquipmentConnector (PEC) at the left hand side ofthe cockpit; this should also release theleg restraining straps. Check and if notreleased, do so manually by operating theclip on both legs (Martin-Baker type clip).

h. Hold the pilot back into the seat andrelease the harness (turn the knob on theQRB a quarter turn to release the straps).Place the straps clear of the pilot and liftcrew clear of the cockpit.

AIRCREW EXTRACTION

1bEJECTION GUNSEAR PIN

1aSEAT FIRINGHANDLE SAFETY PIN

1cROCKETINITIATORSEAR PIN

1dMANUAL SEPARATION SEAR PIN

SEA HARRIER FA2T.O

. 00-105E-9

SE

A H

AR

RIE

R FA

2.

AIRCREW EXTRACTION-Continued

17

MDC

MAIN GUN PIN & SEAR

MAIN GUN PIN & SEAR

SAFETY

PIN

LEG RESTRAINT

JAGUAR ET.O

. 00-105E-9

JAG

UA

R E

.1

AIRCRAFT HAZARDSAMMUNITION BOX

GUN

WEAPONS PYLONS

AIRCRAFT DIMENSIONS

WING SPAN 28’ 6” (8.69 M)LENGTH 55’ 2.5” (16.83 M)HEIGHT 16’ .5” (4.89 M)


Weapons or stores may be: Fuel tanks, bombs, rockets,and missles.


OTHER HAZARDS:Battery acidAssisted escape systemBeryllium +beryllium oxidesBromochlorodifluoromethane (BCF Fire Extinguishant)Bromotrifluoromethane (BTM Fire Extinguishant)Cartridge operated equipmentChlorobromoethane (Fire Extinguishant)Chaff DispenserDimethylformamide (Strobe power pack)Ejector release unitsFlare dispenserLithium (Batteries)Mercury (Temperature bulbs)Methyl Bromide (Fire Extinguishant)Miniature Detonating Cord (MDC)PolytetrafluoroethyleneRadioactive sourcesSonar locator beacon(s) (1-Lithium battery)ThalliumTritium light sourcesFuel: AvturHydraulic oil: OM-15High pressure gases: NitrogenEngine oil: OX-26Oxygen: LOX

WEAPONS PYLONS

GUN

WARNING

JAGUAR ET.O

. 00-105E-9

JAG

UA

R E

.


2

CARTRIDGESSEATS AND CANOPIES

HYDRAULIC OIL TANKS

LIQUID OXYGEN(access by the right side)

ENGINE SUCTION AREA

ENGINE BLAST AREA

ARRESTER HOOK

ACCESS GATES TOEXTINGUISHER ON GROUND

FUEL TANKS F 341110 US GALS (4200 LITRES)

BATTERY

JAGUAR ET.O

. 00-105E-9

JAG

UA

R E

.3

JETTISONABLECANOPIES

FOOT HOLDS

FOOT HOLDS


AIRCRAFT ENTRY

1. NORMAL ENTRY

a. On left side of fuselage, press down streaks or release button, to release handle.

b. Pull release handle and lift canopies.

2. EMERGENCY ENTRY

a. On left or right side of fuselage, break window.

NOTE: Canopy must be locked prior to jettison.

b. Pull corresponding handle to jettison corresponding canopy.

3. CUT-IN

a. Use power rescue saw to cut-in canopy. Cut all four sides.

2bCANOPY JETTISON HANDLES

2aCANOPY JETTISONWINDOW

1aSTREAK ORRELEASE BUTTON

1bRELEASEHANDLE

JAGUAR ET.O

. 00-105E-9

JAG

UA

R E

.4

ENGINE SHUTDOWN, SAFETY ARMAMENTAND ELECTRIC POWER SHUTDOWN1. ENGINE SHUTDOWN

a. Pull throttle, located on left console, to AFT position.

b. Push throttle levers and set throttle in aft STOP position.

c. Lift both fuel shutoff switch covers, located on center pedestal, and place switches in DOWN position.

2. SAFETY ARMAMENT

a. Turn safety armament selector, located on center console, to the left on the SAFETY position.

3. ELECTRIC POWER SHUTDOWN

a. Lift electric power crash stripe, located on left aft console, to the AFT position.

1aTHROTTLE

1bTHROTTLELEVER

1cFUEL SHUTOFFSWITCH COVERS

1cFUEL SHUTOFFSWITCHES

2aARMAMENT SAFETY SELECTOR

3aCRASHSTRIPE

JAGUAR ET.O

. 00-105E-9

JAG

UA

R E

.5

SEAT SAFETYING ANDAIRCREW EXTRACTION

1. SEAT SAFETYING

NOTE: This ejection seat and canopy system is safetied with safety pins or clips.

a. Safe the gun, located top of seat.

b. Safe the extractor gun, located on left side of seat.

c. Safe the high handle, located above face curtain.

d. Safe the lower handle, located center forward seat bucket.

e. Safe the canopy ejection pin located on the left side at the top of the seat.

f. Set “Normal” and “Emergency” oxygen commutator taps to OFF.


a. Pull uncovered handle, located on the left side of seat, for parachute separation.

b. Lift orange lever, located on the left side at bottom of the seat, for crewmember separation.

c. Release ventral (restraints) buckle by the quick disconnect handle to free crewmember from harnesses.

d. Pull up the crewmember by the harness straps.

1cHIGHEJECTIONHANDLE

1dLOWEREJECTIONHANDLE

1cHIGH EJECTIONHANDLE SAFETYPIN

1aGUN SAFETY PIN

1bEXTRACTORGUN 1e

CANOPY EJECTIONSAFETY PIN

1eCANOPY INITIATOR

1bEXTRACTOR GUN SAFETY PIN

1f“NORMAL” OXYGENCOMMUTATOR

1f“EMERGENCY” OXYGENCOMMUTATOR

2aUNCOVERED HANDLE

2bSEAT SEPARATION LEVER

1dLOWEREJECTIONHANDLESAFETY PIN

VENTRALBUCKLE

2cQUICKDISCONNECTHANDLE


JAGUAR GR1T.O

. 00-105E-9

JAG

UA

R G

R1. 1

AIRCRAFT HAZARDS

Ammunition box containing150 rounds of ammunition

30 MMADENCANONS

WEAPONS PYLONS CAN CARRY UP TO 2,500 LBS (1134 KG)


Weapons or stores may be: Fuel tanks, bombs, rockets,missles, and reconnaissance camera pack.


OTHER HAZARDS:Battery acidAssisted escape systemBeryllium +beryllium oxidesBromochlorodifluoromethane (BCF Fire Extinguishant)Bromotrifluoromethane (BTM Fire Extinguishant)Cartridge operated equipmentChlorobromoethane (Fire Extinguishant)Chaff DispenserDimethylformamide (Strobe power pack)Ejector release unitsFlare dispenserLithium (Batteries)Mercury (Temperature bulbs)Methyl Bromide (Fire Extinguishant)Miniature Detonating Cord (MDC)PolytetrafluoroethyleneRadioactive sourcesSonar locator beacon(s) (1-Lithium battery)ThalliumTritium light sourcesFuel: AvturHydraulic oil: OM-15High pressure gases: NitrogenEngine oil: OX-26Oxygen: LOX

WARNING

AIRCRAFT DIMENSIONS


JAGUAR GR1T.O

. 00-105E-9

JAG

UA

R G

R1.

2


AIRCRAFT ENTRY

1. NORMAL ENTRY

a. Operate normal canopy release handle located at lower left corner of left wind shield.

b. Lift up canopy into LOCKED position. Canopy is hinged at rear.

2. EMERGENCY ENTRY

a. Break protective window of emergency canopy release handle, located on port and starboard side of canopy.

b. Pull black and yellow handle. Canopy will jettison.

3. CUT-IN

a. Canopy is made of acrylic plastic and may be cut with a power rescue saw or crash ax. Cut along the canopy frame. Wind screen is bullet proof.

FUEL TANKS

FUEL TANKS

HYDRAULICFLUIDRESERVOIRS

BATTERY (Access via nosewheel bay)

OXYGEN CYLINDER(Located at seat position)

LIQUID OXYGENCONTAINERS

LASER SYSTEM(In nose)

2a, 2bPROTECTIVE WINDOW WITHEMERGENCY CANOPYRELEASE HANDLE

1aNORMAL CANOPYRELEASE HANDLE

JAGUAR GR1T.O

. 00-105E-9

JAG

UA

R G

R1.

3


a. Pull HP cocks throttle, located on left console, back to OFF.

b. Place low pressure fuel cocks, located on center console, down to CLOSED.

c. Break indicator wire and move crash switch, located on aft left console, REARWARD.

1aHP COCKSTHROTTLE

1bLOW PRESSUREFUEL COCKS

1cINDICATOR WIRE

1cCRASH SWITCH

ARMAMENTSAFETYSWITCH

EJECTIONSEAT PINSTOWAGE

COCKPIT

JAGUAR GR1T.O

. 00-105E-9

JAG

UA

R G

R1.

4

SEAT SAFETYING ANDAIRCREW EXTRACTIONNOTE: The Jaguar GR1 uses a Martin-Baker IN9B MK II zero-zero ejection seats. In two seat versions, the aft seat is 15” or 38 cm higher than the forward seat.

1. SEAT SAFETYING




b. Operate PEC.

c. Release PSP.

d. Operate toggle switch to release leg restraints and pull lines through garters.

e. Release QRF and turn and press box firmly. Lay clear all harness and restraints.

f. Remove aircrew member.

g. Install remaining safety pins into ejection seat.

1aMAIN GUN SEARWITH SAFETYPIN HOLE

1aMAIN GUN PLUNGER

1aMAIN GUNWITH CHARGE

1aSAFETY PIN

1a

2a

2e

2c2b

2d

JAGUAR GR1AT.O

. 00-105E-9

JAG

UA

R G

R1A

.


1

JAGUAR GR1BT.O

. 00-105E-9

JAG

UA

R G

R1B

.


1

JAGUAR MK1AT.O

. 00-105E-9

JAG

UA

R M

K1A

. 1

AIRCRAFT HAZARDS

Ammunition box containing150 rounds of ammunition

30 MMADENCANONS

WEAPONS PYLONS CAN CARRY UP TO 2,500 LBS (1134 KG)




OTHER HAZARDS:Battery acidAssisted escape systemBeryllium +beryllium oxidesBromochlorodifluoromethane (BCF Fire Extinguishant)Bromotrifluoromethane (BTM Fire Extinguishant)Cartridge operated equipmentChlorobromoethane (Fire Extinguishant)Chaff DispenserDimethylformamide (Strobe power pack)Ejector release unitsFlare dispenserLithium (Batteries)Mercury (Temperature bulbs)Methyl Bromide (Fire Extinguishant)Miniature Detonating Cord (MDC)PolytetrafluoroethyleneRadioactive sourcesSonar locator beacon(s) (1-Lithium battery)ThalliumTritium light sourcesFuel: AvturHydraulic oil: OM-15High pressure gases: NitrogenEngine oil: OX-26Oxygen: LOXOxygen: Cylinder on ejection seat

WARNING

AIRCRAFT DIMENSIONS


JAGUAR MK1AT.O

. 00-105E-9

JAG

UA

R M

K1A

.2


AIRCRAFT ENTRY

1. NORMAL ENTRY

a. Operate normal canopy release handle located at lower left corner of left wind shield.

b. Lift up canopy into LOCKED position. Canopy is hinged at rear.

2. EMERGENCY ENTRY

a. Break protective window of emergency canopy release handle, located on port and starboard side of canopy.

b. Pull black and yellow handle. Canopy will jettison.

3. CUT-IN

a. Canopy is made of acrylic plastic and may be cut with a power rescue saw or crash ax. Cut along the canopy frame. Wind screen is bullet proof.

FUEL TANKS

FUEL TANKS

HYDRAULICFLUIDRESERVOIRS

BATTERY (Access via nosewheel bay)

OXYGEN CYLINDER(Located at seat position)

LIQUID OXYGENCONTAINERS

LASER SYSTEM(In nose)

2a, 2bPROTECTIVE WINDOW WITHEMERGENCY CANOPYRELEASE HANDLE

1aNORMAL CANOPYRELEASE HANDLE

JAGUAR MK1AT.O

. 00-105E-9

JAG

UA

R M

K1A

.3





2. SAFETY ARMAMENT




1aTHROTTLE

1bTHROTTLELEVER




3aCRASHSTRIPE

JAGUAR MK1AT.O

. 00-105E-9

JAG

UA

R M

K1A

. 4


1. SEAT SAFETYING

NOTE: This ejection seat and canopy system is safetied with safety pins or clips.

a. Safe the gun, located top of seat.

b. Safe the extractor gun, located on left side of seat.

c. Safe the high handle, located above face curtain.

d. Safe the lower handle, located center forward seat bucket.

e. Safe the canopy ejection pin located on the left side at the top of the seat.

f. Set “Normal” and “Emergency” oxygen commutator taps to OFF.


a. Pull uncovered handle, located on the left side of seat, for parachute separation.

b. Lift orange lever, located on the left side at bottom of the seat, for crewmember separation.

c. Release ventral (restraints) buckle by the quick disconnect handle to free crewmember from harnesses.

d. Pull up the crewmember by the harness straps.

1cHIGHEJECTIONHANDLE

1dLOWEREJECTIONHANDLE

1cHIGH EJECTIONHANDLE SAFETYPIN

1aGUN SAFETY PIN

1bEXTRACTORGUN

1eCANOPY EJECTIONSAFETY PIN

1eCANOPY INITIATOR

1bEXTRACTOR GUN SAFETY PIN

1f“NORMAL” OXYGENCOMMUTATOR

1f“EMERGENCY” OXYGENCOMMUTATOR

2aUNCOVERED HANDLE

2bSEAT SEPARATION LEVER

1dLOWEREJECTIONHANDLESAFETY PIN

VENTRALBUCKLE



JAGUAR T2T.O

. 00-105E-9

JAG

UA

R T

2.1

AIRCRAFT HAZARDS

Ammunition box

GUN

WEAPONS PYLONS

AIRCRAFT DIMENSIONS


WEAPONS PYLONSGUN




OTHER HAZARDS:Battery acidAssisted escape systemBeryllium +beryllium oxidesBromochlorodifluoromethane (BCF Fire Extinguishant)Bromotrifluoromethane (BTM Fire Extinguishant)Cartridge operated equipmentChlorobromoethane (Fire Extinguishant)Chaff DispenserDimethylformamide (Strobe power pack)Ejector release unitsFlare dispenserLithium (Batteries)Mercury (Temperature bulbs)Methyl Bromide (Fire Extinguishant)Miniature Detonating Cord (MDC)PolytetrafluoroethyleneRadioactive sourcesSonar locator beacon(s) (1-Lithium battery)ThalliumTritium light sourcesFuel: AvturHydraulic oil: OM-15High pressure gases: NitrogenEngine oil: OX-26Oxygen: LOXOxygen: Cylinders mounted on ejection seats

WARNING

JAGUAR T2T.O

. 00-105E-9

JAG

UA

R T

2.2

JETTISONABLECANOPIES

FOOT HOLDS

FOOT HOLDS


AIRCRAFT ENTRY

1. NORMAL ENTRY

a. On left side of fuselage, press down on release button, to release handle.

b. Pull release handle and lift canopies.

2. EMERGENCY ENTRY

a. On left or right side of fuselage, break window.

NOTE: Canopy must be locked prior to jettison.

b. Pull corresponding handle to jettison corresponding canopy.

3. CUT-IN

a. Use power rescue saw to cut-in canopy. Cut all four sides.

2bCANOPY JETTISON HANDLES

2aCANOPY JETTISONWINDOW

1aRELEASE BUTTON

1bRELEASEHANDLE

FUEL TANKSBATTERIES

LOX

SEAT OXYGEN

EJECTIONSEATS

ARRESTING HOOK

FIRE ACCESS PANELS

HYDRAULIC RESERVOIRS

JAGUAR T2T.O

. 00-105E-9

JAG

UA

R T

2.3





2. SAFETY ARMAMENT




1aTHROTTLE

1bTHROTTLELEVER




3aCRASHSTRIPE

JAGUAR T2T.O

. 00-105E-9

JAG

UA

R T

2.4

SEAT SAFETYING ANDAIRCREW EXTRACTIONNOTE: The Jaguar T2 uses a Martin-Baker IN9B MK II zero-zero ejection seats. In two seat versions, the aft seat is 15” or 38 cm higher than the forward seat.

1. SEAT SAFETYING




b. Operate PEC.

c. Release PSP.

d. Operate toggle switch to release leg restraints and pull lines through garters.

e. Release QRF and turn and press box firmly. Lay clear all harness and restraints.

f. Remove aircrew member.

g. Install remaining safety pins into ejection seat.

1aMAIN GUN SEARWITH SAFETYPIN HOLE

1aMAIN GUN PLUNGER

1aMAIN GUNWITH CHARGE

1aSAFETY PIN

1a

2a

2e

2c2b

2d

MIRAGE IVT.O

. 00-105E-9

MIR

AG

E IV.1

AIRCRAFT HAZARDS

BOMB PYLONS

ENGINE INTAKES

ENGINEEXHAUST

Flare and chaff pod located on starboardouter pylon.

Carries ASMP medium range air to surfacenuclear missles.

MIRAGE IVT.O

. 00-105E-9

MIR

AG

E IV.

2

SPECIAL TOOLS/EQUIPMENTPower Rescue SawCrash AxLadderCanopy Wrench

AIRCRAFT ENTRY

1. NORMAL ENTRY

a. To manual release, insert wrench into holes of male drive square.

b. Turn wrench clockwise.

2. EMERGENCY ENTRY

a. To release pyrotechnically, break window glass for canopy jettison.

b. Pull ring in recess.

3. CUT-IN

a. Cut canopy on all four sides.

EXTERNAL FUEL528 US GALS(2000 LITRES)

BATTERY

OXYGEN

INTERNAL FUEL

EXTERNAL FUEL

1aWRENCHHOLES

2aWINDOW

2bRING

MIRAGE IVT.O

. 00-105E-9

MIR

AG

E IV.

3


a. Move throttle controls,located on left console, completely AFT.

b. Lift throttle flaps, located below throttle controls, to STOP position.

c. Lift fuel cutoff switch covers, located on right console.

d. Move fuel cutoff switches to AFT.

e. Move power cutoff switch,located on right forward instrument panel, DOWN.

1aTHROTTLECONTROLS

1bTHROTTLEFLAPS

1c, 1dFUEL CUTOFFSWITCHES

1ePOWERCUTOFFSWITCH

MIRAGE IVT.O

. 00-105E-9

MIR

AG

E IV.

4


NOTE: The Mirage IV uses a Martin Baker ejection seat. The graphic identifies critical components and safety pin locations for safetying and crew extraction.

a. Install safety pins in face curtain, drogue gun, lower ejection handle. Pins are pip pin type.

b. Install safety pins in canopy fragilization initiator. Pin is clip type.


a. Release lap belt buckle. Lap belt buckle secures crew member by lap belt and shoulder harness.

b. Release uncovered handle to release leg restraints.

c. Pull orange handle on left side of seat. This is a central harness quick release for the release of all restraints.

1aFACE CURTAINSAFETY PIN

2aLAP BELT BUCKLE

1aLOWER EJECTION(D RING) HANDLEAND SAFETY PIN

1bTOP CHARGE MECHANISMSAFETY PIN (PIN IS ROUTEDTHROUGH SEAR)

1aDROGUE GUN MECHANISMSAFETY PIN (PIN IS ROUTEDTHROUGH SEAR)

1bCANOPYFRAGILIZATIONSAFETY PIN

2cORANGEHANDLEFOR CREWRELEASE

2bUNCOVERED HANDLEFOR CREW RELEASE

MIRAGE F1 CT F-1/C-14

T.O. 00-105E

-9

MIR

AG

E F

1 CT.

1

AIRCRAFT HAZARDSNOTE:This file of the Mirage includes:CT or CR, F 1C, and C-14(F-1).

F1 CT

F1 CR OR F1 CT

POINT 3MISSLE

POINT 3MISSLE

POINT 0POINT 0

POINT 2

POINT 1POINT 2

POINT 1

UNDER FUSELAGE

TANKSBOMBSMISSLETANKS

BOMBSMISSLE

TANKSBOMBSMISSLE

CHAFFDISPENSERS

CHAFFDISPENSERS

NOTE: Carriage units are provided with either an air vane or an initiator access door which, in open position, neutralizes load drop.

F1 C

F1 CR


T.O. 00-105E

-9

MIR

AG

E F

1 CT.2


CARBON FIBRECOMPOSITE

CR OR CT

HYDRAULICOIL

ENGINE EXHAUST196 FT (60 M)

INTAKE AREA23 FT (7 M)

BATTERY(RT SIDE)

LIQUID OXYGEN(5 LITRES)(LT SIDE)

EXTERNAL FUEL TANKS(CENTER, LT, & RT SIDES)951 US GAL (3600 LITRES) EACH

INTERNAL FUEL TANKS1083 US GAL (4100 LITRES) TOTALFORWARD GROUP538,574,538 US GAL (1.650 LITRES)REAR GROUP560x2 US GAL (1.120 LITRES)AUXILIARY GROUP560x2 US GAL (1.120 LITRES)WING TANKS175x2 US GAL (350 LITRES)

ALLMODELS


T.O. 00-105E

-9

MIR

AG

E F

1 CT.

3

SPECIAL TOOLS/EQUIPMENTPower Rescue SawCrash Ax

AIRCRAFT ENTRY

1. NORMAL ENTRY

NOTE: Canopy unlock key is stowed in panel located on right side of fuselage aft of right intake.

a. Insert key in square slot, located on left side of fuselage forward left corner of canopy.

b. Turn key clockwise to unlock and open canopy.

c. Lift up canopy.

2. EMERGENCY ENTRY

a. Break window glass, located on left side of fuselage aft of canopy, to expose ring.

b. Pull ring to embrittle or shatter canopy.

3. CUT-IN

a. If emergency entry can not be accomplished, use the power rescue saw or crash ax to enter cockpit area. Cut all four sides to gain access.

1aKEY

1aKEYSQUARESLOT

INTERNALUNLOCKHANDLE

INTERNALCANOPYLINKAGE

2bEMBRITTLEDCANOPY

(RESCUE)

1aKEY

KEY STOWAGEPANEL

2bPULL RING

2aWINDOW


T.O. 00-105E

-9

MIR

AG

E F

1 CT.

4

ENGINE, ARMAMENT, ANDELECTRIC SHUTDOWN1. ENGINE SHUTDOWN

a. Retard throttles, located on left console, AFT while pressing throttle lever.

b. Place fuel cutoff switches, located on aft left console, to OFF, to stop fuel flow.

c. Lift emergency shutoff valve switch guard, located just forward of throttles, and tip up switch AFT.

d. Lift afterburner emergency shutoff valve switch guard, located just forward of throttles, and tip up switch AFT.

2. ARMAMENT SHUTDOWN

a. Pull armament neutralization switch guard, located on upper left console, down and INWARD toward seat.

3. ELECTRIC SHUTDOWN

a. Pull electric power shutdown switches (3), located on upper right console, DOWN, to shutoff battery, ALT 1 and ALT 2.

1aTHROTTLES

1aTHROTTLELEVER

1bFUEL CUTOFFSWITCHES

1cEMERGENCYSHUTOFFSWITCH

1dAFTERBURNEREMERGENCYSHUTOFF SWITCH

2aARMAMENTNEUTRALIZATIONSWITCH

3aELECTRICPOWERSHUTDOWNSWITCHES


T.O. 00-105E

-9

MIR

AG

E F

1 CT. 5

EXTERNAL GROUND EGRESS1. EXTERNAL GROUND EGRESS - C-14 (F-1)

NOTE: If the canopy is damaged during ditching procedures, the canopy will need to be unlocked, the canopy system safetyied and disconnected and the canopy actuator disconnected.

Engines may still be running, be aware of existing dangers with intakes, hot air exhausts, and hot engine exhaust. Airborn debris may also be present that can endanger personnel.




c. Lift up canopy and hold open for next two steps.

d. If canopy is damaged and will hinder ground egress, disconnect two percussion lines by turning knurled connectors counterclockwise.

e. Disconnect bungee cord from percussion lines.

f. Place central percussion on safety.

g. Disconnect canopy actuator by pulling pin out at top of actuator and set canopy aside.

1a, 1bCANOPY UNLOCK KEY

1cCANOPY

1dPERCUSSION LINES

1eBUNGEE CORD

1fCENTRALPERCUSSIONSAFETY

1gCANOPY ACTUATOR PIN

ENGINESUCTION ENGINE

EXHAUST

ENGINEHOT AIR

CANOPYUNLOCK ACCESS

CANOPYEMERGENCYACCESS

EXTERNAL GROUND EGRESS DANGERS

WARNING


T.O. 00-105E

-9

MIR

AG

E F

1 CT.6

SEAT SAFETYING ANDAIRCREW EXTRACTION1. SEAT SAFETYING - F-1C FR VARIATION

a. Install seat catapult safety pin, located top aft of seat.

b. Install canopy initiator safety pin, located top left side of seat.

NOTE: Install safety pins in upper, lower ejection handles and drogue gun if time allows.


a. Pull parachute release handle, located left saft of seat bucket.

b. Pull pilot seat release lever, located left aft bottom side of seat bucket.

c. Push red buttons on lap belt and twist belt lock right or left to release lap belt.

d. Pull up on pilot with shoulder straps to remove aircrew member. LOWER

EJECTIONHANDLE

LOWEREJECTIONHANDLESAFETY PIN

UPPEREJECTIONHANDLE

UPPEREJECTIONHANDLESAFETYPIN

1bCANOPYINITIATORWITH SAFETYPIN

DROGUE GUNWITH SAFETY PIN

OXYGENNORMALSWITCH

OXYGENEMERGENCYSWITCH

1bSEAT RELEASE LEVER

1aPARACHUTERELEASEHANDLE

2cREDBUTTON

2cREDBUTTON

2cLAP BELT LOCK


T.O. 00-105E

-9

MIR

AG

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1 CT.

SEAT SAFETYING AND AIRCREWEXTRACTION-Continue1. SEAT SAFETYING - C-14 (F-1) SP VARIATION

NOTE: Once the canopy is opened, proceed to install TWO main safety pins.

a. Install seat catapult safety pin, located top aft of seat.

b. Install drogue gun safety pin, located on left side of seat.

NOTE: Install safety pins in upper and lower ejection handles if time allows.


a. Unlatch harnesses actuating the silvered lever, which form is like a trigger, located on the left side of the lower portion of the seat.

b. Release the anchor of the harnesses by pressing the lugs (red buttons) and rotating the center portion of the release.

c. Release survival kit, pressing both sides of the clip on the red strap, located on the pilot’s left thigh.

d. Enter the cockpit and grab the pilot under arms and lift him as much as possible.

e. Carry the pilot carefully to ground personnel.

1aSEATCATAPULTSAFETY PIN

UPPEREJECTIONHANDLE

UPPER EJECTIONHANDLE SAFETYPIN HOLE

1bDROGUE GUNWITH SAFETY PINAND STREAMER

2aSILVER LEVER

2bLUGS

2bLAP BELTRELEASE

7


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-9

MIR

AG

E F

1 CT.

SEAT SAFETYING AND AIRCREWEXTRACTION-Continue1. SEAT SAFETYING - F-1 CT OR CR FR VARIATION

NOTE: The Mirage F1 CR or CT uses the Martin Baker MK 10 Ejection seat. Safety pin storage pouch is located on the upper left side of the seat.

a. Install lower ejection handle safety pin, located at bottom forward center of seat.

b. Install canopy embrittlement initiator safety pin, located top left side of seat.


a. Press ventral buckle pushbuttons and turn center portion one quarter turn clockwise to release straps.

b. Press button to disconnect junction unit to lift and release oxygen, radio, and leggings connections.

c. Set both oxygen shutoff pallets to OFF.

d. To release the survival kit, unclip the sticker clips or cut the lowering line.

SAFETY PINSTORAGE

1bCANOPY EMBRITTLEMENTINITIATOR

2cOXYGENSHUTOFFPALLETS

2aVENTRALBUCKLE WITHPUSHBUTTONS

1aLOWER EJECTIONHANDLE SAFETYPIN HOLE

2bJUNCTION UNITBUTTON

2dSTICKERCLIPS

2dLOWERINGLINE

1aSAFETYPIN

8

MIRAGE F1 BT.O

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1 B. 1

POINT 3MISSLE

POINT 2

POINT 1

POINT 2

POINT 1

UNDER FUSELAGE

TANKSBOMBSMISSLE

ROCKETS ROCKETS

NOTE: Carriage devices are provided with either an air vane or an access door to thrusters which, in open position, neutralize air drop.

AIRCRAFT HAZARDS

POINT 3MISSLE

MIRAGE F1 BT.O

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1 B. 2


CARBON FIBRECOMPOSITE

HYDRAULICOIL

ENGINE EXHAUST196 FT (60 M)

INTAKE AREA23 FT (7 M)

BATTERY(LT SIDE)

LIQUIDOXYGEN1.3 US GAL(5 LITRES)(IN WHEELWELL)

EXTERNAL FUEL TANKS(CENTER, LT, & RT SIDES)911 US GAL (3450 LITRES) EACH

INTERNAL FUEL TANKS1011 US GAL (3830 LITRES) TOTAL

MIRAGE F1 BT.O

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1 B. 3


AIRCRAFT ENTRY

1. NORMAL ENTRY




c. Lift up canopy.

2. EMERGENCY ENTRY

a. Break window glass, located on left side of fuselage aft of canopy, to expose ring.

b. Pull ring to embrittle or shatter canopy. Both canopies are weakened simultaneously.

3. CUT-IN


1aKEY

1aKEYSQUARESLOT

INTERNALUNLOCKHANDLE

INTERNALCANOPYLINKAGE

2bEMBRITTLEDCANOPY

RESCUE

1aKEY

KEY STOWAGEPANEL

2bPULL RING

2aWINDOW

EMERGENCY OPENING

MIRAGE F1 BT.O

. 00-105E-9

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E F

1 B.4

ENGINE, ARMAMENT, ANDELECTRIC SHUTDOWN1. ENGINE SHUTDOWN

a. Retard throttles, located on left console, AFT while pressing throttle lever.

b. Place fuel cutoff switches, located on aft left console, to OFF, to stop fuel flow.

c. Lift emergency shutoff valve switch guard, located just forward of throttles, and tip up switch AFT.

d. Lift afterburner emergency shutoff valve switch guard, located just forward of throttles, and tip up switch AFT.


a. Pull armament neutralization switch guard, located on upper left console, down and INWARD toward seat.

3. ELECTRIC SHUTDOWN

a. Pull electric power shutdown switches (3), located on upper right console, DOWN, to shutoff battery, ALT 1 and ALT 2.

1aTHROTTLES

1aTHROTTLELEVER

1bFUELCUTOFFSWITCHES

1dAFTERBURNER EMERGENCYSHUTOFF SWITCH

2aARMAMENTNEUTRALIZATIONSWITCH

1cEMERGENCYSHUTOFFSWITCH

3aELECTRICPOWERSHUTDOWNSWITCHES

MIRAGE F1 BT.O

. 00-105E-9

MIR

AG

E F

1 B.5

SEAT SAFETYING AND AIRCREWEXTRACTION-Continue1. SEAT SAFETYING - F-1 B FR VARIATION

NOTE: The Mirage F1 B uses the Martin Baker MK 10 Ejection seat. Safety pin storage pouch is located on the upper left side of the seat.

a. Install lower ejection handle safety pin, located at bottom forward center of seat.

b. Install canopy embrittlement initiator safety pin, located top left side of seat.


a. Press ventral buckle pushbuttons and turn center portion one quarter turn clockwise to release straps.

b. Press button to disconnect junction unit to lift and release oxygen, radio, and leggings connections.

c. Set both oxygen shutoff pallets to OFF.

d. To release the survival kit, unclip the sticker clips or cut the lowering line.

SAFETY PINSTORAGE

1bCANOPY EMBRITTLEMENTINITIATOR

2cOXYGENSHUTOFFPALLETS

2aVENTRALBUCKLE WITHPUSHBUTTONS

1aLOWER EJECTIONHANDLE SAFETYPIN HOLE

2bJUNCTION UNITBUTTON

2dSTICKERCLIPS

2dLOWERINGLINE

1aSAFETYPIN

MIRAGE 2000 B-N-DT.O

. 00-105E-9

MIR

AG

E 2000 B

ND

.

AIRCRAFT HAZARDS

EXTERNAL

MISSLE

INTERNAL FUS LATREAR

DROP TANK BOMBSROCKET LAUNCHER

DROP TANK BOMBSROCKET LAUNCHER

MISSLE MISSLEDROP TANK BOMBSBOMBS

BOMBS

BOMBS LDP*

FUS LATREAR

EXTERNALINTERNAL FUS LATFRONT

FUS LATFRONT

CENTRALFUSELAGE

ARMAMENT LOAD

1


. 00-105E-9

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ND

.2


SAFETY PIN

LDP*

NOTE: LDP = Laser Designation Pod

SAFETY PIN

AIR VANE

SAFETY PIN

CUTTING DOOR

MISSLE

MISSLE

DROP TANK

CASE SPOTTEDPIN’S LOCATION

CHAFF DISPENSERS AIR VANE


. 00-105E-9

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ND

.3

AIRCRAFT HAZARDS-ContinuedAIRFRAME MATERIALS

CARBON FIBRES

FIBREGLASS

CARBON FIBRES +BORON


. 00-105E-9

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AG

E 2000 B

ND

.4


BATTERY(RT SIDE)

LIQUID OXYGEN 2, 24 US GAL (8, 5 LITRES) (LT SIDE)

INTAKE AREA2 M

2 M

CENTERLINE FUEL TANK1366 US GAL (5170 LITRES)

INTERNAL FUEL TANK1035 US GAL (3920 LITRES)

DROP FUEL TANK2092 US GAL (7920 LITRES)

ENGINE EXHAUST-80 METERS

DUAL EJECTION SEAT VERSION


. 00-105E-9

MIR

AG

E 2000 B

ND

.5


AIRCRAFT ENTRY

1. NORMAL ENTRY

a. Press release buttons, located on release handle left side fuselage, to release unlock handles.

b. Pull unlock handle down to unlock and open corresponding canopy.

NOTE: Move handles up to close and lock canopies, if applicable.

c. Lift corresponding canopy.

2. EMERGENCY ENTRY

NOTE: Emergency controls are located on both sides of fuselage.

a. Break window glass to expose embrittlement handle.

b. Pull canopy embrittlement handle about 8 inches or 20 centimeters. Do not watch canopy while embrittling.

c. Dislocate canopy.

3. CUT-IN

a. If embrittlement system is damaged or inoperative, use power rescue saw for all four sides of canopy or smash canopy with crash ax.

EMBRITTLEDCANOPY

2aWINDOW

1aRELEASEBUTTON

1bUNLOCKHANDLE

LOWEREJECTIONHANDLE

2bEMBRITTLEDHANDLE (TYPICAL)



. 00-105E-9

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ND

.6

ENGINE, ARMAMENT ANDBATTERY SHUTDOWN1. ENGINE SHUTDOWN

NOTE: Directional arrows provide for direction of switch final placement for shutdown.

a. Bring throttle, located on the left console, AFT.

b. Press “STOP” notch, located forward of the throttle, and bring throttle to rear stop.

c. Place the fuel shutoff valve switch with guard, located on the right aft console, up and to OFF.

d. Place the three fuel pump switches, located on the right aft console, in the left position to OFF.


a. Place the armament master switch, located on the left side of the forward instrument panel, downward to OFF.

b. Push missle launcher unlock security guard and switch, located in front of front cockpit control stick, DOWN.

3. BATTERY SHUTDOWN

a. Place the battery cutoff switch, located on right side of the forward instrument panel, downward to OFF.

1aTHROTTLE

2aARMAMENTMASTERSWITCH

3aBATTERY CUT OFF SWITCH

1bSTOPNOTCH

1dFUEL PUMPSWITCHES

1cFUELSHUTOFFSWITCH

1cSWITCHGUARD

2bMISSLE LAUNCHERUNLOCK SECURITY


. 00-105E-9

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.7

1. SEAT SAFETYING

NOTE: Safety pins are located in storage pouch on upper left side of ejection seat.

a. Insert safety pin in lower ejection handle.

b. Insert safety pin in canopy embrittlement initiator, located at central percussion behind seat. Approach from left side of seat.


a. Release quick disconnect handle at center of personnel restraints buckle. Lap belts and shoulder harness will be released.

b. Pull quick evacuation control, located on forward left armrest area.

c. Set “NORMAL - EMERGENCY” oxygen selector on OFF position.

d. Unhook or cut survival pack opening strap to free crewmember from survival pack.

e. Remove crewmember.


SAFETY PINPOUCH

1aLOWEREJECTIONHANDLE

2aQUICKDISCONNECTHANDLE

1bQUICKEVACUATIONCONTROL

1dSURVIVAL PACKOPENING STRAP

2cOXYGENSELECTOR

NORMAL EMERGENCY

1b CANOPYEMBRITTLEMENTINITIATOR

MIRAGE 2000 CT.O

. 00-105E-9

MIR

AG

E 2000 C

.

AIRCRAFT HAZARDS

1

NOTE: To neutralize the guns, pull air vane open to oneself on striped yellow and black panel.

NOTE: Armament is loaded on the fuselage and wings. The fuselage can be loaded with fuel tanks and bombs. The wings can be loaded with fuel tanks, bombs, rocket launcher, and missles. Red stripes on graphic illustrate location of devices.

AIRFRAME MATERIALS

CARBON FIBRES

FIBREGLASS

CARBON FIBRES +BORON

GUNS

AIR VANE

MIRAGE 2000 CT.O

. 00-105E-9

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E 2000 C

.2


BATTERY

LIQUID OXYGEN 32 US GAL (5 LITRES)

INTAKE AREA

2 M

2 M

CENTERLINE FUEL TANK14OO US GAL (5300 LITRES)

INTERNAL FUEL TANK1070 US GAL (4050 LITRES)

DROP FUEL TANK2457 US GAL (9203 LITRES)

ENGINE EXHAUST-80 METERS

SINGLE EJECTION SEAT VERSION

MIRAGE 2000 CT.O

. 00-105E-9

MIR

AG

E 2000 C

.3


AIRCRAFT ENTRY

1. NORMAL ENTRY

a. Press release button, located on release handle left side fuselage, to release unlock handle.

b. Pull unlock handle down to unlock and open canopy.

NOTE: Move handle up to close and lock canopy, if applicable.

c. Lift canopy.

2. EMERGENCY ENTRY

NOTE: Emergency controls are located on both sides of fuselage.

a. Break window glass to expose embrittlement handle.

b. Pull canopy embrittlement handle about 8 inches or 20 centimeters. Do not watch canopy while embrittling.

c. Dislocate canopy.

3. CUT-IN

a. If embrittlement system is damaged or inoperative, use power rescue saw for all four sides of canopy or smash canopy with crash ax.

EMBRITTLEDCANOPY

2aWINDOW

1aRELEASEBUTTON

1bUNLOCKHANDLE

LOWEREJECTIONHANDLE

2bEMBRITTLEDHANDLE (TYPICAL)


MIRAGE 2000 CT.O

. 00-105E-9

MIR

AG

E 2000 C

.4

ENGINE, ARMAMENT ANDBATTERY SHUTDOWN1. ENGINE SHUTDOWN

NOTE: Directional arrows provide for direction of switch final placement for shutdown.

a. Bring throttle, located on the left console, AFT.

b. Press “STOP” notch, located forward of the throttle, and bring throttle to rear stop.

c. Place the fuel shutoff valve switch with guard, located on the right aft console, up and to OFF.

d. Place the three fuel pump switches, located on the right aft console, in the left position to OFF.


a. Place the armament master switch, located on the left side of the forward instrument panel, downward to OFF.

3. BATTERY SHUTDOWN

a. Place the battery cutoff switch, located on right side of the forward instrument panel, downward to OFF.

1aTHROTTLE

2aARMAMENTMASTERSWITCH

3aBATTERYCUT OFFSWITCH

1bSTOPNOTCH

1dFUEL PUMPSWITCHES

1cFUELSHUTOFFSWITCH

1cSWITCHGUARD

MIRAGE 2000 CT.O

. 00-105E-9

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.5


NOTE: Safety pins are located in storage pouch on upper left side of ejection seat.

a. Insert safety pin in lower ejection handle.

b. Insert safety pin in canopy embrittlement initiator, located at central percussion behind seat. Approach from left side of seat.


a. Release quick disconnect handle at center of personnel restraints buckle. Lap belts and shoulder harness will be released.

b. Pull quick evacuation control, located on forward left armrest area.

c. Set “NORMAL - EMERGENCY” oxygen selector on OFF position.

d. Unhook or cut survival pack opening strap to free crewmember from survival pack.


SAFETY PINPOUCH

1aLOWEREJECTIONHANDLE

2aQUICKDISCONNECTHANDLE

1bQUICKEVACUATIONCONTROL

1dSURVIVAL PACKOPENING STRAP

2cOXYGENSELECTOR

NORMAL EMERGENCY

1b CANOPYEMBRITTLEMENTINITIATOR

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PAINT SCHEME

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AIRCRAFT DIMENSIONS

WING SPAN 45 FT 7.5 IN(13.91 METERS)

HEIGHT 19 FT 6.25 IN(5.95 METERS)

LENGTH 54 FT 10.25 IN(16.72 METERS)

GENERAL INFORMATION

The Tornado Interdictor Strike (IDS) and AirDefence Variant (ADV) use similar airframesand the same engines, but different radar,avionics software and weapon suites.

Maximum Level Speed: Mach 2.2, 800 knotsThrust Per Engine: Over 9,000 lbs.Reheated Thrust Per Engine: Over 16.000 lbs.Design Fatigue Life: 16,000 hrs.Minimum Service Life: 4,000 hrs.Operational Weight, Empty: 30,800 lbs.Max. Take-Off Wt: 61,700 lbs.Max. Payload: Over 19,800 lbs.Manufacturer: PANVIA, Munich, Germany

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AIRCRAFT HAZARDSFIRE AND EXPLOSION HAZARDS

1 CO2 Bottle 2 LH and RH Canopy Jettison Rocket Motors 3 Cartridges, Canopy Jettison Initiator Unit 4 Canopy Accumulator 5 Brake Accumulator 6 Pitch Feel Accumulator (up to Serial # 4028) 7 Initiator Unit, MDC System 8 Foward Tank Group 9 MDC Cords10 Right Wing Fuel Tank11 Cartridge, Crash Recorder Airfoil Release Unit12 Rear Tank Group13 Fire Extinguisher Bottle14 Hydraulic Reservoir #215 33 MB Emergency Battery16 Main Accumulators #1 & #217 Hydraulic Reservoir # 118 Lubricating Oil Tank19 Left Wing Fuel Tank20 Main Landing Gear (MLG) Strut21 Main Wheel Tire22 Pitch Feel Accumulator (from Serial # 4029 onwards)23 LOX Converter24 Nitrogen Bottle, Landing Gear Emergency Lowering System25 Nose Landing Gear (NLG) Strut26 Nose Wheel Tire27 Ejection Seat28 Canopy and Windscreen Seal Air Reservoir

12

3

14

56

7

2

9

1011

12

13 14 15

16

17

18

192021

22232425

262728

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TURBO-UNION RD199 MK101TURBOFAN ENGINE

4


BATTERY

VARIABLEGEOMETRY WING FUEL TANKS

SIDEWINDER AIR-TO-AIR MISSILES

OXYGEN

MARTIN BAKER MK 10A EJECTION SEATS

FOXHUNTER AIR INTERCEPT RADAR

MAUSERCANNON

SKY FLASHAIR-TO-AIRMISSILES

EXTERNAL FUEL TANK

RADARWARNINGSYSTEM

TURBO-UNION RD199 MK101TURBOFAN ENGINE

AIR BRAKE

FUEL TANKS

EXTERNAL FUEL TANK

OXYGEN

BATTERY

AIR BRAKEMARTIN BAKER MK 10A EJECTION SEATS

SIDEWINDER AIR-TO-AIR MISSILES

MAUSERCANNON

CHAFF AND FLARE DISPENSERS

AFT PASSIVEECM HOUSING

ECM POD(ELECTRONIC COUNTER MEASURES)

1,000 LB BOMBS

VARIABLEGEOMETRY WING

GROUND MAPPINGAND TERRAINFOLLOWING RADARS

FWD PASSIVEECMHOUSING

HAZARDS AND ARMAMENT

PA 200 ADV

PA 200 IDS

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SPECIAL TOOLS/EQUIPMENTFire Drill IIPower Rescue SawAIRCRAFT ENTRY1. NORMAL ENTRY

If the aircrew has to be rescued with assistance from the outside, special attention has to be paid to the hazards resulting from the ejections seats, the canopy jettison system and the MDC system.

NOTE: Various canopy opening procedures are described. The ejection seats, the canopy jettison system and the MDC system are equipped with pyrotechnic components.

Inadvertent initiation may cause extremely severe or even fatal injuries. Therefore, it is mandatory that the systems be provided with adequate safety devices before the rescue actions are begun. If the canopy was jettisoned, only the ejection seats are to be secured. If possible, the MDC system has to be deactivated on the jettisoned. The individual opera- tions necessary to rescue the aircrew are described. If the aircrew is unable to open the canopy, the rescue crew has various possibilities of gaining access to the cockpits.

a. The canopy can be opened by means of the external canopy control handle. If this is impos- sible, the canopy can be raised manually after it has been unlocked or the transparencies can be detonated.

If the left engine is running, the danger of the left engine air intake has to be considered and the aircrew has be protected before opening the canopy to prevent ingestion into the air intake.

WARNING

WARNING

WARNING

b. If the canopy is undamaged, it can be opened from the outside by the external canopy control handle located on the left side of the front fuselage. If the canopy cannot be opened by the external canopy control handle, it has be opened, by unlocking the canopy using the external canopy control handle.

c. Pull out the external jack release handle, thereby uncoupling the canopy jack. The uncoupling process can also be initiated by the aircrew by operating the internal jack release handle in the front or rear cockpit. Raise cockpit manually and secure against closing.

2. EMERGENCY ENTRY

a. If the canopy cannot be raised manually, detonate the canopy transparencies.

When pulling the external MDC handle, move under- neath aircraft, if possible, to avoid injuries by fractured airborn debris. In any case, turn face away from aircraft and cover exposed places on the body.

b. The canopy transparencies are detonated by the MDC system and blown clear of the canopy frame. The external MDC handle is located on the left side of the front fuselage and covered by a panel.

c. For detonation of the canopy transparencies break the glass.

d. Pull the handle to the total extent of the cable (approx. 3 m) and then tug.

WARNING

2b, 2c, 2dMDC SYSTEMWITH GLASSCOVER, CABLEAND HANDLE

1a, 1bEXTERNALCANOPYCONTROLHANDLE

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ENGINE SHUTDOWN1. EMERGENCY ENGINE SHUTDOWN

NOTE: The following procedure shall among other things be applied, if, in an emergency, the engines have to be shut down by personnel not authorized to accomplish engine runs.

NOTE: The engine throttles are located on the left console in the front cockpit. The GT variant is equipped with two additional throttles in the rear cockpit which, however, cannot be used for engine shutdown.

Do not enter the engine air intake area while the engines are running. Air intake ingestion can cause injury or death to personnel.

a. Access the cockpits using the entry procedures.

b. On the throttle quadrant, push throttle lock forward and select throttle to the HP SHUT position.

c. Select LP cock switches LP COCKS LEFT and RIGHT, located on the left side of forward instrument panel, to the SHUT position.

d. Select all switches on the rapid take-off panel, except the battery master switch BATT MSTR to the OFF position.

e. When the engine has run down, select battery master switch BATT MSTR to the OFF position.

WARNING1bTHROTTLEQUADRANT

1bTHROTTLE

3aLP COCKSWITCHESLH & RH

1dRAPID TAKE-OFF PANEL

1d, 1eMASTERBATTERYSWITCH

1bTHROTTLELOCK

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APU SHUTDOWN1. EMERGENCY MANUAL APU SHUTDOWN

NOTE: In an emergency, e. g. in case of a fire or fracture of oil, fuel or hydraulic lines during operation of the secondary power system, the APU may be shut down by actuating one of the following switches.

a. SHUTDOWN INITIATED IN THE FRONT COCKPIT

(1) Select APU switch to OFF.

(2) Select APU fire test switch APU AUTO TEST to TEST.

(3) Select battery master switch BATT MSTR to OFF (only possible up to Serial No. 4299).

b. SHUTDOWN IN THE RIGHT MAIN LANDING GEAR BAY

(1) Select APU SAFETY switch to SAFE.

1a(1)APUSWITCH

1a(2)APU FIRETEST SWITCH

1a(3)BATTERYMASTERSWITCH

1b(1)APUSAFETYSWITCH

FORWARDCOCKPIT

RIGHT MAINLANDING GEAR BAY

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MARTIN BAKER MK10A EJECTION SEATEJECTION SEAT COMPONENTS

1 Secondary Cartridge, Drogue Gun 2 Primary Cartridge, Drogue Gun 3 Primary Cartridge, Ejection Gun (Catapult) 4 Cartridge, Barostatic Time Release Unit 5 Secondary Cartridge, Upper, Ejection Gun 6 Secondary Cartridge, Lower, Ejection Gun 7 Cartridge, Manual Separation Firing Unit 8 Cartridge, Rocket Pack Firing Unit 9 Rocket Pack10 Cartridge, Seat Pan Firing Unit11 Emergency Oxygen Cylinder12 Cartridge, Rocket Pack Firing Unit13 Cartridge, Harness Power Retraction Unit14 Ejection Control Handle

2

13

4

5

6

7

8

9

10

11

14

12

13

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AIRCREW EXTRACTION1. LOCKING/SAFETYING OF THE ESCAPE SYSTEMS

When accomplishing rescue and recovery actions in the cockpit area, it is mandatory that the canopy jettison system, the MDC system and the ejection seats be completely locked/safetied.

NOTE: The following rescue procedure has to be accomplished to rescue an unconscious aircrew member from an ejection seat. It only applies to the technical sequence of activities; medical care is to be provided by the responsible medical specialist personnel.

If the oxygen mask is still fitted to the helmet, remove mask to prevent death due to suffocation. Post Ta FL1241: If the aircrew member wears NBC protective equipment, both hood zippers have to be opened. If necessary, the quick-release handle on the upper right side of the hood is to be operated. The oxygen mask is now freely accessible and has to be removed.

NOTE: If rescue is attempted via open canopy (MDC not fired) then MDC initiator unit safety pins must be fitted to both cockpits. Pin stowage position similar for both cockpits.

a. Make forward seat safe first by by selecting the safe position at the command ejection selector, located in aft cockpit.

b. Insert seat pan safety pin (yellow color) in the forward and aft seats at the lower ejection handle.

c. Insert canopy jettison initiator unit safety pin, located between cockpits, if applicable.

WARNING

WARNING

LOWER EJECTIONCONTROL HANDLE(D-RING)

1bSEAT PANSAFETY PIN(TYPICAL BOTHCOCKPITS)

MARTIN BAKER EJECTION SEAT MK10

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A

B

F

E D

C

B

NOTE: Operation/step d applies only to aircrew members equipped with NBC protective equipment post TA FL1241.

d. Open upper and lower hood zippers. If required, operate the orange quick-release handle. (Detail F)

e. Operate control knob and raise visor. (Detail A)

f. Open mask mortise lock and remove oxygen mask. (Detail A)

g. Open connector and release dinghy retaining lanyard. (Detail D)

h. Release arm restraint lines on quick-release connector. (Detail B)

i. Open quick-release fitting and release leg and shoulder straps. (Detail D)

j. Unlock PEC man portion handle and release PEC man portion. (Detail C)

k. Ensure that the leg restraint lines are removed from the taper plug lock and the leg garters. (Detail E)

NOTE: Operation/step l applies only to aircrew members equipped with NBC protective equipment post TA FL1241.

l. Disconnect/remove hood scavenging line on the quick- release connection i. a. w. Detail F from the blower.

m. Rescue aircrew from the aircraft.

AIRCREW EXTRACTION-Continued

A

HELMETVISORCONTROLKNOB

MASKMORTISELOCKOXYGEN

MASK

B CD

E

F

UPPER &LOWERHOODZIPPERS

NBCHOOD NBC

HOOD

ORANGEQUICKRELEASEHANDLE

QUICK RELEASECONNECTION

DINGHYCONNECTOR

QUICKRELEASEFITTING

PECHANDLE

PEC

ARMRESTRAINTLINE

QUICKRELEASECONNECTOR

TAPER PLUG LOCK

LEG RESTRAIN LINES

LEG GARTER

LEG GARTER

TORNADO F3T.O

. 00-105E-9

TOR

NA

DO

F3.1

AIRCRAFT DIMENSIONS




TORNADO F3T.O

. 00-105E-9

TOR

NA

DO

F3.2

AIRCRAFT HAZARDS

MASTER ARMAMENT SAFETY SWITCH(Green flag in Safe Position)

Ammunition Box180 Rounds of Ammunition

CANON

MISSLE STATIONS

NOTE: A variety of missles are carried externally.

OTHER HAZARDS:Battery acidAssisted escape systemAsbestosBeryllium + beryllium oxidesBromochlorodifluoromethane (BCF Fire Extinguishant)Bromotrifluoromethane (BTM Fire Extinguishant)Cadium (Battery/Bolt protection/Steel protectionCartridge operated equipmentComposite Materials (Man-made mineral fibres)CoolanolChaff DispenserDimethylformamide (Strobe power pack)Ejector release unitsFlare dispenserLithium (Batteries)Mercury (Temperature bulbs)Miniature Detonating Cord (MDC)PolytetrafluoroethylenePotassium HydroxideRadioactive sourcesSonar locator beacon(s) (1-Lithium battery)ThalliumThorium FluorideWeapon LoadZinc SelenideFuel: AvturHydraulic oil: OM-15High pressure gases: NitrogenEngine oil: OX-26Oxygen: LOX

TORNADO F3T.O

. 00-105E-9

TOR

NA

DO

F3.3


OXYGEN CYLINDERAT SEAT POSITIONS

FUEL

NITROGENCYLINDER

NITROGENCYLINDER

BATTERY

LIQUIDOXYGENCONTAINER


OIL TANKSFLIGHTRECORDER

EXTERNAL FUEL TANKS MAY BEFITTED IN POSITIONS SHOWN

TORNADO F3T.O

. 00-105E-9

TOR

NA

DO

F3.4

SPECIAL TOOLS/EQUIPMENTPower Rescue SawCrash AxAIRCRAFT ENTRY

1. NORMAL ENTRY

a. Press access door, located on left side of the fuselage, release lever and pull lever to STOP position.

2. MANUAL ENTRY

a. Pull yellow/black marked O-handle, located behind normal entry release lever, to STOP position. (Not illustrated.)

b. Press canopy upwards and install steadying strut.

3. EMERGENCY ENTRY

Personnel other than the operator of the emergency release explosive canopy handle must stand well clear of the aircraft. Handle is located on port side of aircraft and has Mild Detonating Cord (MDC)installed.

a. Break the frangible panel, located on the left side of the fuselage, by striking it in the center with the heel of the hand with fist clenched, to expose emergency canopy handle.

b. Grasp the emergency canopy handle with the right hand and move forward and away along a line approximately 45 degrees to the fuselage until the cable becomes taut.

c. Facing away from the aircraft with handle in the right hand, pull the handle sharply.

4. CUT-IN


WARNING

1aACCESSDOOR

3bCANOPY EMERGENCY HANDLE

3aWINDOW

3bCABLE

BREAK GLASS PULL

HANDLE CENTER

OF CABLE THEN TUG

TORNADO F3T.O

. 00-105E-9

TOR

NA

DO

F3.

5


Before operating crash switches, the throttles must be selected back to HP SHUT position.

Failure to follow the above procedure will cause the engines to rapidly accelerate, possibly to destruction.

NOTE: Thumb plates must be pushed forward to allow the throttle/HP cocks to be selected fully back to SHUT position.

a. Pull fully back the throttles/HP cocks, located on the left console.

b. Place LP cocks, located on forward left panel, down to SHUT position.

c. Place the master armament safety switch and key, located on the forward left panel down to the OFF position.

NOTE: Fire extinguisher switches are located on the forward instrument panel.

d. Lift and pull the electric crash switch, located aft on the left console, to isolate and discharge the fire extinguishers in the engine compartments.

WARNING

WARNING

1dELECTRIC CRASH SWITCH

1aTHROTTLES/HP COCKS

1cMASTER ARMAMENTSAFETY SWITCH WITH KEY

FIREEXTINGUISHERSWITCHES

FORWARD COCKPIT

1bLPCOCKS

TORNADO F3T.O

. 00-105E-9

TOR

NA

DO

F3.6


Seat pan must be fitted to both forward and aft seats before attempting further rescue of either crew member.




c. Insert canopy jettison initiator unit, located between cockpits, safety pin.



b. Release arm restraint straps by pressing plungers. Place aside the right and left shoulder straps.

c. Remove PEC, located on left side of seat, by pulling up from seat which also releases leg restraints straps.

d. Release PSP, located left side of seat, by pressing plung ers and lay aside.

e. Release QRB, located left side of seat, by turning and pressing. Pull out lugs.


WARNING2aFACE MASK

2bARM RESTRAINTS

2cPEC

1bLOWEREJECTIONHANDLE

1bLOWEREJECTIONHANDLESAFETYPIN

2dPSP

2eQRB

2bARM RESTRAINTS

1bCANOPY JETTISON SAFETY PIN

SEAT PANFIRINGHANDLE(STOWAGEPOSITION)

1bCANOPYJETTISON INITIATOR

TORNADO GR MK 1AT.O

. 00-105E-9

TOR

NA

DO

GR

MK

1A. 1

AIRCRAFT DIMENSIONS




TORNADO GR MK 1AT.O

. 00-105E-9

TOR

NA

DO

GR

MK

1A.

2

AIRCRAFT HAZARDS

Ammunition Box360 Rounds of Ammunition

WEAPONS PYLONS

NOTE: A variety of missles are carried externally on 9 pylons.

CANONS

OTHER HAZARDS:Battery acidAssisted escape systemAsbestosBeryllium + beryllium oxidesBromochlorodifluoromethane (BCF Fire Extinguishant)Bromotrifluoromethane (BTM Fire Extinguishant)Cadium (Battery/Bolt protection/Steel protectionCartridge operated equipmentComposite Materials (Man-made mineral fibres)CoolanolChaff DispenserDimethylformamide (Strobe power pack)Ejector release unitsFlare dispenserLithium (Batteries)Mercury (Temperature bulbs)Miniature Detonating Cord (MDC)PolytetrafluoroethylenePotassium HydroxideRadioactive sourcesSonar locator beacon(s) (1-Lithium battery)ThalliumThorium FluorideWeapon LoadZinc SelenideFuel: AvturHydraulic oil: OM-15High pressure gases: NitrogenEngine oil: OX-26Oxygen: LOX

TORNADO GR MK 1AT.O

. 00-105E-9

TOR

NA

DO

GR

MK

1A.

3


OXYGEN CYLINDERAT SEAT POSITIONS

FUEL

NITROGENCYLINDER

NITROGENCYLINDER

BATTERY

LIQUIDOXYGENCONTAINER


OIL TANKSFLIGHTRECORDER

EXTERNAL FUEL TANKS MAY BEFITTED IN POSITIONS SHOWN

BATTERY

TORNADO GR MK 1AT.O

. 00-105E-9

TOR

NA

DO

GR

MK

1A.

4

SPECIAL TOOLS/EQUIPMENTPower Rescue SawCrash AxAIRCRAFT ENTRY

1. NORMAL ENTRY

a. Press access door, located on left side of the fuselage, release lever and pull lever to STOP position.

2. MANUAL ENTRY

a. Pull yellow/black marked O-handle, located behind normal entry release lever, to STOP position. (Not illustrated.)

b. Press canopy upwards and install steadying strut.

3. EMERGENCY ENTRY

Personnel other than the operator of the emergency release explosive canopy handle must stand well clear of the aircraft. Handle is located on port side of aircraft and has Mild Detonating Cord (MDC)installed.

a. Break the frangible panel, located on the left side of the fuselage, by striking it in the center with the heel of the hand with fist clenched, to expose emergency canopy handle.

b. Grasp the emergency canopy handle with the right hand and move forward and away along a line approximately 45 degrees to the fuselage until the cable becomes taut.

c. Facing away from the aircraft with handle in the right hand, pull the handle sharply.

4. CUT-IN


WARNING

1aACCESSDOOR

3bCANOPY EMERGENCY HANDLE

3aWINDOW

3bCABLE

BREAK GLASS PULL

HANDLE CENTER

OF CABLE THEN TUG

TORNADO GR MK 1AT.O

. 00-105E-9

TOR

NA

DO

GR

MK

1A.

5


Before operating crash switches, the throttles must be selected back to HP SHUT position.

Failure to follow the above procedure will cause the engines to rapidly accelerate, possibly to destruction.

NOTE: Thumb plates must be pushed forward to allow the throttle/HP cocks to be selected fully back to SHUT position.

a. Pull fully back the throttles/HP cocks, located on the left console.

b. Place LP cocks, located on forward left panel, down to SHUT position.

NOTE: Fire extinguisher switches are located on the forward instrument panel.

c. Lift and pull the electric crash switch, located aft on the left console, to isolate and discharge the fire extinguishers in the engine compartments.

WARNING

WARNING

1cELECTRIC CRASH SWITCH

1aTHROTTLES/HP COCKS

FORWARD COCKPIT

1bLPCOCKS

TORNADO GR MK 1AT.O

. 00-105E-9

TOR

NA

DO

GR

MK

1A.

6


Seat pan must be fitted to both forward and aft seats before attempting further rescue of either crew member.




c. Insert canopy jettison initiator unit, located between cockpits, safety pin.



b. Release arm restraint straps by pressing plungers. Place aside the right and left shoulder straps.

c. Remove PEC, located on left side of seat, by pulling up from seat which also releases leg restraints straps.

d. Release PSP, located left side of seat, by pressing plung ers and lay aside.

e. Release QRB, located left side of seat, by turning and pressing. Pull out lugs.


WARNING2aFACE MASK

2bARM RESTRAINTS

2cPEC

1bLOWEREJECTIONHANDLE

1bLOWEREJECTIONHANDLESAFETYPIN

2dPSP

2eQRB

2bARM RESTRAINTS

1bCANOPY JETTISON SAFETY PIN

SEAT PANFIRINGHANDLE(STOWAGEPOSITION)

1bCANOPYJETTISON INITIATOR

TORNADO GR4T.O

. 00-105E-9

TOR

NA

DO

GR

4.


1

TO 00-105E-9

Chapter 27 Cover

NOTE

Chapter 27 contains emergency rescue andmishap response information for the following NATO aircraft:

GEU, FRA, ITA ATLANTIC BR 1150 GBR CANBERRA PR7 GBR CANBERRA PR9 GBR CANBERRA T4 GBR CANABERA TT18 FRA FALCON 50 MARINE NLD, ESP FOKKER 50 ITA MB 326 ITA MB 339 GBR NIMROD MR. MK 2P GBR NIMROD R-1

CAN,GRC,NOR,PRT,ESP,USA P-3/CP-140/CP-140A

* Aircraft information pending

T.O. 00-105E-9

27-1. INTRODUCTION AND USE.

27-2. 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.

27-3. GENERAL ARRANGEMENT.

27-4. Aircraft type designation has been positionedin the upper right corner of the horizontal illustrationfor rapid identification. Additional aids to rapid orien-tation are:

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

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

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

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

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

f. Details are pulled directly from the illus-tration to highlight an area, thus eliminating unnec-essary searching for desired information.

CHAPTER 27

NATO

BOMBER/MARITIME

AEROSPACE EMERGENCY RESCUEAND MISHAP RESPONSE INFORMATION

27-1

ATLANTIC BR 1150T.O

. 00-105E-9

ATLA

NT

IC B

R 1150. 1

FUEL TANKS

ARMAMENT:TORPEDOSDEPTH CHARGESMISSLES

AFTER DOOR

PRESSUREDOOREMERGENCY

OVERHEADOUTWARDHATCH

2a, 2bEMERGENCYESCAPE HATCHES

1aNORMAL ANDEMERGENCYDOWNWARDOUTWARDHATCH


AIRCRAFT ENTRY

1. NORMAL ENTRY

a. Pull release lever of hatch cover, located aft section lower side of the fuselage, and clasp hatch cover downwards.

b. Go up steps leading forward, located inside of the fuselage, to the pressure cabin door.

c. Pull the sliding bolt of the cabin door to the right and push door inwards, up to STOP position.

2. EMERGENCY ENTRY

a. Escape hatches are located on both sides overwing.

b. Pull red or yellow/black marked lever, located above window, turn lever clockwise to STOP position and remove hatch.

c. Disconnect dinghy pack, located on the step, and clasp step outwards.

3. CUT-IN

a. Marked cut-in areas are located on both sides aft fuselage and one at the top side of fuselage. Cut-in along marked areas.

b. Disconnect fuselage extension from the tail, by cutting or pulling.

DIMENSIONSWING SPAN 119 ‘ 1” (36.30 M)HEIGHT 37’ 2” (11.33 M)LENGTH 104 ‘ 2” (31.75 M)

ATLANTIC BR 1150T.O

. 00-105E-9

ATLA

NT

IC B

R 1150.

2

ENGINE SHUTDOWN ANDAIRCREW EXTRACTION1. ENGINE SHUTDOWN

a. Pull the three yellow/black marked fire “T” handles located center pilot’s overhead panel, up to STOP position.

b. Depress the yellow/black marked “CRASH- BAR”, located left beside the fire “T” handles of the pilot’s overhead panel.


NOTE: All crewmembers, except the pilot and co-pilot, are secured by safety belts. Crew size is 12.

a. Open the quick releases, located at each mid- section of crewmembers, and lay belts aside.

b. Rotate outer assembly to teh left or right until shoulder straps are released. Lay straps aside.

NOTE: Do not remove parachute harness. Transpor tation of injured crewmember will be easier.

1aEMERGENCY FIRET-HANDLES

ENGINEPOWERLEVERS

BATTERYSWITCH

1bCRASH BAR

ENGINEPOWERLEVERS

CANBERRA PR7T.O

. 00-105E-9

CA

NB

ER

RA

PR

7.1

AIRCRAFT HAZARDS

FUEL TANKS

WING TIP FUEL TANKS MAY BE FITTED

ENGINE INTAKEDANGER AREAS

JET ENGINE EXHAUST DANGER AREAS

OXYGEN CYLINDERS

OXYGEN CYLINDERS

OXYGEN CYLINDERLOCATED AT EACHSEAT POSITION

HYDRAULICFLUIDRESERVOIR

BATTERY

THIS BATTERY ONLY FITTEDWHEN CAMERA USED

BATTERIES

OTHER HAZARDS:Battery acidAssisted escape systemBeryllium + beryllium oxidesBromochlorodifluoromethane (BCF Fire Extinguishant)Bromotrifluoromethane (BTM Fire Extinguishant)Cartridge operated equipmentChlorobromoethane (Fire Extinguishment)CoolanolChaff DispenserDimethylformamide (Strobe power pack)Ejector release unitsFlare dispenserGround Illuminating Flare DispenserIsopropyl Nitrate (AVPIN)Lithium (Batteries)Methyl Bromide (Fire Extinguishment)Radioactive sourcesSonar locator beacon(s) (1-Lithium battery)Strontium ChromatesFuel: AvgasHydraulic oil: OM-15High pressure gases: NitrogenEngine oil: OMD-160Oxygen: NIL

CANBERRA PR7T.O

. 00-105E-9

CA

NB

ER

RA

PR

7. 2


AIRCRAFT ENTRY

1. NORMAL ENTRY

a. Open entry door, located on right fuselage below cockpit level, by using moderate hand pressure.

b. Rotate handle, located bottom center of door, counterclockwise.

2. EMERGENCY ENTRY

a. Break in through navigator’s escape hatch or pilot’s canopy.

3. CUT-IN

a. Cut-in areas are marked by broken yellow lines.

1aNORMALENTRYDOOR

1aNORMALENTRYDOORHANDLE

2aPILOT’SCANOPY

2aNAVIGATOR’SESCAPEHATCH

CANBERRA PR7T.O

. 00-105E-9

CA

NB

ER

RA

PR

7.3


a. Pull throttle and HP cocks, located on the left console, back to OFF.

b. Set LP cocks, located on upper left console, to OFF.

c. Set battery isolation switch, located on upper left console, to OFF.

NOTE: Safety pin stowage area located on right console.

1aTHOTTLESAND HP COCKS

1bLP COCKS

1cBATTERYISOLATIONSWITCH

SAFETY PINSTOWAGE

CANBERRA PR7T.O

. 00-105E-9

CA

NB

ER

RA

PR

7.4


a. Insert main gun sear safety pin located on top of seat.

b. If time permits, fit remaining safety pins to render ejection seat safe.



b. Disconnect emergency oxygen supply.

c. Disconnect main oxygen supply.

d. Release PSP.

e. Disconnect Microphone/Telephone.

f. Release seat harness. Also releases negative G strap and leg restraints.

g. Release QRB. Turn and press pull out lugs.

h. Remove crewmember.

i. Fit remaining safety pins to render ejection seat safe if not previously done.

2aFACEMASK

1aMAIN GUNSEAR SAFETYPIN

2eMICROPHONE/TELEPHONE

2bEMERGENCYOXYGENSUPPLY2cMAIN OXYGENSUPPLY

2dPSP

2fSEAT HARNESS

2gQRB

CANBERRA PR9T.O

. 00-105E-9

CA

NB

ER

RA

PR

9.1

AIRCRAFT HAZARDS

FUEL

ENGINE INTAKEDANGER AREA

JET ENGINE EXHAUSTDANGER AREA

OXYGENCYLINDERS

HYDRAULIC FLUIDRESERVOIRS

AVPIN TANK

AVPIN TANK

BATTERIES

OXYGENCYLINDERLOCATED ATEACH SEATPOSITION

NOTE: One aircraft has rear battery moved forward.

WING TIP FUEL TANKS MAY BE FITTED


CANBERRA PR9T.O

. 00-105E-9

CA

NB

ER

RA

PR

9.2


AIRCRAFT ENTRY

1. NORMAL ENTRY

a. Open navigator’s escape hatch, located on starboard (RT) side of fuselage, by the external release handle at forward end of hatch. Press and turn handle.

b. Entry to navigator via hinged nose. Handle is recessed in port (LH) side.

c. Open pilot’s canopy handle, located on port side of fuselage, by pressing the recessed release handle and turning clockwise.

2. EMERGENCY ENTRY


3. CUT-IN


1aNAVIGATOR’SESCAPE HATCH

1aRELEASEHANDLE

1bHINGEDNOSE

1cPILOT’SCANOPYHANDLE

2aNAVIGATOR’SHATCH

2aPILOT’SCANOPY

CANBERRA PR9T.O

. 00-105E-9

CA

NB

ER

RA

PR

9.3



b. Set LP cocks, located on right console, to OFF.

c. Set battery isolation switch, located on right console, to OFF.

NOTE: Safety pin stowage area located on upper left panel above the throttles.

1aTHOTTLESAND HPCOCKS

1bLP COCKS

1cBATTERYISOLATIONSWITCH

SAFETY PINSTOWAGE

CANBERRA PR9T.O

. 00-105E-9

CA

NB

ER

RA

PR

9. 4






b. Release PEC by pulling up to free from seat, also releases leg restraint straps.

c. Release PSP.

d. Release QRB. Turn and press pull out lugs.


f. Fit remaining safety pins to render ejection seat safe if not previously done.

2aFACEMASK

1aMAIN GUN SEARSAFETY PIN

2bPEC

2dQRB

2cPSP

CANBERRA T4T.O

. 00-105E-9

CA

NB

ER

RA

T4. 1

AIRCRAFT HAZARDS


JET ENGINE EXHAUST DANGER AREA

OXYGENCYLINDERS

HYDRAULIC FLUIDRESERVOIR

BATTERIES


FUEL TANKS - WING TIP FUEL TANKS MAY BE FITTED


BATTERY

NOTE: No armament is carried.

CANBERRA T4T.O

. 00-105E-9

CA

NB

ER

RA

T4.

2


AIRCRAFT ENTRY

1. NORMAL ENTRY



2. EMERGENCY ENTRY


3. CUT-IN


1aNORMALENTRYDOOR


2aPILOT’SCANOPY


CANBERRA T4T.O

. 00-105E-9

CA

NB

ER

RA

T4.

3



b. Set throttles and HP cocks, located on the right console, back to OFF.

c. Set LP cocks, located on right console, to OFF.

d. Set battery isolation switch, located on right console, to OFF.

NOTE: Safety pin stowage area located on upper left panel above the throttles.

1aTHOTTLESAND HPCOCKS

1cLP COCKS

1dBATTERYISOLATIONSWITCH

SAFETY PINSTOWAGE

1bTHOTTLESAND HPCOCKS

CANBERRA T4T.O

. 00-105E-9

CA

NB

ER

RA

T4.

4








d. Release PSP.






2aFACEMASK




2dPSP

2fSEAT HARNESS

2gQRB

CANBERRA TT18T.O

. 00-105E-9

CA

NB

ER

RA

TT

18. 1

AIRCRAFT HAZARDS


JET ENGINE EXHAUST DANGER AREA

OXYGENCYLINDERS

HYDRAULIC FLUIDRESERVOIR

BATTERIES


FUEL TANKS -WING TIP FUELTANKS MAY BEFITTED


BATTERY

NOTE: No armament is normally carried.

CANBERRA TT18T.O

. 00-105E-9

CA

NB

ER

RA

TT

18. 2


AIRCRAFT ENTRY

1. NORMAL ENTRY



2. EMERGENCY ENTRY


3. CUT-IN


1aNORMALENTRYDOOR


2aPILOT’SCANOPY


CANBERRA TT18T.O

. 00-105E-9

CA

NB

ER

RA

TT

18.3



b. Set LP cocks, located on right side of forward instrument panel, to OFF.

c. Set battery isolation switch, located behind pilot’s seat, to OFF.

1aTHOTTLESAND HP COCKS

1bLP COCKS

1cBATTERY ISOLATION SWITCH (Behind Pilot Seat)

CANBERRA TT18T.O

. 00-105E-9

CA

NB

ER

RA

TT

18.4








d. Release PSP.






2aFACEMASK




2dPSP

2fSEAT HARNESS

2gQRB

FALCON 50 MARINET.O

. 00-105E-9

FALC

ON

50.

AIRCRAFT PAINT SCHEME

1

FALCON 50 MARINET.O

. 00-105E-9

FALC

ON

50.2

AIRCRAFT DIMENSIONS

13.05 FT(3.98 M)

TAIL SPAN 29.35 FT (7.740 M)

WING SPAN 61.86 FT (18.858 M)

HEIGHT22.83 FT(6.975 M)

LENGTH 60.75 FT(18.516 M)

23.75 FT(7.239 M)

FALCON 50 MARINET.O

. 00-105E-9

FALC

ON

50.

AIRCRAFT HAZARDS

3

ENGINE INTAKE AND DANGER AREA

ENGINE EXHAUST GASES AND DANGER AREA

RADAR EMMISSIONS DANGER AREA

ENGINE #2

ENGINE #1

ENGINE #3

APU

FIRE EXTINGUISHER INBAGGAGE COMPARTMENT

FIREEXTINGUISHERBOTTLES FOR ENGINES

APU FIREEXTINGUISHER BOTTLE

FIRE ZONE FOR APU

ENGINE FIRE ZONES

ENGINE FIRE ZONES (ENGINES #1 & #3)

1. AIRCRAFT HAZARDS FOR ENGINES, APU, AND RADAR

2. ON BOARD FLARES

4 GREEN FLARES4 SMOKE FLARES (10 minutes)2 GREEN SMOKE FLARES (30 minutes)2 GREEN SMOKE FLARES (100 minutes)

FALCON 50 MARINET.O

. 00-105E-9

FALC

ON

50.


4

1. AIRCRAFT SYSTEMS HAZARDS

FUEL TYPE USED: F34-F35 JET A1MAXIMUM MASS OF FUEL:15,513 LBS2,316 GALS8,763 LITRES7,037 KG

HYDRUALIC FLUID:MIL - H - 5606NATO H515 OR H5202 RESERVOIRS: 12 LITRES

HIGH PRESSURE OXYGEN BOTTLE METER

OXYGEN BOTTLE

HIGH PRESSURE LINES

CO-PILOT’SOXYGEN METER

FUELDRAINS

DRAINS

FUEL

OXYGEN

BATTERY

RED LIMIT YELLOW LIMIT

FILL/INTAKE

TRIGGERAIR DISTRIBUTION

OXYGEN GENERATION EQUIPMENT LOCATIONS

FUEL SYSTEM LOCATIONS

INSPECTION DOOR

INSPECTION DOOR

SEPARATED WALL

FILL COVER

HOLE

INSPECTION DOORINSPECTION DOOR

FUEL VENT (DEPRESS)

SEALED &SLANTED

FALCON 50 MARINET.O

. 00-105E-9

FALC

ON

50. 5


AIRCRAFT ENTRY

1. NORMAL ENTRY

a. Open entry door, located on forward left side of thepassenger cabin. At the upper right side of the door,push on the safety button above exterior handle torelease the exterior handle from the release catch.

b. After unlock handle is released, pull handle outward.Follow the door downward preventing freefall. Door willnow be extended exposing entry steps.

2. EMERGENCY ENTRY AND EXITS

NOTE: The aircraft must be depressurized to permit the

emergency exits to open.

a. Emergency exit doors are located over left or right wings.

b. Break red cover above the door window, press exposedred button to open the door. Lift and remove exit door.Do not block opening and egress pathway.

3. INTERNAL ESCAPE WINDOWS

NOTE: Use the flightdeck side escape window when the entry

door and emergency exit door are blocked.

a. Break glass escape window, push button on internalunlock handle, lift handle, push window aft in slide rail.

4. CUT-IN

a. Cut-in cabin enclosure as indicated.

2aEMERGENCY EXIT DOOR WITH RED COVER

1aEXTERIORHANDLERELEASECATCH

1bEXTERIORHANDLE

3aSIDE ESCAPEWINDOW

3aUNLOCKHANDLE

3aUNLOCKHANDLEPUSHBUTTON

NORMAL ROUTE

EMERGENCY ROUTE

1aPUSHBUTTON

2bDOOR WITH WINDOW

1bENTRY DOORWITH STEPS

FALCON 50 MARINET.O

. 00-105E-9

FALC

ON

50.


a. Place the five (BAT 1, BAT2, GEN 1, GEN 2, & GEN 3)shutoff power generator switches, located on theoverhead panel, to the OFF position.

b. Move the three fuel levers, located on center consoleforward of the flaps controls, to the STOP position(completely aft) to insure the normal shutoff of theengines.

c. Pull all three fire pull handles, located on the forwardinstrument panel, to the OUT position to insure themechanical closure of the three fire stop “taps” andshutoff the fuel supply.

1aPOWER GENERATOR SWITCHES

1cFIRE PULLHANDLES

1bFUEL LEVERS

1bFLAPS

6

1bFLIGHT DECK FWDINSTRUMENT PANEL

FALCON 50 MARINET.O

. 00-105E-9

FALC

ON

50.7

APU SHUTDOWN

APU PANEL

RIGHTCONSOLE

1eMASTER

1aBLEED

1bSTOP

1cOIL

1dGENERATOR

1. APU SHUTDOWN (IF OPERATING)

NOTE:APU panel has illuminated buttons, located on the aft rightconsole at the co-pilot station. All buttons are spring loaded.

a. Push the BLEED button placing button in the OFF position.

b. Push the STOP button placing button in the OFF position.

c. The OIL indicator will illuminate if 40%>N1>30%.

d. Push the GEN button placing button in the OFF position.

e. Push the MASTER button placing button in the OFF position.(When N1 = 0% and T5 changes towards 200 degrees C)

FALCON 50 MARINET.O

. 00-105E-9

FALC

ON

50.

CABIN CONFIGURATION, EVACUATION PLANAND AIRCREW/PASSENGER EXTRACTION

8

2aFORWARDPASSENGEREVACUATION

2bAFTPASSENGEREVACUATION

2b AFTPASSENGEREVACUATION

2cFLIGHTDECKWINDOW

O2 MASK & BOTTLE

HALON FIREEXTINGUISHERCOLLECTIVE

FIRST AID ANDTRAUMA KIT

O2 MASKS

1. CABIN CONFIGURATION

a. Maximum capacity: 7Aircrew: 2Operators: 3Additional seating: 2

2. EVACUATION PLAN

a. Forward seated occupants will use the normal entry door.

b. Aft seated occupants will use theemergency exits over the wings.

c. In extreme cases where entry doorand emergency doors are blocked,the flightdeck window will be used.


a. Remove restraints from crew. Crewstations are equipped with shoulderand safety belts. Pull the centerrelease to unlock all restraints.

b. Remove restraints from passengers.Passengers will be equipped withsafety belts. Pull the center beltconnector to unlock the restraints.

DFDR RECORDER

ANTI SMOKEHEADCOVER

4 SAR CHAINS

LIFE JACKETS

ANTI SMOKEGOGGLES

AXE

WATERPROOF SUITS

2 COLLECTIVEFLOTATIONDEVICES

ACUSTICESAX 2A

ACUSTICELT96

EMERGENCY & RESCUE EQUIPMENT

EVACUATION PLAN AND ROUTES

CVR RECORDER

FOKKER 50T.O

. 00-105E-9

FO

KK

ER

50.

AIRCRAFT HAZARDS

1

LENGTH 82’ 10” (25.2 M)

AIRCRAFT DIMENSIONS

WING SPAN 95’ 1.75” (29 M)

HEIGHT27’ 3.5”(8.3 M)

DANGER AREA: RADAR RADIATION

2400

R= 20’ (6 M)

DANGER ZONES: ENGINES AND PROPELLERS

IDLE POWER

V= 56KM/H27M89’

V=8KM/H2.25 M7.4’

25 C0

0 0 0 037 C 30 C 20 C 15 C

TAKE OFFPOWER

V=96.5KM/H54 M178’

V=120 KM/H44 M145’

V=161KM/H33 M109’

V=241KM/H 27 M 89’

V=8 KM/H 7 M 23’

0M0’

1M3.3’

FUEL: 1356 US GAL 1130 IMP GAL 5136 LITRES

CREW: 3

PASSENGERS: MAXIMUM 30

FOKKER 50T.O

. 00-105E-9

FO

KK

ER

50.


MAIN FUEL TANK

MAIN FUEL TANK

OXYGEN BOTTLE

HYDRAULIC RESERVOIR

HYDRAULIC ACCUMULATORS

FIRE EXTINGUISHERBOTTLE (ON STEPS) HYDRAULIC

ACCUMULATORBATTERIES

FIREEXTINGUISHERBOTTLES

FUELCOLLECTORTANK

FUELCOLLECTORTANK

APU

SAFETYPIN BOX

FIREEXTINGUISHERBOTTLE

FIREEXTINGUISHERBOTTLE

OXYGENBOTTLE

OXYGEN BOTTLE

FIRST AID KIT

FUEL INFORMATIONCOLLECTOR FUEL TANK 13 GAL (49.2 LITRES)INTEGRATION TANK (2 INNER TANKS) 475 GAL (1797.5 LITRES) EACHENLARGED INTERNAL MAIN TANKS 670 GAL (2535 LITRES) EACHPYLON TANK 250 GAL (946 LITRES) EACH (OPTIONAL)

ENGINE OILLOCATED ON TOP OF FORWARDENGINE NACELLE

PNUEMATIC BOXLOCATED BY MAIN ENTRY DOOR

NO ARMAMENT IS CARRIED(MARITIME MISSIONS)

APU

FIRE EXTINGUISHERBOTTLE

APU AIRINTAKE

APUEXHAUST

2

EMERGENCY ESCAPE HATCHES

REAR CARGO DOOR

COCKPIT VOICE RECORDERANDFLIGHT DATA RECORDER

FOKKER 50T.O

. 00-105E-9

FO

KK

ER

50.

SPECIAL TOOLS/EQUIPMENTSkin Penetration ToolPower Rescue SawCrash Ax

AIRCRAFT ENTRY

1. CARGO AND REAR ENTRY

a. Lift handle at “PUSH”.

b. Rotate handle counterclockwise to ‘OPEN”.

c. Pull door upwards.

2. FORWARD PASSENGER DOOR

a. Lift door hand at “PUSH”.

b. Turn handle to “OPEN”.

c. Pull door outward. Use caution, door may open rapidly.

3. EMERGENCY ESCAPE HATCHES

a. Push access panel, located on top center of escape hatch, pull hatch outward, and set aside. Enter aircraft.

4. CUT-IN

a. Cut-in areas are applicable only if indicated on airframe. (Both sides of aircraft.)

3

FORWARDCARGO DOOR

SLIDING WINDOWS OPEN ONLYFROM INSIDE ESCAPE ROPEABOVE SLIDING WINDOWS (INSIDE)

OVERHEAD PANEL

FORWARDPASSENGER DOOR

FORWARD AND REAR CARGO DOOR

OPEN

OPEN

1a

1b1c

2a

2b

2c

FORWARD PASSENGER DOORFORWARD

FORWARD

EMERGENCY ESCAPE HATCH

CABIN ESCAPE ROUTES

CUT-IN AREAS LH/RH SIDES

SKIN PENETRATION AREA

FOKKER 50T.O

. 00-105E-9

FO

KK

ER

50.4

ENGINE SHUTDOWN ANDAIRCREW EXTRACTION1. ENGINE SHUTDOWN

NOTE: Configurations may vary.

a. Move gangbar or battery cut-off switch, located on overhead panel, DOWNWARD.

b. Pull emergency shut-off valves, located on upper forward instrument panel, OUT.

c. Move RPM and HPC control handles, located on center console, REARWARD.

d. Turn crossfeed valve control, located on aft portion of center console, OFF.

e. If needed, pull emergency fuel and hydraulic shut-off handles, located on overhead panel, OUTWARD.


NOTE: Crew of two and one observer are located in cockpit. Ejection seats are not used. Seats are equipped with shoulder harnesses and seat belts. Cabin attendant seats may also be equipped with same type restraints.

a. Disconnect shoulder harnesses and seat belts from crewmembers and cabin attendants.

b. Disconnect seat belts from passengers.

1aGANGBAR

1eEMERGENCY FUEL AND HYDRAULIC SHUT-OFF HANDLES

1aBATTERY CUT-OFF SWITCH

OVERHEAD PANEL

1bEMERGENCYSHUT-OFFVALVES

1dCROSSFEED VALVECONTROL

1cRPM AND HPCCONTROL HANDLES

MB 326T.O

. 00-105E-9

MB

326.1


AIRCRAFT ENTRY

1. NORMAL ENTRY

a. Push button on external locking handle, located on forward left fuselage, to expose recessed handle.

b. Pull recessed handle and rotate clockwise to unlock canopy.

c. Raise canopy to full open position. (Canopy is hinged on right side.)

2. EMERGENCY ENTRY

a. Push button on emergency canopy jettison access door.

b. Pull canopy jettison handle to full 2 meter length to jettison canopy.

3. CUT-IN

a. Cut canopy along canopy frame.

FUEL TIP TANK

INTERNAL FUEL TANKS

BATTERY

FUEL TIP TANK

OXYGEN CYLINDERS

1aBUTTONAND EXTERNALLOCKING HANDLE

2aBUTTON

2bCANOPY JETTISONHANDLE

UNLOCKED

LOCKED

PUSH

MB 326T.O

. 00-105E-9

MB

326. 2


a. Pull throttle to IDLE, located on left console, then move aft and outboard to stop (OFF) position.

b. Place fuel shutoff switch, located on upper left console, to OFF.

c. Place master switch, located on right console, to OFF.

NOTE: Oxygen switch is located above the master switch on right console.

d. If time permits, turn oxygen switch OFF.

1aTHROTTLE

1bFUEL SHUTOFF SWITCH

FUELSHUTOFF

1dOXYGEN SWITCH

1cMASTER SWITCH

MB 326T.O

. 00-105E-9

MB

326. 3

SEAT SAFETYING ANDAIRCREW EXTRACTION1. SEAT SAFETYING (MARTIN BAKER)

a. Insert safety pin in ejection gun sear, located at top of seat.

b. Insert safety pin in rocket initiator sear, located on upper left side of seat.

c. Insert safety pin in canopy jettison sear, located in forward cockpit left aft bulkhead.


a. Remove safety fork from harness quick release box.

b. Rotate outer assembly of quick release box 90 degrees clockwise and strike it to open and unlock belts.

c. Release of cut leg restraints and any further connections restricting the removal of the crew member.

d. Remove crew member’s oxygen mask and shut off oxygen switch. See location of page MB 326.2, item 1d.

2aQUICKRELEASEBOX

PRIMARY FIRINGHANDLE

1aEJECTION GUN SEAR

1bROCKET INITIATOR

1cCANOPY JETTISON SEARWITH SAFETY PIN

SECONDARY FIRINGHANDLE

MB 339T.O

. 00-105E-9

MB

339.

AIRCRAFT HAZARDS

1

WEAPONSPYLONS

WEAPONSPYLONS

LOAD AND ARMAMENT CAPABILITIES FOR MB 339C:BOMBS AND FLARESROCKET LAUNCHERS FOR 50, 68, 81 MM AND 2.75 IN ROCKETSLAU 10A OR TB 100-4 ROCKET LAUNCHERSECM PODBAGGAGE CONTAINERUNDER WING TANKS WITH 324 LITRES OF FUELSMOKE OR SMOKE/FUEL TANKGUN POD DEFA 30 MM GUN WITH 125 ROUNDS PER PODPHOTO RECONNAISANCE PODBOMBS/ROCKERS DISPENSERANTI-RUNWAY BOMBS BAP-100 OR TACTICAL SUPPORT BOMBS BAT-120MAVERICK A/G MISSLES (UP TO 2)MATRA 550 MAJIC OR AIM 9 SIDEWINDER A/A MISSLESMARTE MK 2 ANTI-SHIP MISSLE

AIRCRAFT DIMENSIONSWING SPAN WITH TIP TANKS 36’ 9.25” (11.22M)LENGTH 36’ 10.5” (11.24 M)HEIGHT 13’ 1” (3.99 M)

MB 339T.O

. 00-105E-9

MB

339.2


AIRCRAFT ENTRY

1. NORMAL ENTRY

a. Pull forward part of canopy locking handle, located on left side of fuselage, DOWNWARD, to unlock the canopy.

b. Raise the canopy to full open position. The canopy is hinged on right side.

2. EMERGENCY ENTRY

a. To access canopy fragmentation handle, located on left fuselage, push button to open access door.

b. Pull access door forward to expose fragmentation handle mounted on the backside of the access door.

c. Remove canopy fragmentation handle from secure clips and pull handle and cable full length to fragment canopies. (Both sides of canopy frame.)

3. CUT-IN

a. Cut along canopy frame on all sides.

FUEL TIP TANK

FUEL TIP TANKOXYGENCYLINDER

OXYGENCYLINDER

BATTERIES

INTERNALFUELTANKS

1aCANOPYLOCKINGHANDLE

2a, 2bACCESSDOOR

2cFRAGMENTAION HANDLEWITH CABLE

2aBUTTON

UNLOCK

LOCK

MB 339T.O

. 00-105E-9

MB

339.3


a. Raise idle dentent, located on left console forward of throttle, allowing throttle movement.

b. Pull throttle, located on left console, aft to OFF.

c. Place fuel shutoff switch, located forward of throttle on left console, to OFF.

d. Place battery switch, located on forward right panel, to OFF.

NOTE: Oxygen switch is located on left console below the throttle area.

1aIDLEDETENT

1cFUELSHUTOFFSWITCH

1bTHROTTLE

1dBATTERYSWITCH

OXYGENSWITCH

MB 339T.O

. 00-105E-9

MB

339.4


a. Safety ejection gun sear, located on top of seat by inserting safety pin.

b. Safety firing handle, located at bottom forward portion of seat, by inserting safety pin. Safety “T” pin in stored on left side of canopy frame, close to canopy handle.

NOTE: Safety pins are stored in recess on right side of seat.


a. Rotate outer assembly of harness quick release box, located on lap of crewmember, 90 degrees clockwise and strike it to open and unlock belts.

b. Move full aft leg restraint lever, located on right forward portion of seat to release garters.

c. Release or cut any further connections restricting aircrew extraction.

d. Remove crewmember oxygen mask and shutoff oxygen switch.

1bFIRINGHANDLE

1aGUNSEAR

2aHARNESSQUICKRELEASEBOX

1bLEGRESTRAINTLEVER

NIMROD MR.MK 2PT.O

. 00-105E-9

NIM

RO

D M

R.M

K 2P. 1

AIRCRAFT HAZARDSOTHER HAZARDS:Battery acidAsbestosBeryllium + beryllium oxidesBromochlorodifluoromethane (BCF Fire Extinguishant)Bromotrifluoromethane (BTM Fire Extinguishant)Cadium (Batteries/Bolt Protection/Steel Protection)Chlorobromoethane (Fire Extinguishment)Chaff DispenserDimethylformamide (Strobe power pack)Ejector release unitsFlare dispenserLithium (Batteries)Mercury (Temperature Bulbs)Methyl Bromide (Fire Extinguishment)Polytetrafluoroethylene (PTFE)Sonar locator beacon(s) (1-Lithium battery)Strontium ChromatesThalliumThorium FluorideTritium Light Sources (Beta Lights)Fuel: AvturHydraulic oil: OM-15High pressure gases: NitrogenEngine oil: OX-38Oxygen: Gaseous

RADIATIONDANGERAREA

HYDRAULICRESERVOIR

SIGNALPISTOL

PORTABLEOXYGEN

FUEL

HYDRAULICACCUMULATORS

APU OIL

PORTABLEOXYGEN

JET EFFLUXDANGER AREALIQUID

OXYGEN

ENGINE OILTANKS BOTHSIDES

PORTABLEOXYGEN

HYDRAULICACCUMULATORSAND RESERVOIR

AIR INTAKEAND REVERSERDANGER AREA

BATTERIES

30 METERS

PRESSURIZED COMPARTMENT

NIMROD MR.MK 2PT.O

. 00-105E-9

NIM

RO

D M

R.M

K 2P.2


ARMAMENT AREA

ARMAMENT:TORPEDOSBOMBSWEAPONS OR FUEL MAY BE IN BOMB BAYFLARESMARKERS OR SIGNALS

NAVIGATOR’S POSITIONS

WEAPON MASTER SWITCH

MASTER ARMAMENTSAFETY SWITCH

TORPEDO, STORES AND FLARESSELECTOR SWITCHES

TACTICAL NAVIGATOR’S POSITIONROUTINE NAVIGATOR’S POSITION

RETRO LAUNCHERMASTER SWITCH

SONOBUOY LAUNCHERSELECTOR SWITCH

NIMROD MR.MK 2PT.O

. 00-105E-9

NIM

RO

D M

R.M

K 2P. 3


AIRCRAFT ENTRY

1. NORMAL ENTRY

a. Doors are located on the forward right and aft left sides of the fuselage. Turn door handle to open, then push. Doors open inward.

2. EMERGENCY ENTRY

a. Escape hatches are located over each wing. To open, press handle at top of hatch, pull outward and set aside.

3. CUT-N

a. Emergency cut-in panels are located on top of fuselage at mid and aft cabin areas. Use the power rescue saw or crash ax to gain entry.

EMERGENCY CUT-IN PANELSAPU FIREPANEL

INTERNAL FIREINSPECTION PANEL

2aEMERGENCYESCAPEHATCH

INTERNAL FIREINSPECTIONPANEL

1aENTRYDOOR

HAND FIRE EXTINGUISHER

FIRST AID PACK

FIRE AX

GLOVES

SMOKE MASK

FIRE PANELS(2 PER ENGINE)

NIMROD MR.MK 2PT.O

. 00-105E-9

NIM

RO

D M

R.M

K 2P. 4


a. Release the safety catches on the HP fuel cocks, located on the center console.

b. Move the HP fuel cocks DOWN to limit of travel.

c. Place the battery master switch, located on the engineer’s panel aft of the right side window, to OFF.

In case of engine fire:

d. When fire warning lamps are illuminated, operate the engine fire extinguisher switches, located on the right and left overhead panels, to release fire extinguishant into the corresponding engine.

In case of APU fire:

e. Place APU master switch, located on right engineers panel, down to OFF.

ESSENTIAL SUPPLIES SWITCH

EMERGENCY LIGHT SWITCH

1cBATTERY MASTER SWITCH

ENGINEERS PANEL

ENGINE FIREEXINGUISHERSWITCHES

APU FIRE1eAPU MASTER SWITCH

1aHP FUELCOCKSHANDBRAKE LEVER

THROTTLE AND REVERSETHRUST LEVERS

NIMROD MR.MK 2PT.O

. 00-105E-9

NIM

RO

D M

R.M

K 2P. 5

AIRCREW EXTRACTION1. AIRCREW EXTRACTION

NOTE: Aircraft does not have ejection systems.

a. On crew seats, remove face masks before disconnecting hoses.

b. Release the seat harness by turning restraint release in either direction.

NOTE: Escape ropes are located at forward and rear main doors and escape hatches.

c. Forward main door can be opened by turning and pulling the internal door release handle. Door opens inward. Door is equipped with an escape chute.

d. Side escape hatches at port and starboard wings can be opened by pulling the emergency exit hatch handle located top center of hatch.

e. Main rear door can be opened by turning and pulling the internal door release handle. Door opens inward. The door is equipped with an escape chute.

NOTE: The aircraft is equipped with a ladder mounted at the rear.

1aCREW SEAT(TYPICAL)

1bSEAT HARNESS RELEASE

ESCAPE ROPESTOWAGE

INTERNALLADDER

1cFORWARDMAIN DOOR

1cFORWARDMAIN DOORHANDLE

1eREAR MAIN DOOR

1eREAR MAINDOOR HANDLE

REARMAINDOORSTEP(RAISED)

1dESCAPEHATCHWITHHANDLE(TYPICAL)

STOWAGE

PULL

YELLOWHOOKRED

HOOK

GREENBLUE

NIMROD R-1T.O

. 00-105E-9

NIM

RO

D R

-1.

AIRCRAFT HAZARDS

1

OTHER HAZARDS:Battery acidAsbestosBeryllium + beryllium oxidesBromochlorodifluoromethane (BCF Fire Extinguishant)Bromotrifluoromethane (BTM Fire Extinguishant)Cadium (Batteries/Bolt Protection/Steel Protection)Chlorobromoethane (Fire Extinguishment)Chaff DispenserDimethylformamide (Strobe power pack)Ejector release unitsFlare dispenserLithium (Batteries)Mercury (Temperature Bulbs)Methyl Bromide (Fire Extinguishment)Polytetrafluoroethylene (PTFE)Sonar locator beacon(s) (1-Lithium battery)Strontium ChromatesThalliumThorium FluorideTritium Light Sources (Beta Lights)Fuel: AvturHydraulic oil: OM-15High pressure gases: NitrogenEngine oil: OX-38Oxygen: Gaseous

RADIATIONDANGERAREA

HYDRAULICRESERVOIR

SIGNALPISTOL

PORTABLEOXYGEN

FUEL

HYDRAULICACCUMULATORS

APU OIL

PORTABLEOXYGEN

JET EFFLUXDANGER AREALIQUID

OXYGEN

ENGINE OILTANKS BOTHSIDES

PORTABLEOXYGEN

HYDRAULICACCUMULATORSAND RESERVOIR

AIR INTAKEAND REVERSERDANGER AREA

BATTERIES

11 METERS

PRESSURIZED COMPARTMENT

NO ARMAMENT IS CARRIED

NIMROD R-1T.O

. 00-105E-9

NIM

RO

D R

-1. 2


AIRCRAFT ENTRY

1. NORMAL ENTRY

a. Doors are located on the forward right and aft left sides of the fuselage. Turn door handle to open, then push. Doors open inward.

2. EMERGENCY ENTRY

a. Escape hatches are located over each wing. To open, press handle at top of hatch, pull outward and set aside.

3. CUT-N

a. Emergency cut-in panels are located on top of fuselage at mid and aft cabin areas. Use the power rescue saw or crash ax to gain entry.

EMERGENCY CUT-IN PANELSAPU FIREPANEL

INTERNAL FIREINSPECTION PANEL

2aEMERGENCYESCAPEHATCH

INTERNAL FIREINSPECTIONPANEL

1aENTRYDOOR

HAND FIRE EXTINGUISHER

FIRST AID PACK

FIRE AX

GLOVES

SMOKE MASK

FIRE PANELS(2 PER ENGINE)

NIMROD R-1T.O

. 00-105E-9

NIM

RO

D R

-1.3


a. Release the safety catches on the HP fuel cocks, located on the center console.

b. Move the HP fuel cocks DOWN to limit of travel.

c. Place the battery master switch, located on the engineer’s panel aft of the right side window, to OFF.

In case of engine fire:

d. When fire warning lamps are illuminated, operate the engine fire extinguisher switches, located on the right and left overhead panels, to release fire extinguishant into the corresponding engine.

In case of APU fire:

e. Place APU master switch, located on right engineers panel, down to OFF.

ESSENTIAL SUPPLIES SWITCH

EMERGENCY LIGHT SWITCH

1cBATTERY MASTER SWITCH

ENGINEERS PANEL

ENGINE FIREEXINGUISHERSWITCHES

APU FIRE1eAPU MASTER SWITCH

1aHP FUELCOCKSHANDBRAKE LEVER

THROTTLE AND REVERSETHRUST LEVERS

NIMROD R-1T.O

. 00-105E-9

NIM

RO

D R

-1.4

AIRCREW EXTRACTION1. AIRCREW EXTRACTION

NOTE: Aircraft does not have ejection systems.

a. On crew seats, remove face masks before disconnecting hoses.

b. Release the seat harness by turning restraint release in either direction.

NOTE: Escape ropes are located at forward and rear main doors and escape hatches.

c. Forward main door can be opened by turning and pulling the internal door release handle. Door opens inward. Door is equipped with an escape chute.

d. Side escape hatches at port and starboard wings can be opened by pulling the emergency exit hatch handle located top center of hatch.

e. Main rear door can be opened by turning and pulling the internal door release handle. Door opens inward. The door is equipped with an escape chute.

NOTE: The aircraft is equipped with a ladder mounted at the rear.

1aCREW SEAT(TYPICAL)

1bSEAT HARNESS RELEASE

ESCAPE ROPESTOWAGE

INTERNALLADDER

1cFORWARDMAIN DOOR

1cFORWARDMAIN DOORHANDLE

1eREAR MAIN DOOR

1eREAR MAINDOOR HANDLE

REARMAINDOORSTEP(RAISED)

1dESCAPEHATCHWITHHANDLE(TYPICAL)

STOWAGE

PULL

YELLOWHOOKRED

HOOK

GREENBLUE

P-3/CP-140/CP-140AT.O

. 00-105E-9

P-3.1

The aircraft information is located in Chapter 22 containing US Navy aircraft.

aircraft rescue info

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