WELCOME TO TECHNICAL ORDER 00-105E-9, 1 FEBRUARY 2006, … Segment 30.pdf · 2007. 12. 18. · to go directly to the technical order, click on the continue button. welcome to technical

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

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THIS IS SEGMENT 30 COVERING CHAPTER 30 from the Lynx MK7 to Sea King HAS/ASW/6.

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 Retaining out of date rescue information can negatively affect the user’s operability and outcome of emergencies.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 30 INFORMATION CHANGE NOTICE

None.

TO 00-105E-9

Chapter 30 Cover

NOTE

Chapter 30 contains emergency rescue andmishap response information for the following NATO aircraft:

ITA A 109ITA, TUR AB 204ITA, TUR AB 204A/SITA, TUR AB 206 TUR AB 212

ITA,TUR,ESP AB 212A/S USA, TUR AH-1 P/W

USA, GBR AH-64 TUR AS-532 DNK AS-550C2 GEU BO-105CB

CAN, ITA, USA, GBR CH-47/HC2/3 GEU, USA CH-53/H-53D,E

CAN CH-146* FRA ECUREUIL ALSTAR AS 355 FRA ECUREUIL 2* FRA FENNEC AS 555AN GBR GAZELLE AH1 GBR GAZELLE HT2 GBR GAZELLE HT3 ITA HH-3F* USA, TUR H/M/S/UH-60A,G,H,J,L S-70-28D USA, TUR HUGHES 300/MH-6 DNK, USA HUGHES 500/OH-6 GBR LYNX HAS 3 PRT LYNX LBH MK9 GBR LYNX MK3 GBR LYNX MK7 GBR LYNX MK8 DNK LYNX MK90B GBR LYNX MK95 FRA LYNX WG 13 GBR MERLIN TUR OH-13S

USA, TUR OH-58A/C/D GBR,FRA,ESP,PRT,TUR PUMA HC1/SA 330

BEL SA 313/318 BEL, FRA, PRT, NLD SA 316B/319B/SE 3160

FRA SA 341/342 GBR SEA KING AEW 2 GBR SEA KING ASW 5

GBR, ITA, ESP SEA KING HAR 3/SH 3D GBR SEA KING HAS/ASW/6 GBR SEA KING MK4 GBR SEA KING MK6 GBR SEA KING MK7

GEU,GBR,DNK,BEL,NOR SEA KING MK-41/HC-4/S-61/WESTLAND SAR GEU, DNK SEA LYNX MK-88 USA, ESP SH-60B FRA SUPER FRELON SA 321 FRA, ESP, NLD SUPER PUMA & COUGAR/HD-21

USA, ITA, GRE, NLD UH-1 USA, TUR, NOR UH-1N GBR WESSEX HC2/HC5C

* Aircraft information pending

LYNX MK 7T.O

. 00-105E-9

LYN

X M

K7.

AIRCRAFT PAINT SCHEME

1

LYNX MK 7T.O

. 00-105E-9

LYN

X M

K7.

AIRCRAFT DIMENSIONS

2

7FT 1.5IN(2.175M)

STATIC GROUND LINE

LENGTH43 FT 8 IN (13.24M)

HEIGHT12 FT 5 IN (3.775M)

4 FT 4 IN (1.32M)

BLADES FOLDED

LYNX MK 7T.O

. 00-105E-9

LYN

X M

K7.3

7FT 1.5IN(2.175M)

BLADE SPAN 42 FT (12.800M)

HEIGHT12 FT 5 IN (3.775M)

BLADES SPREAD

AIRCRAFT DIMENSIONS-Continued

5 FT 10 IN (1.776M)

50 FT 1 IN(15.239M)

4 FT 4 IN (1.322M)

POST-MOD 609

6 FT 1.5 IN (1.867M)

7 FT 9 IN(2.362M)

3 FT 9 IN(1.147M)

25 FT 1.6 IN (7.660M)

LENGTH39 FT 7 IN(12.000M)

LIGHT STATIC GROUND LINE

LYNX MK 7T.O

. 00-105E-9

LYN

X M

K7.

AIRCRAFT DATA AND HAZARD LIST

HAZARD TYPE ITEM QUANTITY LOCATION

Acid - Sulphuric On Aircraft

AL 36 Windscreen Wash Fluid On Aircraft

Asbestos On Aircraft

Avtur F-34 Fuel Fuel Internal 973 LExternal 2X436 L

Fuel Tanks

Beryllium - Beriliua (Beryllium Oxides) On Aircraft

Bromochlorodifluoro - Methane (BCF) On Aircraft

Composite Materials (Man MadeMinerals)

Airframe Materials Carbon Fibre RotorBlades

Dimethylformamide Strobe Power Packs

Flourolastomers Burnt Seals

Gaseous Tritium Light Sources Lights Beta Lights

Lithium (Non Rechargeable Batteries) Batteries Batteries

OEP-215 Engine Oil 6.8 L Engine


OM-15 Hydraulic Oil 20 L Hydraulic System

OX-38 Engine Oil 6.8 L Engine

Oxygen Nil

Sonar Locator Beacon(s) Sonor Beacon 1 On Aircraft

Weapon Load (if fitted) Weapon(s) Mission Variable Stub Wings

Zinc Selenide Flir Cockpit

HAZARD LISTAIRCRAFT DATA Single Rotor Helicopter Two Rolls-Royce Gem 41-1turboshaft Military Freight/Passenger: 2 crew Maximum 10 passengers Aircraft Weight: 8,000 lbs. (3,620 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):

Service issue overalls and gloves and Civil Emergency Services normal uniform with overall required. Appropriate weather protection. Safety helmet (as required). Half-face (ori-nasal) mask. Examples: 3M Disposable Mask 22G/1321426 Sabre Half Mask 22G/4220-99-865-4140 Baxter Half Mask 22G/4220-99-865-4149

WARNING

4

LYNX MK 7T.O

. 00-105E-9

LYN

X M

K7.

AIRCRAFT HAZARDS

5

THERMAL IMAGING TOW ROOF SIGHT

MISSILE COMMAND AMPLIFIER ELECTRONIC POWER SUPPLY UNIT

STABILISATION CONTROL AMPLIFIER UNIT

TOW MISSILELAUNCHERS (X2)AND LAUNCHERCARRIER ASSEMBLYON NATO FLANGE

INTERFACE UNIT

THERMAL IMAGINGELECTRONICS UNIT

HIGH PRESSURE PUREAIR GENERATOR (HIPPAG)

MACHINE GUN

TOW/TOWTI MISSILE SYSTEMSAND MACHINE GUN

STABILISATION CONTROL AMPLIFIER UNIT

INTERFACE UNIT

ELECTRONIC POWER SUPPLY UNIT

MISSILE COMMAND AMPLIFIER UNIT

TOW ROOF SIGHT

TOW MISSILE SYSTEM

TOWTI MISSILE SYSTEM

TOW MISSILELAUNCHERS (X2)AND LAUNCHERCARRIER ASSEMBLYON NATO FLANGE

LYNX MK 7T.O

. 00-105E-9

LYN

X M

K7.6

HANDHOLDSENGINE FIRE ACCESS(BOTH SIDES)

ACCESS TO BATTERY,FLOTATION & EXTINGUISHERBOTTLES

STEPS

STEP

FRONT DOORS -2 CREW

REAR DOORS -9 PASSENGERSOR STRETCHERS

2aJETTISONHANDLEINSIDE

1a, 1bEXTERNALENTRYHANDLES

EMERGENCYRELEASEPULL DOWN

HAND FIRE EXTINGUISHER FIRST AID KITS

2aEMERGENCYENTRY

HAND GRIPS

SPECIAL TOOLS/EQUIPMENTPower Rescue SawCrash Ax

AIRCRAFT ENTRY

1. NORMAL ENTRY

a. Turn external entry door handles up, pull forward door out and forwards. Slide rear door aft.

b. To open windows in rear doors, pull down release handle, pull windows outwards. ( A blade may have to be inserted between frame and door.)

2. EMERGENCY ENTRY

a. For forward door, slide window aft, push jettison forward and down. Pull outwards.

3. CUT-IN

a. Cut-in fuselage as required.

NOTE: Winch in main cabin may be swung out of way by pulling down cord on starboard side.

2bRELEASEHANDLE

LYNX MK 7T.O

. 00-105E-9

LYN

X M

K7.7

AIRCRAFT EXTERNAL VIEWS,DOORS, AND WINDOWS

ENGINEEXHAUST

ENGINE INTAKE

BATTERYCOMPARTMENT ROCKET

PODS REAR DOORHANDLE

PILOT DOORHANDLE

FIREACCESS PANEL

ENGINE INTAKE

ENGINEEXHAUST

REAR DOOR OPEN HANDLE

EMERGENCY WINDOW JETTISON HANDLE PILOT DOOR

OPEN HANDLE

LYNX MK 7T.O

. 00-105E-9

LYN

X M

K7. 8

COCKPIT AND CABIN DOORS

SWIVELCATCH

UPPERPLUNGERBOLT

LOWERPLUNGERBOLT

INTERNALHANDLE

SWIVELCATCH

SLIDINGWINDOWLOCKINGLEVER

HAND HOLD UPPERHINGE PIN

INDICATOR WIRE

EMERGENCYJETTISONLEVER

FWD

LOWERHINGE PIN

DOOROPENLATCHOPERATINGROD

FWD

A

B

C

COCKPIT DOOR

CABINDOOR1. INTERNAL VIEWS

LATCH

LATCHGUIDE

SPRINGSTRUT

INTERNAL HANDLEWITH BETA LIGHTINDICATOR WIRE

C

INTERNALHANDLE

EXTERNALHANDLE

B APLUNGER BOLT

SPIGOT

LYNX MK 7T.O

. 00-105E-9

LYN

X M

K7.9

ENGINE SHUTDOWN1. ENGINE SHUTDOWN WITH TOW AND TOWTI COCKPIT CONTROLS

a. Raise engine condition levers, located on overhead control console, UP (aft) to HP COCK OFF postion.

b. Place LP fuel cocks, located on overhead control console, aft to SHUT position.

c. Place master armament safety switch, located on forward instrument panel, to OFF position, if applicable.

d. Place battery master switch, OR, battery switch located on the overhead control console, to OFF position.

CIRCUIT BREAKER PANEL CX

TEST POWER SOCKET TEST

SOCKET 2 CIRCUITBREAKERPANEL CY

1aENGINECONDITIONLEVERS

PILOTSSTEERINGINDICATOR

MASS (3POSITION)

SUPPORT ARM WITHSIGHT HAND-CONTROLAND ARMREST(POST MOD 5543)

HANDWHEEL

LAUNCHER ACTIVATE PORT/STBD TEST SWITCH

LEFT HAND GRIP

TOW CONTROL PANEL

TOW ROOF SIGHT

TOW CONTROLS

TOWTI CONTROLS

PILOTSSTEERINGINDICATOR

MASS (3POSITION)


CIRCUITBREAKERPANEL CY

TESTSOCKET 2

TEST POWER SOCKET

CIRCUIT BREAKER PANEL CX

CONTROLLERARMREST AND SIGHT HAND CONTROL

LAUNCHER ACTIVATE PORT/STBD TEST SWITCH

THERMAL IMAGINGLEFT HAND GRIP

TOW CONTROL PANEL

THERMAL IMAGINGCONTROL UNIT

THERMAL IMIAGINGROOF SIGHT

THERMAL IMIAGINGDISPLAY UNIT

1d BATTERYSWITCH

1bLP FUELCOCKS

ENGINE FIREEXTINGUISHERS

LYNX MK 7T.O

. 00-105E-9

LYN

X M

K7.10

ENGINE SHUTDOWN-Continued

1cMASTERARMAMENTSAFETYSWITCH

1dBATTERYMASTERSWITCH


1bLP FUELCOCKS

1dBATTERYSWITCH

LYNX MK 7T.O

. 00-105E-9

LYN

X M

K7.

AIRCREW EXTRACTION ANDEMERGENCY EXIT DOORS

11 TELEMIC

BARREL

PSP

1aQRFHARNESSCONNECTION

-2 CREW, FRONT-9 CREW, AFT: TROOPS OR STRETCHERS IN REAR CABIN

1aFRONT SEAT

1bMID CABIN SEAT

1cREARSEAT

EMERGENCY EXITS

WINDOW

SLIDING WINDOW

NORMAL EXITHANDLES

BETA LIGHTS(RADIO ACTIVE)


2aREARCABINDOORLEVER

2aJETTISON LEVER

1. AIRCREW EXTRACTION

a. Release crew in forward seats by releasing the QRF harness connection and other associated connections.

b. Release crew in mid cabin seats by releasing restraint harnesses and other associated connections.

c. Release crew in rear seats by releasing restraint harnesses and other associated connections.

2. EMERGENCY EXIT DOORS

NOTE: Exit doors can be jettisoned to make extraction of crewmembers faster. (Also refer to page 8 for closer detail.)

a. For front doors, push jettison forward and down, then push door out.

b. For rear cabin doors, push jettison lever, located at bottom center of window, aft, then push window out.

LYNX MK 8T.O

. 00-105E-9

LYN

X M

K8.1


LYNX MK 8T.O

. 00-105E-9

LYN

X M

K8.2

AIRCRAFT DIMENSIONS

HEIGHT (3.594M)

BLADES SPREAD AND FOLDED

50 FT 1 IN(15.239M)

(1.322M)

(1.867M)

7 FT 9 IN(2.362M)

(1.147M)(7.731M)

LENGTH(12.333M)

2.778M2.940M

(4.502M) (12.500M)(4.496M)

STATIC GROUND LINESTATIC GROUND LINE

(3.014M) (10.854M) MAX OVERALL LENGTH (FOLDED)

HEIGHT (3.200M)MAX FOLDED

LYNX MK 8T.O

. 00-105E-9

LYN

X M

K8.3

AIRCRAFT DATA AND HAZARD LIST

HAZARD TYPE ITEM QUANTITY LOCATION

Acid - Sulphuric On Aircraft

AL 36 Windscreen Wash Fluid On Aircraft

Asbestos On Aircraft

Avtur F-34 Fuel Fuel Internal 973 LExternal 2X436 L

Fuel Tanks

Beryllium - Beriliua (Beryllium Oxides) On Aircraft

Bromochlorodifluoro - Methane (BCF) On Aircraft

Composite Materials (Man MadeMinerals)

Airframe Materials Carbon Fibre RotorBlades

Dimethylformamide Strobe Power Packs

Flourolastomers Burnt Seals

Gaseous Tritium Light Sources Lights Beta Lights

Lithium (Non Rechargeable Batteries) Batteries Batteries



OM-15 Hydraulic Oil 20 L Hydraulic System

OX-38 Engine Oil 6.8 L Engine

Oxygen Nil

Sonar Locator Beacon(s) Sonor Beacon 1 On Aircraft

Weapon Load (if fitted) Weapon(s) Mission Variable Stub Wings

Zinc Selenide Flir Cockpit

HAZARD LISTAIRCRAFT DATA Single Rotor Helicopter Two Rolls-Royce Gem 41-1turboshaft Military Freight/Passenger: 2 crew Maximum 10 passengers Aircraft Weight: 8,000 lbs. (3,620 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):

Service issue overalls and gloves and Civil Emergency Services normal uniform with overall required. Appropriate weather protection. Safety helmet (as required). Half-face (ori-nasal) mask. Examples: 3M Disposable Mask 22G/1321426 Sabre Half Mask 22G/4220-99-865-4140 Baxter Half Mask 22G/4220-99-865-4149

NOTE: For additional hazards, see the other Lynx MK models in this publication.

WARNING

LYNX MK 8T.O

. 00-105E-9

LYN

X M

K8.

4

HANDHOLDSENGINE FIRE ACCESS(BOTH SIDES)

ACCESS TO BATTERY,FLOTATION & EXTINGUISHERBOTTLES

STEPS

STEP

FRONT DOORS -2 CREW

REAR DOORS -9 PASSENGERSOR STRETCHERS

2aJETTISONHANDLEINSIDE

1a, 1bEXTERNALENTRYHANDLES


HAND FIRE EXTINGUISHER FIRST AID KITS

2aEMERGENCYENTRY

HAND GRIPS


AIRCRAFT ENTRY

1. NORMAL ENTRY



2. EMERGENCY ENTRY


3. CUT-IN



2bRELEASEHANDLE

LYNX MK 8T.O

. 00-105E-9

LYN

X M

K8.5

ENGINEEXHAUST

ENGINEINTAKE

FIREACCESS

NORMAL DOOR RELEASE

EMERGENCYWINDOW RELEASE

NORMAL DOOR RELEASE

AIRCRAFT EXTERNAL VIEWS,DOORS, AND WINDOWS

LYNX MK 8T.O

. 00-105E-9

LYN

X M

K8.6

ENGINE SHUTDOWN1. ENGINE SHUTDOWN

a. Raise engine condition levers, located on overhead control console, UP (aft) to HP COCK OFF postion.

b. Place LP fuel cocks, located on overhead control console, aft to SHUT position.

c. Place battery master switch, located on the overhead control console, to OFF position.

1cBATTERY MASTER SWITCH

OVERHEAD CONSOLE

ENGINE FIREEXTINGUISHERS

1bLP FUEL COCKS

1aENGINE CONDITION LEVERS

ROTORBRAKE

WARNING PANEL

CABIN LIGHTS

PILOTPOSITION

JETTISON

HARPOON

HOISTC0-PILOTPOSITION

DOORHANDLE (BOTH SIDES)

DOORJETTISON

LYNX MK 8T.O

. 00-105E-9

LYN

X M

K8.

7

AIRCRAFT FAMILIARIZATION

FLOTATION BOTTLES

BATTERY

INTERNALNORMALDOORRELEASE

MASTER ARMAMENT SAFETY SWITCH

INTERNALEMERGENCYWINDOWJETTISONHANDLE

LYNX MK 8T.O

. 00-105E-9

LYN

X M

K8.8


TELEMIC

BARREL

PSP

1aQRFHARNESSCONNECTION


1aFRONT SEAT

1bMID CABIN SEAT

1cREARSEAT

EMERGENCY EXITS

WINDOW

SLIDING WINDOW

NORMAL EXITHANDLES



2aREARCABINDOORLEVER

2aJETTISON LEVER


a. Release crew in forward seats by releasing the QRF harness connection and other associated connections.

b. Release crew in mid cabin seats by releasing restraint harnesses and other associated connections.

c. Release crew in rear seats by releasing restraint harnesses and other associated connections.


NOTE: Exit doors can be jettisoned to make extraction of crewmembers faster.

a. For front doors, push jettison forward and down, then push door out.


LYNX MK-90BT.O

. 00-105E-9

LYN

X M

K-90B

.


1

LYNX MK-90BT.O

. 00-105E-9

LYN

X M

K-90B

.

AIRCRAFT DIMENSIONS AND GENERAL INFORMATION

2

Rotor diameter 42 ft (12.8 m)

Dimensions (External):Overall Length Rotors Turning 15. 16 mFuselage Length 13. 33 mWidth (excluding rotor) 2. 94 mOverall Height 3. 48 mFolded Length 10. 85 mFolded Width 2. 94 mFolded Height 3. 25 mMain Rotor Diameter 12. 80 mTail Rotor Diameter 2. 36 m

Dimensions (Internal):Cabin Length 2. 05 mCabin Width 1. 78 mCabin Height 1. 42 m

Role:Utility, attack, antitank

Similar Aircraft:OH-58 Kiowa, Hirundo A109, UH-1Iroquois, UH-1N Model 212, Dauphin 2and multiple Lynx designations formany countries (See Jane’s -All The World’s Aircraft 2002-2003 page 488).

Armament:Cannon, minigun, rockets, missiles,HOT or TOW antitank missiles

Crew: 2 (Cockpit)VIP: 1 - 3 (Mid Cabin)Passengers - 2 (Rear Cabin)

LYNX MK-90BT.O

. 00-105E-9

LYN

X M

K-90B

. 3

TAIL ROTORMAIN ROTOR

BATTERYFUEL TANKS

ARMAMENT


AIRCRAFT ENTRY

1. NORMAL ENTRY

NOTE: The cockpit and cabin doors, located both sides of fuselage, are not droppable.

a. Turn exterior handle of cockpit door clockwise and open the door.

b. Turn exterior handle of cabin door clockwise, pull door outwards and slide aft or to the right.

2. EMERGENCY ENTRY

a. Press the marked button of the exit release on the sliding windows, located on both cabin doors, on either side of the fuselage.

b. Rotate handle clockwise to top position and pull the window outwards.

3. CUT-IN

a. Cut-in to windows or fuselage as required.

2aCABIN DOORS

1aCOCKPIT ENTRYDOOR ANDEMERGENCYENTRY WINDOW

2bEMERGENCYEXIT RELEASE

2bEMERGENCYWINDOWENTRY FORCABIN DOOR

LYNX MK-90BT.O

. 00-105E-9

LYN

X M

K-90B

. 4

AIRCRAFT DOORS AND WINDOWS

INTERNAL L/H DOOR EMERGENCY ENTRY L/H SIDE CABIN DOOR - INTERNAL VIEW

CABIN DOOR - EXTERNAL VIEW

REAR DOOR BETA LIGHT

BETA LIGHT ROTOR

LYNX MK-90BT.O

. 00-105E-9

LYN

X M

K-90B

.5

ENGINE FIRE ACCESS DOOR (LH VIEW)

BETA LIGHT HOIST DINGHY

HOIST

AIRCRAFT HOIST, FIRE ACCESS, AND DINGHY

LYNX MK-90BT.O

. 00-105E-9

LYN

X M

K-90B

. 6


a. Raise finger lift stop and move throttles, located on pilot’s overhead panel, down to the OFF position.

b. Lift fuel shutoff switches, located on pilot’s overhead console, and place to OFF position.

c. Place the battery switches, located on the overhead console, to the OFF position.

OVERHEAD PANEL

1aL/H THROTTLE

1aR/H THROTTLE

1cBATTERYSWITCHES

1bFUEL SHUTOFFSWITCHES

COCKPIT FACING FORWARD

OVERHEAD CONSOLE

LYNX MK-90BT.O

. 00-105E-9

LYN

X M

K-90B

.

AIRCREW EXTRACTION1. AIRCREW EXTRACTION

a. On the pilot and co-pilot seats, pull redrelease snap from harness quick releasebox until straps are released.

b. Passenger seats at mid cabin areequipped with lap belts and a singleshoulder harness and released by thesingle point release. The seat is either atwo or three person capacity.

1aQUICK RELEASE BOX

RESTRAINT STRAPS CONFIGURATION FOR PILOT AND CO-PILOT

7

1aFRONT SEATS AND RESTRAINTS

1bMID CABIN SEATS (RIGHT VIEW)

1bMID CABIN SEATS (LEFT VIEW)

LYNX MK-90BT.O

. 00-105E-9

LYN

X M

K-90B

.

AIRCREW EXTRACTION-Continued

8

1cREAR SEAT AND RESTRAINTS AND FIRST AID KIT LOCATION (KIT IS YELLOW BOX)

1. AIRCREW EXTRACTION-Continued

c. Passenger seats at the rear cabinare equipped with lap belts and asingle shoulder harness released bythe single point release. The seat iseither a two or three person capacityand is also the location for the firstaid kit (yellow box).

d. The mid cabin seats can be removedor installed in a one, two, or threeseat configuration. A mounting rackis displayed without the seats and aone seat configuration. This is theVIP(s) location.

CAUTION

This helicopter can be configured inall possible seat configurations.HOWEVER, in the VIP seat configu-ration, when the rear seat or seattank is installed, it CAN NOT beused for passenger purposes.Personnel will not be able to enter orexit the rear seat area.

1dMID CABIN SEAT MOUNTING RACK

1dMID CABIN MOUNTING RACKWITH ONE SEAT INSTALLED

LYNX MK-90BT.O

. 00-105E-9

LYN

X M

K-90B

. 9

AIRCREW EXTRACTION FOR SEAT TANKAND FIRE EXTINGUISHER LOCATION

1aSEAT TANK

2aFIRE EXTINGUISHER

1. SEAT TANK

a. A seat fuel tank can be locatedunder the rear cabin seat. Capacityis 620 lbs/92 gals (388.9L). Thispassenger seat at the rear cabin isequipped with lap belts and a singleshoulder harness released by thesingle point release. The seat has atwo person capacity and also thelocation for the first aid kit (yellowbox above the right seat).

2. FIRE EXTINGUISHER

a. The fire extinguisher is located onthe upper right side of the co-pilotseat.

LYNX MK95T.O

. 00-105E-9

LYN

X M

K95.1

MAIN ROTOR BLADESENGINEEXHAUST TAIL ROTOR

RADAR

AUXILLIARY FUEL TANKS

N2 MAIN FUEL TANK

BATTERY

N1 MAIN FUEL TANK

N1 COLLECTOR TANK

N2 COLLECTOR TANKFORWARD FUEL TANK

FIRING

HEAVY STORESELECTRICAL SKINBREAK

NOTE: Simple beam carriers, one on each side of the fuselage for the carriage of MK 44 or MK 46 torpedoes.

AIRCRAFT HAZARDSOTHER HAZARDS:Acids - BatteriesAsbestosBeryllium + Beryllium OxidesBromochlorodifluoromethane - Fire ExtinguishantDimethylformamide - Strobe Power PackFluorolastomers - Burnt SealsLithium - BatteriesSonar Locator Beacon(s) - Lithium Battery (Does not apply to PO Navy aircraft)Tritium Light Sources - Beta LightsWeapon LoadWindscreen Wash Fluid AL-36Zinc SelenideFuel: AVTURHydraulic Oil: OM-15HP Gases: NitrogenEngine Oil: OX-38/OEP-70/OEP-215Oxygen: NIL

LYNX MK95T.O

. 00-105E-9

LYN

X M

K95.2

NOTE: Beta lights are installed on the aircraft. Any broken light constitutes a radiation hazard. Persons in vicinity should evacuate upwind. In an enclosed space, persons should evacuate and then ventilate area for at least thirty minutes.

1. BETA LIGHT LOCATIONS

a. Battery master switch (green).b. Hoist column lock (2 green, 1 red).c. Cabin door emergency hatches (10 green).d. Blade fold position marker (1 green).e. Emergency services safety break.f. Master armament safety switch.

NOTE: More beta light information located on page Lynx MK95.5.

AIRCRAFT HAZARDS-Continued1aBETA LIGHT

OVERHEAD CONSOLE BATTERYMASTER SWITCH BETA LIGHT

RESCUE HOISTBETA LIGHTS

1bBETALIGHT

FORWARD

FORWARDFORWARD

FORWARD

1cBETALIGHT

WINDOW JETTISONLEVER BETA LIGHT

CABIN DOOREMERGENCYBETA LIGHT

1fMASTER ARMAMENTSAFETY SWITCHBETA LIGHT

1eREDBETALIGHT

GREENBETALIGHT

STRIKERPLATE

1dBETALIGHT

LYNX MK95T.O

. 00-105E-9

LYN

X M

K95.3

SPECIAL TOOLS/EQUIPMENTPower Rescue SawCrash AxAIRCRAFT ENTRY1. NORMAL ENTRY

NOTE: The cockpit and cabin doors are not droppable. They are located on both sides of the fuselage.

a. To open both cockpit doors: turn exterior handle of door, located bottom right or left (depending on which side of approach) UPWARDS.b. To open both cabin doors: turn the external door handle, located forward of window, backwards, pull door out and forwards and slide door aft.

2. EMERGENCY ENTRY

Both cockpit doors and cabin windows are jettisonable externally or internally.

NOTE: A blade may have to be inserted between frame and door to gain forced entrance.

a. To jettison external cockpit doors: slide sliding window aft, push the internal jettison lever, located forward of sliding window, forwards and down, then pull outwards.b. To jettison internal cockpit doors: push the internal jettison lever, located forward of sliding window, forwards and down, then pull outwards.c. To jettison both external single in each cabin door: (see rescue arrow) pull the emergency release pull down lever, located externally below window frame, down, then pull window outwards using handgrips at lower corners of window.d. To jettison both internal single cabin windows: pull the internal jettison handle below the window, down, then push window outwards.

3. CUT-INa. Cut-in fuselage or windows as required.

CAUTION

SLIDINGWINDOW

SLIDINGWINDOWRAIL/HINGES

FIXEDWINDOWS

INTERNALHANDLE

CATCH

INTERNALHANDLEWITH BETALIGHTS

HANDHOLD

EMERGENCYJETTISONLEVER

SLIDINGWINDOWLOCKINGLEVER

MANUAL INTERNAL HANDLE

INTERNAL JETTISONHANDLE

BETA LIGHTS

EXTERNAL VIEW OFLEFT HAND DOOR

INTERNAL VIEW OFLEFT HAND DOOR

HANDGRIPS

EXTERNAL VIEW OFLEFT CABIN DOOR


INTERNAL VIEWOF LEFT HANDCABIN DOOR

MANUAL EXTERNALHANDLE DETAIL

INDICATORWIRE DETAIL

EXTERNALCABIN DOORHANDLE

LYNX MK95T.O

. 00-105E-9

LYN

X M

K95.4


a. Move both throttle levers, located on the overhead console, up to HP cock OFF position, or fully backwards.

b. Place booster pump switches, located on fuel management section of the overhead console, to OFF position.

c. Place LP cocks, located on fuel management panel, to the SHUT position.

d. In case of engine fire, activate the engine fire extinguisher switches, located on the overhead console.

e. Move battery master switch, located on the overhead console, up to the OFF position.

1eBATTERY MASTER SWITCH

OVERHEAD CONSOLE

1dENGINE FIREEXTINGUISHERS

1cLP FUEL COCKS

1aTHROTTLE LEVERS

ROTORBRAKE

WARNING PANEL

CARGORELEASESWITCH

PILOTPOSITION

JETTISONBUTTON

HOIST

C0-PILOTPOSITION

WINDOWCATCH

DOORJETTISON

CABIN LIGHTS

EXTERNALLOADRELEASE

HAND FIREEXTINGUISHERNORMAL HANDLES

(BOTH SIDES)

MASS

LYNX MK95T.O

. 00-105E-9

LYN

X M

K95.5


1dTELEMIC

BARREL1dPSP

1a, 1b, 1cRESTRAINTDIAL


1aFRONT SEAT

1aMID CABIN SEAT

1eREARSEAT

EMERGENCY EXITS

WINDOW

SLIDING WINDOW

NORMAL EXITHANDLES



2bREARCABINDOORLEVER

2aJETTISON LEVER


a. To release personnel restraints: press center top of restraint dail and rotate dial 1/4 of a turn to either right or left. Front and mid cabin seats only.

b. Pull up on dial until the restraint straps are released.

c. Place all restraints out of the way to prevent entanglement during extraction.

d. Disconnect telmic and PSP, and any other disconnect(s), if applicable, that will prevent extraction.

e. Disconnect restraints from rear seats.


NOTE: Exit doors can be jettisoned to make extraction of crewmembers faster.

a. For front doors, push jettison lever forward and down, then push door out.


LYNX WG13T.O

. 00-105E-9

LYN

X W

G13. 1


AIRCRAFT ENTRY

1. NORMAL ENTRY

a. Pull door handle on passenger door, located on left side of fuselage, counter- clockwise to open door.

b. Rotate crew door handle, located on left side of fuselage, clockwise to open door.

2. EMERGENCY ENTRY

a. Rotate handle, located on left side of fuselage, to release window on passenger door.

3. CUT-IN

a. Cut-in windows or fuselage as required.

OTHER HAZARDSAcids - BatteriesAsbestosBeryllium + Beryllium OxidesBromochlorodifluoromethane - Fire ExtinguishantDimethylformamide - Strobe Power PackFluorolastomers - Burnt SealsLithium - BatteriesSonar Locator Beacon(s) - Lithium BatteryTritium Light Sources - Beta LightsWeapon LoadWindscreen Wash Fluid AL-36Zinc SelenideFuel: AVTURHydraulic Oil: OM-15HP Gases: NitrogenEngine Oil: OX-38/OEP-70/OEP-215Oxygen: NIL

MAIN ROTORS TAILROTORS

MAIN FUEL TANKS

BATTERY

FUEL FEEDERTANKS

1bCREWDOORHANDLE

1aPASSENGERDOOR HANDLE

2aWINDOWRELEASEHANDLE

TORPEDO INSTALLATION

CABLE EXTRACTORCONNECTOR

TORPEDO CABLEANCHORING TUBE

ACTUATORCONVENTIONALHEAVY WEAPONSHOLDER

MISSLE INSTALLATION

MISSLEHOLDER

MISSLELAUNCHER

FIXED BOXESCONTAININGEXPLOSIVESHAFTS

LYNX WG13T.O

. 00-105E-9

LYN

X W

G13.2

ENGINE SHUTDOWN ANDAIRCREW EXTRACTIONS1. ENGINE SHUTDOWN

NOTE: Engine shutdown procedures pending, however other Lynx models, in this manual may be applicable if cockpit layout is similar.

2. AIRCREW EXTRACTIONS

NOTE: Before extracting aircrew members, release the three point attachment of the dinghy package.

a. To release personnel restraints: press center top of restraint dail and rotate dial 1/4 of a turn to either right or left. Front and mid cabin seats only.

b. Pull up on dial until the restraint straps are released.

c. Place all restraints out of the way to prevent entanglement during extraction.

d. Disconnect telmic and PSP, and any other disconnect(s), if applicable, that will prevent extraction.

2dTELEMIC

BARREL

2dPSP

2a, 2b, 2cRESTRAINTDIAL

2aFRONT SEAT

2aMID CABIN SEAT

2eREARSEAT

2aFRONT SEAT (TYPICAL)

DINGHYTHREE POINTATTACHMENT

DINGHY

SEAT HEIGHTADJUSTINGLEVER

SHOULDER HARNESS REEL

SHOULDERHARNESSCONTROLAND LEVER

SEAT FASTATTACH PINS

MERLINT.O

. 00-105E-9

ME

RLIN

.1


MERLINT.O

. 00-105E-9

ME

RLIN

.

AIRCRAFT DIMENSIONS

2

BLADES SPREAD

NOTE: The Merlin has a normal crew of 5.

STATIC GROUND LINE

19950 MM

6620 MM

22500 MM

9300 MMRADIUS

2000 MMDIAMETER

MERLINT.O

. 00-105E-9

ME

RLIN

.3

AIRCRAFT DIMENSIONS-ContinuedBLADES FOLDED

15750 MM

5200 MM

5200 MM0.0

15750 MM

16806 MM

STATIC GROUND LINE

OLEO CENTER 1910

OLEO CENTER 1910

242285

3025

210

2046

2140

2435

DOOR FULLY OPEN

WHEEL C

MAIN DOOR SWING

210305 480

2140

L

NOTE:Double main wheel configurationdoes not affect wheel base, butnote change of nose wheel width.

MERLINT.O

. 00-105E-9

ME

RLIN

.4

AIR INTAKES

2M4.4M

7.5M RADIUS FROM ENGINE CENTER

5M

3M

50 0

BDA

E C EF

AIRCRAFT HAZARDS1. HAZARDS

Normal weapon carried is the Stingray Torpedo.

Personnel are to exercise extreme care when movingthe Merlin MK1 using a mechanical handler, due to itsprofile both with and without ballast weights.

Aircrew situational awareness on deck. Deck crewsshould be made aware that due to poor rearwards fieldof view, the pilot may not be fully aware of activity inthe vicinity of the aircraft and therefore rigorous andclear communication procedures between aircrew andthe FDO are required. This is particularly importantduring the operation of PRISM. Consideration shouldbe given to using an extra communications number ona long lead connected to the aircraft intercom.

Rotor downwash is produced by the Merlin which willgenerate large clouds of salt spray which can coverthe whole ship and soak the flight deck, especially inbeam or astern relative winds. The downwash alsohas the potential to blow over flight deck personnel. Itis recommended that the FDO be provided with asafety harness attached to a strong point.

A Rotor disk: Beware of blade swoop.

B Tail Rotor.

C Radar on Dome.

D Main engine exhausts X3 and APU exhaust.

E Beware of Flotation Bags.

F Tail Pylon Fold/Hinge Point.

WARNING

MERLINT.O

. 00-105E-9

ME

RLIN

.5

AIRFRAME MATERIALS

CARBONKEVLARNOMEX

CARBONKEVLARNOMEX

KEVLARNOMEX

KEVLARNOMEX

KEVLARNOMEX

KEVLARNOMEX

CARBONKEVLAR

LA SKINSTRINGER

LAHONEYCOMBSKINSLA FRAMES

CARBONNOMEX

LA SKINSTRINGER

NOTE: Main and tail rotor blades are made out of composite materials.

MERLINT.O

. 00-105E-9

ME

RLIN

.

EXTERNAL VIEWS AND FIRE ACCESS POINTSRT SIDE

APU FIRE ACCESS

3 ENGINE FIRE ACCESS

6

LT SIDE

2 ENGINE FIRE ACCESS1 ENGINE FIRE ACCESS

MERLINT.O

. 00-105E-9

ME

RLIN

.

SPECIAL TOOLS/EQUIPMENTPower Rescue Saw

AIRCRAFT ENTRY

1. NORMAL ENTRY



2. EMERGENCY ENTRY


3. CUT-IN



7 RIGHT OR STARBOARD SIDE

LEFT OR PORT SIDE

MERLINT.O

. 00-105E-9

ME

RLIN

.8

LT SIDE REAR WINDOW

EXTERNAL WINDOWS AND DOORS

LT SIDE PILOT WINDOW

RT SIDE OBSERVER’S WINDOW

ON MAIN CARGO DOOR

RT SIDE EMERGENCY ACCESS

MERLINT.O

. 00-105E-9

ME

RLIN

.9


NOTE: All components are located on the overhead control panel and when activated the cockpit is considered safe.

a. Turn all three engine shutdown switches to the OFF position.

b. Place all three engine fuel shutoff switches to the OFF position.

c. If APU is on, press start/stop button to the SHUTOFF position.

d. Turn master armament switch counter clockwise to the SAFE position.

e. Place the battery master switch to the OFF position.

OVERHEAD CONTROL PANEL

MASTER ARMAMENT SWITCH

ENGINE FUEL SHUTOFF

SWITCHES

APU SHUTOFF

BATTERY MASTE

R

ENGINE SHUTDOWN SWITCHES

1 2 3

MERLINT.O

. 00-105E-9

ME

RLIN

.10

ENGINE SHUTDOWN-Continued1. ENGINE SHUTDOWN-TRAINER PANELS

NOTE: The illustrated panels are taken from a trainer used for engine shutdown.

MERLINT.O

. 00-105E-9

ME

RLIN

.11

AIRCREW EXTRACTION

LT SIDE CO-PILOT WINDOW OBSERVER’S WINDOW

CABIN DOOR

CABIN ARRANGEMENT-UNOCCUPIED


NOTE:There are no ejections seats to safe.There are 2 crew in the cockpit, 2crew at the cabin console and 1observer at the right cabin door.

a. Disconnect lap belts and shoulder harnesses at the central harness release buckle.

MERLINT.O

. 00-105E-9

ME

RLIN

.12

AIRCREW EXTRACTION-Continued

CABIN ARRANGEMENT-OCCUPIED

CABIN ARRANGEMENT WITH OBSERVER-OCCUPIED

CABIN ARRANGEMENT-OCCUPIED

OH-13ST.O

. 00-105E-9

OH

-13S.1

MAIN ROTORTAIL ROTOR

FUEL TANKS

CREW DOOR(BOTH SIDES)

JETTISONABLEDOOR RELEASE


AIRCRAFT ENTRY

1. NORMAL ENTRY

a. Open crew doors located on both sides of aircraft.

2. EMERGENCY ENTRY

a. Use the jettison door release handles located on each crew door.

3. CUT-IN

a. Cut-in to cockpit windows as required.

ARMAMENT

OH-13ST.O

. 00-105E-9

OH

-13S.2

ENGINE SHUTDOWN ANDAIRCREW EXTRACTION1. ENGINE SHUTDOWN

a. Place the mixture control, located on the forward control panel, to IDLE CUT OFF position.

b. Place the battery switch, located on the forward control panel, to the OFF position.

c. Place the magnetos switch, located on the forward control panel, to the OFF position.

d. Place the throttle, located to the left of the forward control panel, to the OFF position.

e. Place all remaining switches to OFF.


a. Release crew from all restraint straps.

b. Place restraints to the side to avoid entanglement.

1aMIXTURE CONTROL1bBATTERY SWITCH

1cMAGNETOS SWITCH

1eMISCELLANEOUSSWITCHES

1dTHROTTLE

FORWARD CONTROL PANEL

OH-58A/C/DT.O

. 00-105E-9

OH

-58A/C

/D. 1

The aircraft information is located in Chapter 13 containing US Army aircraft.

PUMA HC1/SA 330T.O

. 00-105E-9

PU

MA

HC

1/SA

330. 1

TAIL ROTORDANGER AREA

JET EFFLUXDANGER AREA

FREON ENGINE FIREEXTINGUISHER (ONESHOT ONLY)

ENGINE OILTANKS (BUILTINTO ENGINE)

JETEFFLUXDANGERAREA

ENGINEINTAKEDANGERAREA

MAIN ROTORDANGER AREADO NOT ENTERWHILE BLADESARE WINDING UPOR SLOWING DOWN

NOTE:Cabin may contain hazardousstores or “Ferry-Flight” fuel(Each large tank can contain370 kg fuel)

AVIATION FUELIN CRASH-PROOFBAGS UNDERCABIN FLOOR1000 KG MAX

JETEFFLUXDANGERAREA

I.R. TORCHNIGHTSUN SX-16DANGER INTENSE INFRA-RED RADIATION(May not be visible.) (Mounted on frame righthand side of fuselage.)

BATTERY INSTOWAGEFORWARDBOTTOM LEFT WALL OF CABIN

APPROACH INTHIS AREAWHEN ENGINESARE RUNNING

AIRCRAFT HAZARDSOTHER HAZARDS:Acids - BatteriesBeryllium + Beryllium OxidesBromochlorodifluoromethane - Fire ExtinguishantBromotrifluoromethane - Fire ExtinguishantCadium - BatteriesChlorobromoethane - Fire ExtinguishantComposite Materials - Man made mineral fibresDimethylformamide - Strobe Power PackNightsun Light SystemPolytetrafluoroethylene - PTFESonar Locator Beacon(s) - Lithium BatteryTritium Light Sources - Beta LightVery Flare

Fuel: AVTURHydraulic Oil: OM-15HP Gases: Nitrogen/Air/EntinoxEngine Oil: OX-36Oxygen: Gaseous

AIRCRAFT ARMAMENT

NOTE: Machine guns may be fitted in cabin doorways. Light weapons and explosives may be carried internally.

PUMA HC1/SA 330T.O

. 00-105E-9

PU

MA

HC

1/SA

330.2


AIRCRAFT ENTRY

1. NORMAL AND EMERGENCY ENTRY

a. Open main cabin doors, located both sides of fuselage for normal entry.

b. Emergency entry for main cabin doors can be jettisoned externally by removing break- able plastic cover, lifting handle, and pulling down on red or yellow/black striped triangu- lar handles in center of door. Pull down and push out. Door window panel can be broken.

c. Emergency entry for cockpit access, use the external pilot’s or co-pilot’s jettisonable panel, by operating the red or yellow/black striped handles, on each lower door frame, by turning the handle and pushing upwards.

d. Emergency entry through cargo ramp, the center of a fixed panel may be broken in.

2. CUT-IN

a. Cut-in area is on the overhead panel above the cockpit area.

2aOVERHEADPANELCUT-INAREA

1a, 1bMAIN CABIN DOOR (BOTH SIDES) DAILY USE FIRST AID

KIT ON RIGHT SIDE OFREAR WALL

1dFIXED PANEL-CENTER MAYBE BROKEN IN

CABIN AREA16 TROOPS6 STRETCHERSAND 4 SEATS(OBSTRUCTINGPORT DOOR)- STORES MAY BECARRIED INCLUDINGEXPLOSVIES OR FUEL-FERRY TANKS- CABIN SIDE WINDOWSMAY BE BROKEN INTO

INTERCONNECTINGPASSAGEWAY FORCOCKPIT AND CABIN

1cEXTERNAL JETTISON

PILOT’S COCKPITACCESS DOOR

CO-PILOT’SJETTISONABLEPANEL

PORTABLE FIRE EXTINGUISHERAND FIRE AX IN CABIN FORWARDRIGHT BULKHEAD

PUMA HC1/SA 330T.O

. 00-105E-9

PU

MA

HC

1/SA

330.3


a. Pull aft on battery switch, located on the overhead control console, to OFF position.

b. Pull aft on alternator switches, located on the overhead control console, to OFF position.

c. Pull aft on the fuel shut-off levers, (marked red) located on the overhead control console, to OFF position.

d. In case of engine fire, on the fire control warning panel, push buttons for 1 or 2 engines extinguishers. Extinguishers are single shot type.

CENTRALIZEDWARNINGLIGHTS PANEL

1cLP FUEL SHUT-OFFCONTROL LEVERS(MARKED RED)

ENGINE THROTTLECONTROL LEVERS(MARKED YELLOW)

1aBATTERY SWITCH 1b

ALTERNATOR SWITCH

EMERGENCY CUT-OFF SWITCHES WITH“ALL-OFF” BAR YELLOW/BLACK

ROTOR BRAKECOCKPIT LIGHT

ROLA SELECTOR

PILOT’SDOORJETTISONLEVERSTRIPEDYELLOW/BLACK

PILOT’SRELEASEBUTTONSON CYCLICCOLUMN

EMERGENCY JETTISONCONTROL ON COLLECTIVEPITCH CONTROL LEVER(CABLE CUTTER)

MAINWHEELSBRAKE(RED)

1d FIREWARNINGPANEL

CO-PILOTRELEASEBUTTONSON CYCLICCOLUMNPANEL JETTISON LEVER

STRIPED RED/BLACK

HYDRAULICHANDPUMPANDSELECTOR

PUMA HC1/SA 330T.O

. 00-105E-9

PU

MA

HC

1/SA

330.4

AIRCREW EXTRACTION

COCKPITACCESSDOOR

CO-PILOT’SJETTISONDOOR

FIXED PANEL WITHCENTER KICKOUT PANEL

CABINACCESSDOORS

INTERNALJETTISONHANDLES(RED/BLACK)

EMERGENCY USE FIRST AID KIT(CONTROLLED DRUGS, ETC.)PORTABLE FIRE EXTINGUISHERAND FIRE AX IN CABIN FORWARDRIGHT BULKHEAD

ACCESSLADDERSTOWAGE

FIRST AID KITON SIDE WALLRIGHT HAND SIDE(DAILY USE)FIRE AX

HAND FIREEXTINGUISHER SIGNAL PISTOLAND CARTRIDGES ON FORWARDRIGHT BULKHEAD IN CABIN

HAND FIREEXTINGUISHERIN COCKPIT


NOTE: Jettison doors, if necessary, and use all doors and entry ways including ramp kickout panel for extraction process. An access ladder may be mounted over fixed panel. Window panel can be broken.

a. Release restraint straps from crew.

b. Release lap belts from 16 troops or 6 stretchers and 4 seats. Medivac configuration will obstruct port door.

CABIN AREA

SA 313/318T.O

. 00-105E-9

SA

313/318. 1


AIRCRAFT ENTRY

1. NORMAL ENTRY

a. Main entry doors are located on the right and left sides of the airframe. Open doors for entry or exit.

2. EMERGENCY ENTRY

a. Use main entry doors for emergency entry.

3. CUT-IN

a. Cut-in windows or doors as required.

4. ENGINE SHUTDOWN

a. Place three switches, located on the center control console, to the DOWN position.

b. Pull two fuel levers, located on the forward portion of the center control console, to the AFT position.

1a, 2aMAIN ENTRY DOOR(BOTH SIDES)

FUELTANKS

MAIN ROTORENGINEEXHAUST TAIL ROTOR

4aTHREE SWITCHES

4bFUEL LEVERS

SA 316B/SA 319B/ SE 3160

T.O. 00-105E

-9

SA

316B/S

A 319B

/SE

3160.

AIRCRAFT DIMENSIONS

1

HEIGHT2.6 METERS

1.5 METERS

MAIN ROTORDIPPED MAIN ROTOR

LENGTH12.32 METERS

DIAMETER1.97 METERS

TAIL ROTOR

SA 316B/SA 319B/ SE 3160

T.O. 00-105E

-9

SA

316B/S

A 319B

/SE

3160.2

MAIN ROTOR

ENGINE EXHAUST TAIL ROTOR

BATTERY(ON RIGHT SIDE)FUEL TANK1b, 2a

SLIDINGCARGO DOOR(BOTH SIDES)

1a, 2aCABIN DOOR(BOTH SIDES)


AIRCRAFT ENTRY

1. NORMAL ENTRY

a. Enter through cabin doors by turning door handle downwards. Door opens forward.

b. Enter through sliding cargo doors by turning door handle to rear. Slide door aft to open.

2. EMERGENCY ENTRY

a. To remove cargo doors, turn two keys to inside. Push two push buttons in, then turn them to inside.

b. For emergency release, break plexiglass at lever (located internally) and move this lever to bottom to unlock release lug, then pull door toward you.

3. CUT-IN

a. Cut-in to doors or windows as required.

1aCABIN DOOR HANDLE

1bCARGO DOOR HANDLE

2bINTERNAL EMERGENCY RELEASE LEVER

2aKEYS

2aPUSHBUTTON

SA 316B/SA 319B/ SE 3160

T.O. 00-105E

-9

SA

316B/S

A 319B

/SE

3160.

1aFUEL LEVERS

1. ENGINE SHUTDOWN - SA 316B

a. Pull both fuel levers, located on forward portion of center control console, to the AFT position.b. Place the battery switch, located on the overhead panel, to the AFT position.

2. ENGINE SHUTDOWN - SA 319B

a. Move flow lever, located on forward portion of center console right side, to the AFT position.b. Move the fuel cutoff (flame arrester), located on the forward portion of the center console left side, to the AFT position.c. Place the power switch, located on the upper portion of the center console, to STOP position.d. Place the battery switch, located on the overhead control panel, to the STOP position.

3. ENGINE SHUTDOWN - SE 3160

a. Place fuel cutoff and fuel flow control levers, located on the center control console, to AFT position.b. Place generator and battery switches, located on the upper center control console, to the OFF position.c. Pull out main rotor brake control handle at 175 rpm (inner ring of duel tachometer).

4. EMERGENCY ENGINE SHUTDOWN

a. Follow steps 3a thru 3c.b. Disconnect battery by pulling out the hearpin turn round nut to the left and pull the battery out of the aircraft.

ENGINE SHUTDOWN

3

1bBATTERYSWITCH

SA 316B

SE 3160

3bBATTERYSWITCH

3bGENERATORSWITCH

3aFUEL FLOWCONTROLLEVER

3cDUALTACHOMETER

3cMAINROTORBRAKECONTROLHANDLE

3aFUELSHUT-OFFLEVER

2cPOWERSWITCH

2 aFLOWLEVER

2bFUELCUT-OFF

SA 319B 2dBATTERYSWITCH

SA 341/342T.O

. 00-105E-9

SA

341/342.1

MAIN ROTOR

TAIL ROTOR

FUEL TANK

MISSLES(BOTH SIDES)

BATTERY

1bPASSENGER DOOR HANDLE1a

FORWARD DOOR HANDLE

NOTE: Main rotor blades have carbon fibre along the length.


AIRCRAFT ENTRY

1. NORMAL AND EMERGENCY ENTRY

a. Pilot and copilot doors are opened by pressing button on door handle and turning handle.

b. To open passenger door, pilot or copilot doors must be opened first, then lower handle on passenger door and pull out.

2. CUT-IN

a. Cut-in windows and doors as required.

3. ENGINE SHUTDOWN

a. Pull aft on fuel cut-off handle, marked yellow and black striped secured by safety wire, located on overhead panel.


a. Aircrew seats are equipped with shoulder harness and lap belts. Disconnect aircrew restraints and remove.

3aFUEL CUT-OFFHANDLE

SEA KING AEW 2T.O

. 00-105E-9

SE

A K

ING

AE

W 2. 1

AIRCRAFT HAZARDS

TAILROTORDANGERAREA

AIRCRAFT ARMAMENT - None is normally carried.

OTHER HAZARDS:Pyrotechnics: Signal pistol and cartridges,marine markers, smoke/flame floats,and underwater sound signals.

* Beryllium: Hazardous material in Beta lights around exits.

- Lethal if fumes or dust absorbed by the body.

Acids - BatteriesBromochlorodifluoromethane - Fire ExtinguishantBromotrifluoromethane - Fire ExtinguishantCartridge Operated EquipmentChlorobromoethane - Fire ExtinguishantComposite Materials - Man Made Mineral FibresDimethylformamide - Strobe Power PackLithium - BatteriesMethyl Bromide - Fire ExtinguishantPolytetrafluoroethylene - PTFESonar Locator Beacon(s) - Lithium BatteryTritium Light Sources - Beta LightsVery FlareFuel: AVTURHydraulic Oil: OM-15HP Gases: Nitrogen/AirEngine Oil: OX-38Oxygen: NIL

MAINROTORDANGERAREA

CABLECUTTER INWINCHHOUSING

HYDRAULIC OILRESERVOIRS ANDMAIN GEARBOX

ENGINE FIREEXTINGUISHERBOTTLES

ENGINEEXHAUSTEFFLUX

ENGINE OILTANKS

ENGINE AIRINTAKE

BATTERYFUEL TANK(FLEXIBLE CELLS)5,500 LBS.806.45 GALS(3410 LITRES)

FLOTATIONEQUIPMENT

RADHAZ10METERRADIUS

GEARBOX OIL

SEA KING AEW 2T.O

. 00-105E-9

SE

A K

ING

AE

W 2.

2

2aCOCKPIT WINDOW(BOTH SIDES)

2bCABIN ESCAPEHATCH

2b HANDLE

TO OPEN: PRESS AND TURN

EXIT RELEASE TURN

HF AERIAL

2cESCAPEHATCHES

3bENGINE FIREACCESS DOOR

FIRST AID KIT

PULL TABEXIT RELEASE

FIREEXTINGUISHERS

2aCOCKPIT WINDOW(SIMILAR TOOPPOSITE SIDE)

1dSLIDINGENTRY DOOR

REDHANDLE

1aNORMALENTRY DOORLOWER SECTION


AIRCRAFT ENTRY

1. NORMAL ENTRY

NOTE: Self-illuminated Beta lights mark location of doors, hatches and window.

a. On entry door, located on forward left side of fuselage, press button, rotate handle clockwise to DOWN position.

b. Pull lower entry door section outwards and expose boarding steps.

c. Lift upper door section to snap position allowing upper door to stay open.

d. On sliding entry door, located on aft right side of fuselage, slide handle to right and push sliding door to the right.

2. EMERGENCY ENTRY

a. Cockpit windows can be externally removed by turning door handle clockwise and pulling window out by handle grip on window.

b. Cabin escape hatch can be externally removed by pressing button on handle, turning handle and pulling window outwards.

c. Escape hatches can be externally removed by pulling tab for exit release and then pulling hatch outward.

3. CUT-IN

a. Cut-in around windows and doors as required. Designated windows are marked for cut-in.

b. Use the engine fire access door for fire access.

2aHANDLEGRIP 2a

HANDLE

3aCUT-IN WINDOW

1cUPPERDOORSECTIONIN SNAPPOSITION

EXIT RELEASEPULL DOWN

PULL HANDLE FOREMERGENCY RELEASE

CUT FOR EMERGENCY RESCUE

SEA KING AEW 2T.O

. 00-105E-9

SE

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AE

W 2.3


a. Pull and lift speed select levers, located on overhead panel, to SHUT-OFF position.

b. Switch firewall valves, located on forward instrument panel, down to CLOSE position.

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

2. ENGINE FIRE SHUTDOWN

a. Pull engine fire handles, located on overhead panel.

b. Set fire switch, located on overhead panel, to MAIN.

c. Pull and lift speed select levers to SHUT-OFF position.

d. Switch down firewall valves to CLOSE position.

e. Turn battery master switch to OFF position.

1c, 2eBATTERY MASTER SWITCH

2aENGINE FIRE EXTINGUISHER& EMERGENCY PULL HANDLES

THROTTLES

ROTOR BRAKE

2bFIRE SWITCH

1a, 2cSPEED SELECT LEVERS

LANDINGGEARCONTROL

1b, 2dFIREWALL VALVES

PARKING BRAKE

SHOULDER HARNESS RELEASE

CARGORELEASE

SLIDING WINDOW RELEASE

JETTISON HANDLE

SEA KING AEW 2T.O

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4


a. For upper personnel door, emergency release at aft end, and push upper door out.

b. For cabin window escape hatches, pull tag, remove seal, and push out.

c. For cargo door escape hatch, pull handle aft, and push out.

d. For cockpit windows, jettison can be actuated from internally.

e. All crew seats are fitted with a quick-release harness. Push center and turn.

BETA LIGHTS ARE FIXED AROUND ESCAPE HATCHES AND DOORS

1aUPPERPERSONNELDOOR

1bCABINWINDOWESCAPEHATCH

1cCARGODOORESCAPEHATCH

1dCOCKPIT WINDOWS

LOCATION OFBETA LIGHTS

1eQUICK-RELEASEHARNESS

SEA KING ASW 5T.O

. 00-105E-9

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AS

W 5.

AIRCRAFT HAZARDSAIRCRAFT ARMAMENT - None is normally carried.

OTHER HAZARDS:Pyrotechnics: Signal pistol and cartridges,marine markers, smoke/flame floats, practice depthcharges, and underwater sound signals.




TAIL ROTORDANGERAREA

MAIN ROTORDANGER AREA

CARTRIDGEINITIATEDRESCUEHOISTCABLESHEAR


CARTRIDGE INITIATEDENGINE FIRE EXTINGUISHERBOTTLES

ENGINE EXHAUST EFFLUX

ENGINE OIL TANKS

ENGINE AIR INTAKE

BATTERYFUEL TANK(FLEXIBLE CELLS)6,500 LBS.953 GALS(4030 LITRES)(AVCAT/AVTUR)

FLOTATIONEQUIPMENT

RADHAZ

GEARBOX OIL

AL5RESERVOIR

BATTERY

SIGNALPISTOL &CARTRIDGES-ONLY SAR ACFT

BERYLLIUM(3 PLACES)

CARTRIDGE INITIATEDSONOR SU CABLE SHEAR

1

SEA KING ASW 5T.O

. 00-105E-9

SE

A K

ING

AS

W 5.

AIRCRAFT HAZARDS-Continued

2

AIRCRAFT ARMAMENT

Weapon load may include:TorpedosDepth ChargesSpecial Weapon600 lb MC BombAlso:SonobuoysBathythermal BuoysMarine Sound SignalsMarine MarkersSmoke and Flame Floats

SPECIAL WEAPON(HEMC)PORT FORWARDPOSITION ONLY

Selection of Master Armament SafetySwitch to SAFE isolates all weapon circuits

SAFETY PIN WITHSTREAMER

MASTER ARMAMENTSAFETY SWITCH

FIRE/SAFEINDICATOR

STORES JETTISON

(PRE-MOD)

(POST MOD)

BRSL-SPECIALWEAPONCONTROLBOX

ARMAMENT CONTROL PANEL

CUTTERWEAPONLANYARD

SPECIAL WEAPONCIRCUIT BREAKER ANDSELECTION SWITCHES

SEA KING ASW 5T.O

. 00-105E-9

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AS

W 5.

3


2bCABIN ESCAPEHATCH

2b HANDLE


EXIT RELEASE TURN

HF AERIAL

2cESCAPEHATCHES


FIRST AID KIT


FIREEXTINGUISHERS


1dSLIDINGENTRY DOOR

REDHANDLE



AIRCRAFT ENTRY1. NORMAL ENTRY






2. EMERGENCY ENTRY




3. CUT-IN



2aHANDLEGRIP 2a

HANDLE

3aCUT-IN WINDOW





SEA KING ASW 5T.O

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4




c. Turn master armament safety switch, located on the overhead panel, to SAFE position.

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



b. Set fire extinguisher operating switch, located on overhead panel, to MAIN.



e. Turn master armament safety switch to SAFE position.

f. Turn battery master switch to OFF position.

1d, 2fBATTERY MASTER SWITCH


THROTTLES

ROTOR BRAKE

2bFIREEXTINGUISHEROPERATINGSWITCH

1a, 2cSPEED SELECTLEVERS

LANDINGGEARCONTROL


PARKING BRAKE


CARGORELEASE


JETTISON HANDLE

1c, 2eMASTER ARMAMENTSAFETY SWITCHWITH SAFETY PINAND STREAMER

SPECIAL WEAPONCONTROL BOX BRSL

SEA KING ASW 5T.O

. 00-105E-9

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AS

W 5.

5






e. Crew seats are fitted with a 5 point quick- release harness. Push center and turn.

f. Troop seats, (roles dictate configuration) may be 8, 4, or 2 seats and a desk, are fitted with a 2 point lap straps. Turn knob to release.

BETA LIGHTS ARE FIXED AROUND ESCAPE EXITS




JUMPSEAT

AS ROLE:8 TROOP SEATS

1dCOCKPIT SIDEWINDOWS

AR &TROOPROLE:

1eCREW SEATS

1fTROOPSEATS

SEA KING HAR 3/SH 3DT.O

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R 3/S

H 3D

.1

AIRCRAFT HAZARDS


AIRCRAFT ARMAMENT - None is normally carried.

OTHER HAZARDS:Pyrotechnics: Signal pistol and cartridges





HOIST CABLECUTTER(CARTRIDGE)


ENGINE FIREEXTINGUISHERBOTTLES

ENGINEEXHAUSTEFFLUX ENGINE OIL TANKS

ENGINE AIR INTAKE

BATTERYFUEL TANK(FLEXIBLE CELLS)6,300 LBS.923.75GALS(3906LITRES)

FLOTATIONEQUIPMENT

RADHAZ

GEARBOX OIL

SIGNAL PISTOLAND CARTRIDGES


. 00-105E-9

SE

A K

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HA

R 3/S

H 3D

.2


2bCABIN ESCAPEHATCH

2b HANDLE


EXIT RELEASE TURN

HF AERIAL

2cESCAPEHATCHES

3bENGINE FIREACCESSDOOR

FIRST AID KIT


FIREEXTINGUISHER


1dSLIDINGENTRY DOOR

REDHANDLE



AIRCRAFT ENTRY

1. NORMAL ENTRY






2. EMERGENCY ENTRY




3. CUT-IN



2aHANDLEGRIP 2a

HANDLE

3aCUT-IN WINDOW





FIRST AID KIT

FIREEXT.


. 00-105E-9

SE

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HA

R 3/S

H 3D

. 3




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



b. Set fire switch, located on overhead panel, to MAIN.



e. Turn battery master switch to OFF position.

1c, 2eBATTERY MASTER SWITCH


THROTTLES

ROTOR BRAKE

2bFIRE SWITCH

1a, 2cSPEED SELECT LEVERS

LANDINGGEARCONTROL


PARKING BRAKE


CARGORELEASE


JETTISON HANDLE


. 00-105E-9

SE

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HA

R 3/S

H 3D

.





WINDOWS (5)

CREW DOOR

CARGO DOORWINDOW

EMERGENCY EXITS

1gRELEASE KNOB

1ePILOTS AND RADAROPERATOR SEATS

1dCOCKPITWINDOWS

1fAFT CABIN SEATS

1gTROOP/PASSENGERSEATS

4






e. Pilot and radar operator seats are fitted with a 5 point quick-release harness. Push center and turn.

f. Aft cabin seats are fitted with a 4 point quick- release harness. Push center and turn.

g. Troop/passenger seats are fitted a 2 point lap straps. Turn knob to release.

AIRCREW EXTRACTION

SEA KING HAS/ASW 6T.O

. 00-105E-9

SE

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HA

S/A

SW

6.

AIRCRAFT HAZARDSAIRCRAFT ARMAMENT - None is normally carried.

OTHER HAZARDS:Pyrotechnics: Signal pistol and cartridges,marine markers, smoke/flame floats, practice depthcharges, and underwater sound signals.






CARTRIDGEINITIATEDRESCUEHOISTCABLESHEAR


CARTRIDGE INITIATEDENGINE FIRE EXTINGUISHERBOTTLES

ENGINE EXHAUST EFFLUX

ENGINE OIL TANKS

ENGINE AIR INTAKE

BATTERYFUEL TANK(FLEXIBLE CELLS)6,500 LBS.953 GALS(4030 LITRES)(AVCAT/AVTUR)

FLOTATIONEQUIPMENT

RADHAZ

GEARBOX OIL

AL5RESERVOIR

BATTERY

SIGNALPISTOL &CARTRIDGES-ONLY SAR ACFT

BERYLLIUM(3 PLACES)

CARTRIDGE INITIATEDSONOR SU CABLE SHEAR

1


. 00-105E-9

SE

A K

ING

HA

S/A

SW

6.

AIRCRAFT HAZARDS-Continued

2

AIRCRAFT ARMAMENT

Weapon load may include:TorpedosDepth ChargesSpecial Weapon600 lb MC BombAlso:SonobuoysBathythermal BuoysMarine Sound SignalsMarine MarkersSmoke and Flame Floats

SPECIAL WEAPON(HEMC)PORT FORWARDPOSITION ONLY

Selection of Master Armament SafetySwitch to SAFE isolates all weapon circuits

SAFETY PIN WITHSTREAMER

MASTER ARMAMENTSAFETY SWITCH

FIRE/SAFEINDICATOR

STORES JETTISON

(PRE-MOD)

(POST MOD)

BRSL-SPECIALWEAPONCONTROLBOX

ARMAMENT CONTROL PANEL

CUTTERWEAPONLANYARD

SPECIAL WEAPONCIRCUIT BREAKER ANDSELECTION SWITCHES


. 00-105E-9

SE

A K

ING

HA

S/A

SW

6.3


2bCABIN ESCAPEHATCH

2b HANDLE


EXIT RELEASE TURN

HF AERIAL

2cESCAPEHATCHES


FIRST AID KIT


FIREEXTINGUISHERS


1dSLIDINGENTRY DOOR

REDHANDLE



AIRCRAFT ENTRY1. NORMAL ENTRY






2. EMERGENCY ENTRY




3. CUT-IN



2aHANDLEGRIP 2a

HANDLE

3aCUT-IN WINDOW






. 00-105E-9

SE

A K

ING

HA

S/A

SW

6.4




c. Turn master armament safety switch, located on the overhead panel, to SAFE position.

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



b. Set fire extinguisher operating switch, located on overhead panel, to MAIN.



e. Turn master armament safety switch to SAFE position.

f. Turn battery master switch to OFF position.

1d, 2fBATTERY MASTER SWITCH


THROTTLES

ROTOR BRAKE

2bFIREEXTINGUISHEROPERATINGSWITCH

1a, 2cSPEED SELECTLEVERS

LANDINGGEARCONTROL


PARKING BRAKE


CARGORELEASE


JETTISON HANDLE

1c, 2eMASTER ARMAMENTSAFETY SWITCHWITH SAFETY PINAND STREAMER

SPECIAL WEAPONCONTROL BOX BRSL


. 00-105E-9

SE

A K

ING

HA

S/A

SW

6.5






e. Crew seats are fitted with a 5 point quick- release harness. Push center and turn.

f. Troop/passenger seats are fitted a 2 point lap straps. Turn knob to release.

1eCREW SEATS

1dCOCKPIT SIDEWINDOWS

SONOBUOYS MAY BE REPLACED BY UP TO 8 TROOP SEATS

1fTROOP SEATS

1f2 POINTRELEASEKNOB

1e5 POINT QUICK-RELEASE KNOB





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WELCOME TO TECHNICAL ORDER 00-105E-9, 1 FEBRUARY 2006, … Segment 30.pdf · 2007. 12. 18. · to go directly to the technical order, click on the continue button. welcome to technical