WELCOME TO TECHNICAL ORDER 00-105E-9, 1 FEBRUARY 2006, … Segment 30.pdf · 2007. 12. 18. · to...
Transcript of WELCOME TO TECHNICAL ORDER 00-105E-9, 1 FEBRUARY 2006, … Segment 30.pdf · 2007. 12. 18. · to...
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WELCOME TO TECHNICAL ORDER 00-105E-9, 1 FEBRUARY 2006, REVISION 11.
TO SEE THE SEGMENT INFORMATION CHANGE NOTICE, CLICK ON THE NOTICE BUTTON.
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IN THIS SEGMENT.
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 Retaining out of date rescue information can negatively affect the user’s operability and outcome of emergencies.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
OEP-70 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 over- head 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)
1aENGINECONDITIONLEVERS
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
1aENGINECONDITIONLEVERS
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)
BETA LIGHTS(RADIO ACTIVE)
2aREARCABINDOORLEVER
2aJETTISON LEVER
1. AIRCREW EXTRACTION
a. Release crew in forward seats by releasing the QRF harness connection and other associ- ated 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
AIRCRAFT PAINT SCHEME
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
OEP-215 Engine Oil 6.8 L Engine
OEP-70 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
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
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 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 over- head 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
AIRCREW EXTRACTION ANDEMERGENCY EXIT DOORS
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)
BETA LIGHTS(RADIO ACTIVE)
2aREARCABINDOORLEVER
2aJETTISON LEVER
1. AIRCREW EXTRACTION
a. Release crew in forward seats by releasing the QRF harness connection and other associ- ated 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.
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-90BT.O
. 00-105E-9
LYN
X M
K-90B
.
AIRCRAFT PAINT SCHEME
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
SPECIAL TOOLS/EQUIPMENTPower Rescue SawCrash Ax
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 clock- wise 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
ENGINE SHUTDOWN1. ENGINE SHUTDOWN
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
EMERGENCYRELEASEPULL DOWN
INTERNAL VIEWOF LEFT HANDCABIN DOOR
MANUAL EXTERNALHANDLE DETAIL
INDICATORWIRE DETAIL
EXTERNALCABIN DOORHANDLE
LYNX MK95T.O
. 00-105E-9
LYN
X M
K95.4
ENGINE SHUTDOWN1. ENGINE SHUTDOWN
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 man- agement 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
AIRCREW EXTRACTION ANDEMERGENCY EXIT DOORS
1dTELEMIC
BARREL1dPSP
1a, 1b, 1cRESTRAINTDIAL
-2 CREW, FRONT-9 CREW, AFT: TROOPS OR STRETCHERS IN REAR CABIN
1aFRONT SEAT
1aMID CABIN SEAT
1eREARSEAT
EMERGENCY EXITS
WINDOW
SLIDING WINDOW
NORMAL EXITHANDLES
BETA LIGHTS(RADIO ACTIVE)
BETA LIGHTS(RADIO ACTIVE)
2bREARCABINDOORLEVER
2aJETTISON LEVER
1. AIRCREW EXTRACTION
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.
2. EMERGENCY EXIT DOORS
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.
b. For rear cabin doors, push jettison lever, located at bottom center of window, aft, then push window out.
LYNX WG13T.O
. 00-105E-9
LYN
X W
G13. 1
SPECIAL TOOLS/EQUIPMENTPower Rescue SawCrash Ax
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
AIRCRAFT PAINT SCHEME
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
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.
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
ENGINE SHUTDOWN1. ENGINE SHUTDOWN
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
1. AIRCREW EXTRACTION
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
SPECIAL TOOLS/EQUIPMENTPower Rescue SawCrash Ax
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.
2. AIRCREW EXTRACTION
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
SPECIAL TOOLS/EQUIPMENTPower Rescue SawCrash Ax
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
ENGINE SHUTDOWN1. ENGINE SHUTDOWN
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
1. AIRCREW EXTRACTION
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
SPECIAL TOOLS/EQUIPMENTPower Rescue SawCrash Ax
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)
SPECIAL TOOLS/EQUIPMENTPower Rescue SawCrash Ax
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.
SPECIAL TOOLS/EQUIPMENTPower Rescue SawCrash Ax
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.
4. AIRCREW EXTRACTION
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
SPECIAL TOOLS/EQUIPMENTPower Rescue SawCrash Ax
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
A K
ING
AE
W 2.3
ENGINE SHUTDOWN1. ENGINE SHUTDOWN
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
. 00-105E-9
SE
A K
ING
AE
W 2.
4
AIRCREW EXTRACTION1. AIRCREW EXTRACTION
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
SE
A K
ING
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.
* 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
TAIL ROTORDANGERAREA
MAIN ROTORDANGER AREA
CARTRIDGEINITIATEDRESCUEHOISTCABLESHEAR
HYDRAULIC OILRESERVOIRS ANDMAIN GEARBOX
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
SE
A K
ING
AS
W 5.
3
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
SPECIAL TOOLS/EQUIPMENTPower Rescue SawCrash Ax
AIRCRAFT ENTRY1. 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 ASW 5T.O
. 00-105E-9
SE
A K
ING
AS
W 5.
4
ENGINE SHUTDOWN1. ENGINE SHUTDOWN
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 master armament safety switch, located on the overhead panel, to SAFE position.
d. 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 extinguisher operating 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 master armament safety switch to SAFE position.
f. Turn battery master switch to OFF position.
1d, 2fBATTERY MASTER SWITCH
2aENGINE FIRE EXTINGUISHER& EMERGENCY PULL HANDLES
THROTTLES
ROTOR BRAKE
2bFIREEXTINGUISHEROPERATINGSWITCH
1a, 2cSPEED SELECTLEVERS
LANDINGGEARCONTROL
1b, 2dFIREWALL VALVES
PARKING BRAKE
SHOULDER HARNESS RELEASE
CARGORELEASE
SLIDING WINDOW RELEASE
JETTISON HANDLE
1c, 2eMASTER ARMAMENTSAFETY SWITCHWITH SAFETY PINAND STREAMER
SPECIAL WEAPONCONTROL BOX BRSL
SEA KING ASW 5T.O
. 00-105E-9
SE
A K
ING
AS
W 5.
5
AIRCREW EXTRACTION1. AIRCREW EXTRACTION
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. 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
1aUPPERPERSONNELDOOR
1bCABINWINDOWESCAPEHATCH
1cCARGODOORESCAPEHATCH
JUMPSEAT
AS ROLE:8 TROOP SEATS
1dCOCKPIT SIDEWINDOWS
AR &TROOPROLE:
1eCREW SEATS
1fTROOPSEATS
SEA KING HAR 3/SH 3DT.O
. 00-105E-9
SE
A K
ING
HA
R 3/S
H 3D
.1
AIRCRAFT HAZARDS
TAIL ROTORDANGERAREA
AIRCRAFT ARMAMENT - None is normally carried.
OTHER HAZARDS:Pyrotechnics: Signal pistol and cartridges
* 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
MAIN ROTORDANGER AREA
HOIST CABLECUTTER(CARTRIDGE)
HYDRAULIC OILRESERVOIRS ANDMAIN GEARBOX
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
SEA KING HAR 3/SH 3DT.O
. 00-105E-9
SE
A K
ING
HA
R 3/S
H 3D
.2
2aCOCKPIT WINDOW(BOTH SIDES)
2bCABIN ESCAPEHATCH
2b HANDLE
TO OPEN: PRESS AND TURN
EXIT RELEASE TURN
HF AERIAL
2cESCAPEHATCHES
3bENGINE FIREACCESSDOOR
FIRST AID KIT
PULL TABEXIT RELEASE
FIREEXTINGUISHER
2aCOCKPIT WINDOW(SIMILAR TOOPPOSITE SIDE)
1dSLIDINGENTRY DOOR
REDHANDLE
1aNORMALENTRY DOORLOWER SECTION
SPECIAL TOOLS/EQUIPMENTPower Rescue SawCrash Ax
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
FIRST AID KIT
FIREEXT.
SEA KING HAR 3/SH 3DT.O
. 00-105E-9
SE
A K
ING
HA
R 3/S
H 3D
. 3
ENGINE SHUTDOWN1. ENGINE SHUTDOWN
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 HAR 3/SH 3DT.O
. 00-105E-9
SE
A K
ING
HA
R 3/S
H 3D
.
BETA LIGHTS ARE FIXED AROUND ESCAPE EXITS
1aUPPERPERSONNELDOOR
1bCABINWINDOWESCAPEHATCH
1cCARGODOORESCAPEHATCH
WINDOWS (5)
CREW DOOR
CARGO DOORWINDOW
EMERGENCY EXITS
1gRELEASE KNOB
1ePILOTS AND RADAROPERATOR SEATS
1dCOCKPITWINDOWS
1fAFT CABIN SEATS
1gTROOP/PASSENGERSEATS
4
1. AIRCREW EXTRACTION
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. 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
A K
ING
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.
* 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
TAIL ROTORDANGERAREA
MAIN ROTORDANGER AREA
CARTRIDGEINITIATEDRESCUEHOISTCABLESHEAR
HYDRAULIC OILRESERVOIRS ANDMAIN GEARBOX
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 HAS/ASW 6T.O
. 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
SEA KING HAS/ASW 6T.O
. 00-105E-9
SE
A K
ING
HA
S/A
SW
6.3
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
SPECIAL TOOLS/EQUIPMENTPower Rescue SawCrash Ax
AIRCRAFT ENTRY1. 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 HAS/ASW 6T.O
. 00-105E-9
SE
A K
ING
HA
S/A
SW
6.4
ENGINE SHUTDOWN1. ENGINE SHUTDOWN
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 master armament safety switch, located on the overhead panel, to SAFE position.
d. 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 extinguisher operating 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 master armament safety switch to SAFE position.
f. Turn battery master switch to OFF position.
1d, 2fBATTERY MASTER SWITCH
2aENGINE FIRE EXTINGUISHER& EMERGENCY PULL HANDLES
THROTTLES
ROTOR BRAKE
2bFIREEXTINGUISHEROPERATINGSWITCH
1a, 2cSPEED SELECTLEVERS
LANDINGGEARCONTROL
1b, 2dFIREWALL VALVES
PARKING BRAKE
SHOULDER HARNESS RELEASE
CARGORELEASE
SLIDING WINDOW RELEASE
JETTISON HANDLE
1c, 2eMASTER ARMAMENTSAFETY SWITCHWITH SAFETY PINAND STREAMER
SPECIAL WEAPONCONTROL BOX BRSL
SEA KING HAS/ASW 6T.O
. 00-105E-9
SE
A K
ING
HA
S/A
SW
6.5
AIRCREW EXTRACTION1. AIRCREW EXTRACTION
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. 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
BETA LIGHTS ARE FIXED AROUND ESCAPE EXITS
1aUPPERPERSONNELDOOR
1bCABINWINDOWESCAPEHATCH
1cCARGODOORESCAPEHATCH