manufacturer
Airbus
configuration
Search and rescue
condition
Used
year
1991
time
9280
helicopter location
Europe
listing ID
HT9483
Description
- CONFIGURATION: SAR WITH CVR INSTALLATION
- GOODRICH HOIST CLASS 2 (272KG) FIXED PARTS
- CARGO SLING WITH DYNAMOMETER AND
- ELECTRICAL MIRROR (1,600KG) FIXED PARTS
avionics
- VHF-AM VHF-422C (2X) (8.33KHZ UPGRADED)
- INTER COMMUNICATION SYSTEM TEAM TB 31 WITH 3 CONTROL BOXES 1976 (1 IN CABIN)
- PA WITH 4 LOUDSPEAKERS TEAM BA1920
- THALES AHV-16 RADIO ALTIMETER
- ATC TRANSPONDER GARMIN GTX-330 (MODE-S)
- SAT COM LATTITUDE
- VHF/FM MARITIME NAT NPX-138
- CVR HONEYWELL 30B
- ADF KING KDF-806
- DME KING KDM-706A
- VOR/ILS KING KNR-634A
- AIR DATA COMPUTER
- GPS MARCONI CMA3012
- TELEPHONICS RDR1400 WEATHER/SEARCH RADAR
- RADAR INTERFACE IU2023
- JEPPESEN MAP SKYFORCE SKYMAP IIIC
equipment
INSTRUMENTS
- 2 ALTIMETERS
- 2 AIRSPEED INDICATORS WITH DIGITAL SPEED DISPLAY
- 2 GYRO HORIZON
- 2 SFIM CG130 + 4” HSI
- 1 SELECTOR SWITCH FOR GYROCOMPASS #1 & #2
- 2 RATE-OF-CLIMB INDICATORS, WITH PROVISIONS FOR RATE-OF-CLIMB
- PRE-SET ON PILOTS’ SIDE
- 1 RMI ON PILOTS’ SIDE
- 1 STANDBY GYRO HORIZON
- 3 HEATED PITOT HEADS
- DUAL TORQUEMETER ON PILOT SIDE
- TAIL PIPE TEMPERATURE INDICATORS
- 2 ENGINE OIL PRESSURE AND TEMPERATURE INDICATORS
- 2 FUEL PRESSURE INDICATORS
- 1 MAIN GEARBOX OIL PRESSURE AND TEMP INDICATOR
- 2 HYDRAULIC PRESSURE GAUGES
- 1 VOLTMETER
- 1 AMMETER
- 1 DUAL FUEL CONTENTS GAUGE
- 1 FUEL CIRCUIT CONTROL AND INSPECTION PANEL
- 1 ELECTRICAL CONTROL PANEL
- 1 LANDING GEAR POSITION SELECTOR AND INDICATOR
- 2 STOPWATCHES
- 1 TRIPLE TACHOMETER FOR ROTOR AND 1&2 FREE TURBINES RPM ON PILOT’S SIDE
- 1 ROTOR TACHOMETER ON CO-PILOT’S SIDE
- 2 NG INDICATORS (GAS GEN 1&2)
- 1 STANDBY MAGNETIC COMPASS
- 1 OUTSIDE AIR TEMPERATURE INDICATOR
- 1 WARNING PANEL
- 2 MASTER ALARM LIGHTS
- 2 MANOEUVRE LIMIT WARNING LIGHT
- 2 FIRE WARNING LIGHTS AND 2 DUAL FIRE EXTINGUISHING CONTROLS FOR ENGINE BAYS
- 1 “L/G NOT EXTENDED” WARNING LIGHT
- SPARE SPACE FOR RADAR SCREEN AND COM/NAV EQUIPMENT
- ICING DETECTOR (ROSE MOUNT)
ADDITIONAL EQUIPMENT
- DIRECTION FINDER CHELTON DF7 SYSTEM
- DOPPLER INSTALLATION, RACAL D91
- HELICOPTER EMERGENCY EGRESS LIGHTING (HEEL)
- HR-SMITH CPI-503 ADELT
- DUKANE DK120 ULB
- AVAD RACAL V694 100FT, CH, UC WARNING
- SAND FILTERS, FIXED PARTS
- GOODRICH HOIST CLASS2 (272KG) FIXED PARTS
- SPECTROLAB SX-5 SEARCH LIGHT
- CARGO SLING WITH DYNAMOMETER AND ELECTRICAL MIRROR (1600KG) FIXED PARTS
- RN NAV2 + DOUPLER D91
- DE-ICED WINSHIELD
- FLIR EO/IR HARD POINTS
- HEEL SYSTEM
- UHF RADIO INSTALLATION
- AIS TRANSPONDER INSTALLATION
- SAR CABIN LAYOUT / CVR INSTALLATION
interior
- 1 CABIN FLOOR CAPABLE OF THE VARIOUS OPTIONAL TYPES OF ARRANGEMENTS
- 2 REMOVABLE PILOT AND CO-PILOT HIGH BACK-REST SEATS, ADJUSTABLE IN REACH AND HEIGHT EACH FITTED WITH A SAFETY BELT AND SHOULDER 4-POINT HARNESS SAR LAY-OUT
- 2 PILOT AND CO-PILOT JETTISONABLE DOORS, EACH FITTED WITH A BAD WEATHER WINDOW AND AN INTERNAL STORAGE UNIT.
- 2 HINGED JETTISONABLE CABIN FRONT DOORS
- 2 ENLARGED AND BUBBLED REAR SLIDING DOORS WITH JETTISONABLE WINDOW FROM INSIDE AND OUTSIDE
- 4 RETRACTABLE FOOTSTEPS
- 2 UPPER TINTED PANES
- CABIN UPHOLSTERY WITH SOUND PROVING
- 1 INSTRUMENT PANEL, ONE CONSOLE AND ONE CEILING PANEL
- DUAL FLIGHT CONTROL
- ENGINE CONTROLS
- ROTOR BRAKE CONTROL
- 1 HEATING/DEMISTING/VENTILATION SYSTEM
- 2 WINDSHIELD WIPERS
- 2 ILLUMINATED CHART HOLDERS
- 2 HEADSET HOLDERS (SILEX)
- 1 PORTABLE FIRE-EXTINGUISHER
general characteristics
FLIGHT CONTROLS
- 1 MAIN ROTOR WITH 4 GLASS AND CARBON-FIBRE BLADES WITH STARFLEX HEAD FITTED WITH GUST AND DROOP STOPS, MAST FITTED WITH ROTOR RPM PHONIC WHEEL
- 1 TAIL ROTOR WITH 11 COMPOSITE MATERIAL BLADES BUILT INTO THE VERTICAL FIN
- 1 FLYING CONTROL SYSTEM, FITTED WITH 3 DUAL-CHAMBER/DUAL BODY MAIN SERVO UNITS (CYCLIC AND COLLECTIVE PITCH CHANNELS) AND 1 DUAL-CHAMBER/DUAL BODY REAR SERVO-UNIT (ON TAIL ROTOR PITCH
CONTROL CHANNEL)
- 1 SFIM CDV 155 FLIGHT DIRECTOR COUPLER (4-AXIS) (WITH 2ND RADAR ALTIMETER)
ELECTRICAL INSTALLATION
- 2 250VA, 115/26V, 400 HZ 1-PHASE STATIC INVERTERS
- 2 STARTER GENERATORS (4,8 KW, 28VDC)
- 1 43AMP-HR CADMIUM-NICKEL BATTERY WITH TEMP DETECTOR
- 1 EXTERNAL DC POWER RECEPTACLE
- 1 INSTRUMENT WHITE/BLUE LIGHTING SYSTEM
- 2 CABIN EXTENSION LIGHTS
- 1 INSTRUMENT LIGHT FOR FLIGHT IN STORMY CONDITIONS
- 1 CABIN DOME LIGHT
- 4 CABIN LIGHT STRIPS
- 10KVA ALTERNATOR
- 1 LUGGAGE HOLD DOME-LIGHT
- 3 POSITION LIGHT
- 1 ANTI-COLLISION LIGHT
- RETRACTABLE LH LANDING LIGHT, ADJUSTABLE IN ELEVATION
- RETRACTABLE RH LANDING LIGHT, ADJUSTABLE IN ELEVATION AND IN AZIMUTH ALLOWING SEARCH LIGHT AND HOIST LIGHT
- 1 CABIN POWER OUTLET (28VDC)
- 1 EMERGENCY BATTERY FOR AUTOMATIC LIGHTING OF THE DOME LIGHTS AND SIGNS
- 1 ROTOR TACHOMETER ON CO-PILOT’S SIDE UNDER FUSELAGE ANTI-COLLISION STROBE LIGHT
TRANSMISSION
- 1 MAIN GEARBOX, ANTI-VIBRATION MOUNTED, WITH OIL SIGHT GAUGE, MAGNETIC PLUG, OIL PRESSURE AND TEMPERATURE PICK-UP, LUBRICATION SYSTEM, THERMAL SWITCH, ROTOR TACHOMETER DRIVE AND HOLES FOR
ENDOSCOPE AND OIL SAMPLING
- 1 TAIL GEARBOX WITH OIL SIGHT GAUGE AND MAGNETIC PLUG
- 1 MAIN GEARBOX OIL COOLING SYSTEM
- 2 ENGINE/MAIN GEARBOX COUPLING SHAFTS
- 1 ROTOR BRAKE
- 2 FREE WHEELS INTEGRAL WITH MAIN GEARBOX
HYDRAULICS
- 2 INDEPENDENT HYDRAULIC SYSTEMS FEEDING THE SERVO-UNITS, LANDING GEAR ACTUATION SYSTEM AND ASSISTED BRAKES
- SELF-SEALING HYDRAULIC GROUND COUPLING
- 1 STAND-BY HYDRAULIC SYSTEM WITH ELECTRO-PUMP FOR EMERGENCY ACTUATING OF THE LANDING GEAR, HYDRAULIC ASSISTANCE FOR FLIGHT CONTROLS TESTS ON GROUND WITH ROTOR STOPPED AND PARK BRAKE
PRESSURE
GENERAL
- FUSELAGE COMPRISING THE CABIN AND LUGGAGE HOLD
- LUGGAGE HOLDS WITH FLOOR, TIE DOWN NET AND ACCESS DOOR
- TAIL BOOM WITH STABILIZER FITTED WITH 2X LATERAL FINS AND TERMINATED BY A SHROUDED TAILROTOR BUILD INTO THE VERTICAL MAIN FIN
- RETRACTABLE TRICYCLE LANDING GEAR WITH AXIALLY LOCKABLE CASTERING NOSE WHEEL UNIT,ASSISTED DIFFERENTIAL BRAKES ON PILOTS AND CO-PILOTS
- STATION AND PARKING BRAKE
- BUILD IN FOOTSTEPS 2 ON EACH SIDE FOR ACCESS TO THE TRANSMISSION DECK
- FIXED PARTS FOR MAIN ROTOR BLADE FOLDING
- STRUCTURAL PROVISIONS FOR 1600KG CARGO SLING
- STRUCTURAL REINFORCEMENTS FOR HOIST
- JACKING, HOISTING, MOORING AND GRIPPING POINTS
- 1 FUEL SYSTEM INCLUDING 5 TANKS SPLIT INTO 2 GROUPS, WITH A TOTAL USABLE CAPACITY OF 1135 LITRES, 4 IMMERSED BOOSTER PUMPS, 1 TRANSFER - PUMP AND AN INDICATION OF LOW LEVELS.
- 1 HYDRAULIC BLEED CONTROL FOR THE WHOLE FUEL SYSTEM
- 2 ENGINES LUBRICATION AND OIL COOLING SYSTEMS
- 2 FIRE DETECTION AND EXTINGUISHING SYSTEMS
- 2 ANTI-ICING AIR INTAKE GRIDS
- 2 HYDRAULIC SENSORS FOR TORQUE METER BUILT INTO THE ENGINES
- 2 ENGINES EXHAUST PIPES
- ENGINE FLUSHING DEVICE
