manufacturer
Airbus
configuration
Offshore
condition
Used
year
2009
time
3100
helicopter location
Africa
listing ID
HT9665
Description
Price reduced.....contact us to discuss
Oil & gas configured, 2009 AS365N3 for sale. Additional equipment includes emergency flotation with AFDS, helicopter emergency egress lighting, Dukane DK120 ULB and sand filters (fixed parts).
Location: Ivory Coast
avionics
AVIONICS
- VHF-AM ROCKWELL COLLINS (2X) KTR 908
- INTER COMMUNICATION SYSTEM TEAM TB 31 WITH 3 CONTROL BOXES 1976 (1 IN CABIN)
- PA WITH 4 LOUDSPEAKERS NAT AA30-431
- THALES AHV-16 RADIO ALTIMETER
- ATC TRANSPONDER MST67A (MODE-S)
- HF/SSB BENDIX KING KHF950
- SSCVFDR HONEYWELL AR COMBI
- ADF HONEYWELL KDF-806
- DME HONEYWELL KDM 706A
- VOR/ILS HONEYWELL KNR-634A (2X)
- AIR DATA COMPUTER SHADIN ADC-2000
- GPS NAVIGATION FREEFLIGHT 2101 I/O APPROACH+
- SFIM CDV 85 D3 FLIGHT DIRECTOR COUPLER
- TELEPHONICS RDR1600C WEATHER/SEARCH RADAR
- UMS
- HUMS FULL (M’ARMS)
INSTRUMENTS
- 2 X2 PFD/ND COLLINS MFD-255
- 1 STANDBY GYRO HORIZON
- 1 STANDBY ALTIMETER
- 1 STANDBY AIRSPEED INDICATOR
- 1 DUAL TORQUE, ON PILOT’S SIDE
- 2 ENGINES EXHAUST PIPES TEMPERATURE INDICATOR
- 2 ENGINES OIL PRESSURE AND TEMP 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
- 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
- 1 OVERHEAD PANEL INCLUDING ENGINE CONTROL PANEL WITH 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)
- 1 LANDING GEAR POSITION SELECTOR AND INDICATOR
- 1 AFCS CONTROL PANEL
equipment
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 FENESTRON TYPE TAIL ROTOR WITH COMPOSITE MATERIAL BLADES BUILT INTO THE VERTICAL FIN
- 1 FLIGHT 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 PA155D DUPLEX-TYPE AUTO PILOT
ADDITIONAL EQUIPMENT
- EMERGENCY FLOATATION WITH AFDS
- EXTERNAL AERAZUR (SR-10) LIFE RAFT INSTALLATION, INCLUDING CABIN FOOTSTEPS
- HELICOPTER EMERGENCY EGRESS LIGHTING (HEEL)
- HR-SMITH CPI-503 ADELT
- DUKANE DK120 ULB
- AVAD RACAL V694 100FT, CH, UC WARNING
- FRONT GLASS INSTEAD OF PLEXIGLASS
RETROFITS
- SATCOM (COMMUNICATION AND TRACKING) (SKYROUTER)
- SSQAR INSTALLATION
- VHF/FM INSTALLATION (NPX-138)
PROVISIONS
- SAND FILTERS, FIXED PARTS
- AUXILIARY FUEL TANK IN THE HOLD, FIXED PARTS
- GOODRICH HOIST CLASS1 (272KG) FIXED PARTS
- CARGO SLING WITH DYNAMOMETER AND ELECTRICAL MIRROR (1600KG) FIXED PARTS
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
- 12 STANDARD SEAT LAY-OUT
- 4 POINTS HARNESSES FOR 11 STANDARD SEAT LAYOUTS
- 2 PILOT AND CO-PILOT JETTISON ABLE DOORS, EACH FITTED WITH A BAD WEATHER WINDOW AND AN INTERNAL STORAGE UNIT
- DOORS WITH AIR INLETS
- 2 HINGED JETTISON ABLE CABIN FRONT DOORS
- 2 ENLARGED AND BUBBLED REAR SLIDING DOORS WITH JETTISON ABLE WINDOW FROM INSIDE AND OUTSIDE
- 2 RETRACTABLE FOOTSTEPS
- 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 UPPER TINTED PANES
- 2 FRONT PLEXIGLASS PANES
- 2 WINDSHIELD WIPERS
- 2 ILLUMINATED CHART HOLDERS
- 2 HEADSET HOLDERS
- 1 PORTABLE FIRE-EXTINGUISHER
- 1 FLIGHT MANUAL
- FIRST-AID KIT EU-OPS COMPLIANT
general characteristics
- AIRFRAME CYCLES: 8,500
- FUSELAGE COMPRISING THE CABIN AND LUGGAGE HOLD
- LONG NOSE
- LUGGAGE HOLD WITH FLOOR, TIE DOWN NET AND ACCESS DOOR
- TAIL BOOM WITH STABILIZER FITTED WITH 2X LATERAL FINS AND TERMINATED BY A SHROUDED TAIL ROTOR 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
- 3 HEATED PITOT HEADS
- BUILD IN FOOTSTEPS 2 ON EACH SIDE FOR ACCESS TO THE TRANSMISSION DECK
- ANTI-CORROSION PROTECTION
- FIXED PARTS FOR MAIN ROTOR BLADE FOLDING
- STRUCTURAL PROVISIONS FOR 1600KG CARGO SLING
- STRUCTURAL REINFORCEMENTS FOR HOIST
- JACKING, HOISTING, MOORING AND GRIPPING POINTS
POWER PLANT
- 1 FUEL SYSTEM INCL. 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
- 2 ENGINES LUBRICATION AND OIL COOLING SYSTEMS
- 2 FIRE DETECTION AND EXTINGUISHING SYSTEMS
- 2 ANTI-ICING AIR INTAKE GRIDS
- 2 PHASE ANGLE TORQUE METER SENSORS BUILT INTO THE ENGINES
- 2 ENGINES EXHAUST PIPES
- ENGINE FLUSHING DEVICE
TRANSMISSION SYSTEM
- 1 MAIN GEARBOX
- 1 TAIL GEARBOX
- 1 MAIN GEARBOX OIL COOLING SYSTEM
- 2 ENGINE/MAIN GEARBOX COUPLING SHAFTS
- 1 TAIL ROTOR DRIVE SHAFT
- 1 ROTOR BRAKE
- 2 FREE WHEELS INTEGRAL WITH MAIN GEARBOX
HYDRAULIC SYSTEM
- 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
ELECTRICAL INSTALLATION
- 2 STATIC INVERTERS (800VA, 115/26V, 400HZ, 1PHASE)
- 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
- 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
- UNDER FUSELAGE ANTI-COLLISION STROBE LIGHT
