manufacturer
Airbus
configuration
Offshore
condition
Used
year
2009
time
4325
helicopter location
Africa
listing ID
HT9667
Description
Price reduced.....contact us to discuss
Oil and Gas Configuration. The cabin floor is capable of the various optional types of arrangements, and the first aid kit is EU-OPS compliant. Avionics includes air data computer Shadin ADC-2000, GPS navigation Freeflight 2101 I/O approach+ and HUMS Full (M’ARMS).
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 AA20-431
- THALES AHV-16 RADIO ALTIMETER
- ATC TRANSPONDER MST67A (MODE-S)
- 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)
- DF INSTALLATION (CHELTON)
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
CABIN
- 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
- 11 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 (SILEX)
- 1 PORTABLE FIRE-EXTINGUISHER
- 1 FLIGHT MANUAL
- 1 FIRST-AID KIT EU-OPS COMPLIANT
general characteristics
- AIRFRAME CYCLES: 9,110
- 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
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
Other AS365N3 Listings:
