2009 Airbus/Eurocopter AS 365N-3 for sale, Ivory Coast

Price: USD $2,142,704
Price entered as: €2,000,000 Price Reduced
West Africa, Ivory Coast
Year
2009
S/N
TBD
Reg
-
TT
3,100

Aircraft Description

2.0M EURO - PRICE REDUCED

AIRCRAFT 2009 AS365N3

LOCATION IVORY COAST

AIRFRAME HOURS 3,100

AIRFRAME CYCLES 8,500

CONFIGURATION OIL & GAS

 

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

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AIRFRAME / TOTAL LANDINGS / ENGINES / APU / WEIGHT

AIRFRAME

AIRFRAME HOURS 3,100
AIRFRAME CYCLES 8,500
CONFIGURATION OIL & GAS

ENGINES

2 SAFRAN ARRIEL 2C TURBINE ENGINES PROVIDING EACH 729 KW
(977 SHP - TAKE OFF POWER RATING), FULL AUTHORITY DIGITAL ENGINES
CONTROL SYSTEM (NO MECHANICAL BACKUP NECESSARY)
NUMBER 2 X SAFRAN ARRIEL 2C
LEFT - 72 L/H: 24,512
RIGHT - 72 R/H: 24,451
  • AVIONICS & CONNECTIVITY
    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 ΔNG 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
  • Interior & Entertainment
    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
  • EXTERIOR
    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
  • Additional Equipment & Information
    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)

    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

    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
    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
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