2006 Airbus/Eurocopter AS 365N-3 for sale, Belgium

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Airbus/Eurocopter AS 365N-3 Exterior
Price: €2,000,000 Price Reduced
Europe, Belgium
Year
2006
S/N
6740
Reg
OO-NHM
TT
5042

Aircraft Description

2.0M EURO - PRICE REDUCED

2006 AS365-N3

TIME SINCE NEW 5,042
LANDINGS SINCE NEW 11,612

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.
BUILT 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.

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AIRFRAME / TOTAL LANDINGS / ENGINES / APU / WEIGHT

AIRFRAME

Time Since New 5,042
Landings Since New 11,612

ENGINES

Component Times
Item Retirement or OH Hours Remaining Hours Remaining % Remaining % Remaining
MRB’s 20,000 14,919 75%
MGB 3,000 968 32%
Starflex 5,000 4,173 83%
TGB 3,000 2,416 80%

2 x Arriel 2C No 1 No 2 No 1 No 2
TTSN 9,374 10,715
Engine MO3 3,500 3,007 2,633 86% 75%
Engine MO3 Calendar 15 years 13.5 years 13 years 90% 87%


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: 24396
RIGHT 72: R/H: 24057
  • AVIONICS & CONNECTIVITY
    VHF-AM ROCKWELL COLLINS VHF-422C (2X).
    INTER COMMUNICATION SYSTEM TEAM TB 31 WITH 3 CONTROL BOXES 1976 (1 IN CABIN.)
    PA WITH 4 LOUDSPEAKERS BAKER M1050.
    HEADSETS SILEC 4449-1 (2X).
    THALES AHV-16 RADIO ALTIMETER.
    ATC TRANSPONDER MST67A (MODE-S).
    HF/SSB BENDIX KING KHF950.
    VHF/FM MARITIME NAT NPX-138.
    SSCVFDR HONEYWELL AR COMBI.
    TCAS GOODRICH HP899.
    TCAS RYAN TAS600.
    ADF HONEYWELL KDF-806.
    DME HONEYWELL KDM 706A.
    VOR/ILS HONEYWELL KNR-634A (2X).
    AIR DATA COMPUTER SHADIN ADC-2000.
    FLIGHT MANAGEMENT SYSTEM UNIVERSAL UNS-1K (INCLUDING GPS).
    SFIM CDV 85 D3 FLIGHT DIRECTOR COUPLER.
    TELEPHONICS RDR1400 WEATHER/SEARCH RADAR.
    UMS.
    HUMS FULL (M’ARMS).
    JEPPENSEN MAP HONEYWELL KMD850.
    JEPPENSEN MAP SKYFORCE SKYMAP IIIC.

    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.
  • 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.
    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.
    FIRST-AID KIT JAR-OPS COMPLIANT.
  • Additional Equipment & Information
    EMERGENCY FLOATATION WITH AFDS.
    INTERNAL AERAZUR (SR-8) LIFE RAFT INSTALLATION.
    HELICOPTER EMERGENCY EGRESS LIGHTING (HEEL).
    HR-SMITH CPI-503 ADELT.
    DUKANE DK120 ULB.
    AVAD RACAL V694 100FT, CH, UC WARNING.
    ELT KANNAD 406AF.
    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.
    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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