1997 Airbus/Eurocopter AS 365N-3 for sale, Netherlands

Price: USD $2,142,704
Price entered as: €2,000,000 Price Reduced
Europe, Netherlands
Year
1997
S/N
TBD
Reg
-
TT
9,858

Aircraft Description

2.0M EURO - PRICE REDUCED

AIRCRAFT 1997 AS365N3

LOCATION NETHERLANDS

AIRFRAME

AIRFRAME HOURS 9,858

AIRFRAME LANDINGS 21,306

CONFIGURATION SAR

 

SAND FILTERS, FIXED PARTS

AUXILIARY FUEL TANK IN THE HOLD, FIXED PARTS

GOODRICH HOIST CLASS2 (272KG) FIXED PARTS

SPECTROLAB SX-5 SEARCH LIGHT

CARGO SLING WITH DYNAMOMETER AND ELECTRICAL MIRROR (1600KG) FIXED

PARTS

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AIRFRAME / TOTAL LANDINGS / ENGINES / APU / WEIGHT

AIRFRAME

AIRFRAME HOURS 9,858
AIRFRAME LANDINGS 21,306
CONFIGURATION SAR

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
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

ENGINES

2 SAFRAN ARRIEL 2C TURBINE ENGINES PROVIDING EACH 729 KW
(990CH – 977 SHP) SUPER CONTINGENCY RATING, F ULL AUTHORITY
DIGITAL ENGINES CONTROL SYSTEM
NUMBER 2 X SAFRAN ARRIEL 2C
LEFT - 72 L/H: 24,045
RIGHT - 72 R/H: 49,005
1 FUEL SYSTEM INCLUDING 5 TANKS SPLIT INTO 2 GROUPS, WITH A TOTAL
USABLE CAPACITY OF 1,135 LITRES, 4 IMMERSED BOOSTER PUMPS, 1 TRANSFER
PUMP AND AN INDICATION OF LOW LEVELS. OPTIONAL A LONG-RANGE TANK
CAN BE ADDED.
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
2 WINDSHIELD WIPERS
2 ILLUMINATED CHART HOLDERS
2 HEADSET HOLDERS (SILEX)
1 PORTABLE FIRE-EXTINGUISHER
1 FLIGHT MANUAL
FIRST-AID KIT JAR-OPS COMPLIANT
  • AVIONICS & CONNECTIVITY
    AVIONICS

    VHF-AM ROCKWELL COLLINS 422C (8.33 KHZ) (2X)
    INTER COMMUNICATION SYSTEM TEAM TB 31 WITH 3 CONTROL BOXES
    1976 (1 IN CABIN)
    PA WITH 4 LOUDSPEAKERS BAKER M1050
    THALES AHV-16 RADIO ALTIMETER
    ATC TRANSPONDER GARMIN GTX-330 (MODE-S)
    VHF/FM MARITIME NAT NPX-138
    CVR HONEYWELL AR COMBI
    UHF HONEYWELL KTR-909
    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 155 FLIGHT DIRECTOR COUPLER
    TELEPHONICS RDR1400 WEATHER/SEARCH RADAR
    JEPPENSEN MAP SKYFORCE SKYMAP IIIC

    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
    2 FUEL PRESSURE INDICATORS
    1 MAIN GEARBOX OIL PRESSURE AND TEMP IND
    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 COPILOT’S SIDE
    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
    ICING DETECTOR
    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 HEIGHTEACH FITTED WITH A SAFETY BELT AND SHOULDER 4-POINT
    HARNESS
    SAR LAY-OUT
    3 POINTS HARNESSES
    2 PILOT AND CO-PILOT JETTISONABLE DOORS, EACH FITTED WITH A BAD
    WEATHER WINDOW AND AN INTERNAL STORAGE UNIT. DOORS WITH AIR INLETS
    2 HINGED JETTISONABLE CABIN FRONT DOORS
    2 ENLARGED AND BUBBLED REAR SLIDING DOORS WITH JETTISONABLE WINDOW
    FROM INSIDE AND
    OUTSIDE
    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
  • EXTERIOR
    Yellow
  • Additional Equipment & Information
    DIRECTION FINDER CHELTON DF935
    HELICOPTER EMERGENCY EGRESS LIGHTING (HEEL)
    HR-SMITH CPI-503 ADELT
    DUKANE DK120 ULB
    SAAB R4 AIS SYSTEM
    ICE DETECTION KIT

    OGP RECOMMENDED EQUIPMENT

    IFR CERTIFIED
    AUTOPLIOT OR AFCS
    2 PRIMARY TRANSCEIVERS WITH 1 VHF MINIMUM
    MODE C OR S TRANSPONDER
    ELT WITH TSO 126
    GPS (IFR TSO)
    1 ADF
    2 VOR/ILS & 1 DME
    INSTANTANEOUS VERTICAL SPEED INDICATOR (IVSI)
    RADIO ALTIMETER WITH AUDIO/VISUAL ALERT WITH ANALOGUE DISPLAY
    WEATHER RADAR WITH COLOUR SCREEN (MIN. SCALE 2,5NM)
    PUBLIC ADDRESS/INTERCOM SYSTEM WIRELESS
    CVR - AS MANDATED BY CAA
    AIRFRAME/ENGINE VIBRATION MONITORING SYSTEM
    UPPER TORSO RESTRAINTS, ALL SEATS
    1 FIRST-AID KITS
    2 FIRE EXTINGUISHERS WITH PRESSURE GAUGES PREFERRED
    EMERGENCY EXIT LIGHTING SYSTEM
    AIRCRAFT FLOTATION EQUIPMENT
    EMERGENCY POP-OUT WINDOW
    SONAR TRANSMITTER (PINGER)
    AUTO-INFLATION OF FUSELAGE FLOATS
    HEATING FOR CABIN
    LITTER KIT, CARGO HOOK, HOIST

    TRANSMISSION

    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
    FLIGHT CONTROLS
    1 MAIN ROTOR WITH 4 GLASS AND CARBON-FIBRE BLADES WITH STARFLEX
    HEAD FITTED WITH GUSTAND 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

    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

    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

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