1991 Eurocopter AS365 N2 Turbine Helicopter For Sale

Features include 4 Axis Autopilot, 10 pax seating, Fuselage comprising the cabin & luggage hold, Retractable Tricycle Landing Gear, Assisted Differential Brakes on pilots & co-pilots station & Parking Brake. Includes Jacking, Hoisting, Mooring & Gripping Points.

Type:
Helicopter (Turbine)
Manufacturer:
Eurocopter
Model:
AS365 N2
Year:
1991
Serial Number:
Enquire
Reg. Number:
Enquire
Total Time:
9,280 Hours
Seats:
Enquire
Price:
Price upon request

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Price:
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Aircraft Type:
Aircraft Model & Manufacturer:
Year:
1991
Total Time:
9280
Registration Number:
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Serial Number:
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Seats:
Not Listed
Aircraft Location:
Contact Name:
Stephen Green
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Description

AIRFRAME
HOURS 9,280
CYCLES 15,675
CONFIGURATION SAR WITH CVR INSTALLATION

ENGINES
2 SAFRAN ARRIEL 1C2 TURBINE ENGINES PROVIDING EACH 569 KW
(774CH – 763 SHP) SUPER CONTINGENCY RATING,
FULL AUTHORITY DIGITAL ENGINES CONTROL SYSTEM
NUMBER 2 X SAFRAN ARRIEL 1C2
LEFT – 71 L/H: 12,162
RIGHT – 71 R/H: 9,343
1 FUEL SYSTEM INCLUDING 5 TANKS SPLIT INTO 2 GROUPS, WITH A TOTAL USABLE CAPACITY OF 1135 LITRES, 4 IMMERSED BOOSTER PUMPS, 1 TRANSFER PUMP & AN INDICATION OF LOW LEVELS.
1 HYDRAULIC BLEED CONTROL FOR THE WHOLE FUEL SYSTEM
2 ENGINES LUBRICATION & OIL COOLING SYSTEMS
2 FIRE DETECTION & EXTINGUISHING SYSTEMS
2 ANTI-ICING AIR INTAKE GRIDS
2 HYDRAULIC SENSORS FOR TORQUEMETER BUILT INTO THE ENGINES
2 ENGINES EXHAUST PIPES
ENGINE FLUSHING DEVICE

TRANSMISSION
1 MAIN GEARBOX, ANTI-VIBRATION MOUNTED, WITH OIL SIGHT GAUGE, MAGNETIC PLUG, OIL PRESSURE & TEMPERATURE PICK-UP, LUBRICATION SYSTEM, THERMAL SWITCH, ROTOR TACHOMETER DRIVE & HOLES FOR ENDOSCOPE & OIL SAMPLING.
1 TAIL GEARBOX WITH OIL SIGHT GAUGE & MAGNETIC PLUG
1 MAIN GEARBOX OIL COOLING SYSTEM
2 ENGINE/MAIN GEARBOX COUPLING SHAFTS
1 ROTOR BRAKE
2 FREE WHEELS INTEGRAL WITH MAIN GEARBOX

HYDRAULICS
2 INDEPENDENT HYDRAULIC SYSTEMS FEEDING THE SERVO-UNITS, LANDING GEAR ACTUATION SYSTEM & 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 & PARK BRAKE PRESSURE

FLIGHT CONTROLS
1 MAIN ROTOR WITH 4 GLASS & CARBON-FIBRE BLADES WITH STARFLEX HEAD FITTED WITH GUST & DROOP STOPS, MAST FITTED WITH ROTOR RPM PHONIC WHEEL
1 TAIL ROTOR WITH 11 COMPOSITE MATERIAL BLADES BUILT INTO THE VERTICAL FIN
1 FLYING CONTROL SYSTEM, FITTED WITH 3 DUAL-CHAMBER/DUAL BODY
MAIN SERVO UNITS (CYCLIC & COLLECTIVE PITCH CHANNELS) & 1 DUAL-CHAMBER/DUAL BODY REAR SERVO-UNIT (ON TAIL ROTOR PITCH
CONTROL CHANNEL)
1 SFIM CDV 155 FLIGHT DIRECTOR COUPLER (4-AXIS) (WITH 2ND RADAR ALTIMETER)

ELECTRICAL INSTALLATION
2 250VA, 115/26V, 400 HZ 1-PHASE STATIC INVERTERS
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
10KVA ALTERNATOR
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 & IN AZIMUTH ALLOWING SEARCH LIGHT & HOIST LIGHT
1 CABIN POWER OUTLET (28VDC)
1 EMERGENCY BATTERY FOR AUTOMATIC LIGHTING OF THE DOME LIGHTS & SIGNS
1 ROTOR TACHOMETER ON CO-PILOT’S SIDE
UNDER FUSELAGE ANTI-COLLISION STROBE LIGHT

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
3 HEATED PITOT HEADS
DUAL TORQUEMETER ON PILOT SIDE
TAIL PIPE TEMPERATURE INDICATORS
2 ENGINE OIL PRESSURE & TEMPERATURE INDICATORS
2 FUEL PRESSURE INDICATORS
1 MAIN GEARBOX OIL PRESSURE & TEMP INDICATOR
2 HYDRAULIC PRESSURE GAUGES
1 VOLTMETER
1 AMMETER
1 DUAL FUEL CONTENTS GAUGE
1 FUEL CIRCUIT CONTROL & INSPECTION PANEL
1 ELECTRICAL CONTROL PANEL
1 LANDING GEAR POSITION SELECTOR & INDICATOR
2 STOPWATCHES
1 TRIPLE TACHOMETER FOR ROTOR & 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
2 FIRE WARNING LIGHTS & 2 DUAL FIRE EXTINGUISHING CONTROLS FOR ENGINE BAYS
1 “L/G NOT EXTENDED” WARNING LIGHT
SPARE SPACE FOR RADAR SCREEN & COM/NAV EQUIPMENT
ICING DETECTOR (ROSE MOUNT)

AVIONICS
VHF-AM VHF-422C (2X) (8.33KHZ UPGRADED)
INTER COMMUNICATION SYSTEM TEAM TB 31 WITH 3 CONTROL BOXES 1976 (1 IN CABIN)
PA WITH 4 LOUDSPEAKERS TEAM BA1920
THALES AHV-16 RADIO ALTIMETER
ATC TRANSPONDER GARMIN GTX-330 (MODE-S)
SAT COM LATTITUDE
VHF/FM MARITIME NAT NPX-138
CVR HONEYWELL 30B
ADF KING KDF-806
DME KING KDM-706A
VOR/ILS KING KNR-634A
AIR DATA COMPUTER
GPS MARCONI CMA3012
TELEPHONICS RDR1400 WEATHER/SEARCH RADAR
RADAR INTERFACE IU2023
JEPPESEN MAP SKYFORCE SKYMAP IIIC

CABIN
1 CABIN FLOOR CAPABLE OF THE VARIOUS OPTIONAL TYPES OF ARRANGEMENTS
2 REMOVABLE PILOT & CO-PILOT HIGH BACK-REST SEATS, ADJUSTABLE IN REACH & HEIGHT EACH FITTED WITH A SAFETY BELT & SHOULDER 4-POINT HARNESS SAR LAY-OUT
2 PILOT & CO-PILOT JETTISONABLE DOORS, EACH FITTED WITH A BAD WEATHER WINDOW & AN INTERNAL STORAGE UNIT.
2 HINGED JETTISONABLE CABIN FRONT DOORS
2 ENLARGED & BUBBLED REAR SLIDING DOORS WITH JETTISONABLE WINDOW FROM INSIDE & OUTSIDE
4 RETRACTABLE FOOTSTEPS
2 UPPER TINTED PANES
CABIN UPHOLSTERY WITH SOUND PROVING
1 INSTRUMENT PANEL, ONE CONSOLE & ONE CEILING PANEL
DUAL FLIGHT CONTROL
ENGINE CONTROLS
ROTOR BRAKE CONTROL
1 HEATING/DEMISTING/VENTILATION SYSTEM
2 WINDSHIELD WIPERS
2 ILLUMINATED CHART HOLDERS
2 HEADSET HOLDERS (SILEX)
1 PORTABLE FIRE-EXTINGUISHER

ADDITIONAL EQUIPMENT
DIRECTION FINDER CHELTON DF7 SYSTEM
DOPPLER INSTALLATION, RACAL D91
HELICOPTER EMERGENCY EGRESS LIGHTING (HEEL)
HR-SMITH CPI-503 ADELT
DUKANE DK120 ULB
AVAD RACAL V694 100FT, CH, UC WARNING
SAND FILTERS, FIXED PARTS
GOODRICH HOIST CLASS2 (272KG) FIXED PARTS
SPECTROLAB SX-5 SEARCH LIGHT
CARGO SLING WITH DYNAMOMETER & ELECTRICAL MIRROR (1600KG) FIXED PARTS
RN NAV2 + DOUPLER D91
DE-ICED WINSHIELD
FLIR EO/IR HARD POINTS
HEEL SYSTEM
UHF RADIO INSTALLATION
AIS TRANSPONDER INSTALLATION
SAR CABIN LAYOUT / CVR INSTALLATION

GENERAL
FUSELAGE COMPRISING THE CABIN & LUGGAGE HOLD
LUGGAGE HOLDS WITH FLOOR, TIE DOWN NET & ACCESS DOOR
TAIL BOOM WITH STABILIZER FITTED WITH 2X LATERAL FINS & 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 & CO-PILOTS STATION & PARKING BRAKE
BUILD IN FOOTSTEPS 2 ON EACH SIDE FOR ACCESS TO THE TRANSMISSION DECK
FIXED PARTS FOR MAIN ROTOR BLADE FOLDING
STRUCTURAL PROVISIONS FOR 1600KG CARGO SLING
STRUCTURAL REINFORCEMENTS FOR HOIST
JACKING, HOISTING, MOORING & GRIPPING POINTS