2009 AS365 N3_2

2009 Eurocopter AS365 N3 Turbine Helicopter For Sale

Oil & Gas Configuration, Shadin ADC 2000 Air Data Computer, SATCOM, Sand Filters, Jacking, Hoisting, Mooring & Gripping Points.

Type:
Helicopter (Turbine)
Manufacturer:
Eurocopter
Model:
AS365 N3
Year:
2009
Serial Number:
Enquire
Reg. Number:
Enquire
Total Time:
4,325 Hours
Seats:
11
Price:
Price upon request

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Price:
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Aircraft Type:
Aircraft Model & Manufacturer:
Year:
2009
Total Time:
4325
Registration Number:
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Serial Number:
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Seats:
Aircraft Location:
Contact Name:
Stephen Green
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Description

AIRFRAME
HOURS 4,325
CYCLES 9,110
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: 24,264
RIGHT – 72 R/H: 24,596

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 & AN INDICATION OF LOW LEVELS
2 ENGINES LUBRICATION & OIL COOLING SYSTEMS
2 FIRE DETECTION & EXTINGUISHING SYSTEMS
2 ANTI-ICING AIR INTAKE GRIDS
2 PHASE ANGLE TORQUE METER SENSORS BUILT INTO THE ENGINES
2 ENGINES EXHAUST PIPES

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

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

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 & IN AZIMUTH
ALLOWING SEARCH LIGHT & HOIST LIGHT
1 CABIN POWER OUTLET (28VDC)
1 EMERGENCY BATTERY FOR AUTOMATIC LIGHTING OF THE DOME LIGHTS & SIGNS
UNDER FUSELAGE ANTI-COLLISION STROBE LIGHT

FLIGHT CONTROLS
1 MAIN ROTOR WITH 4 GLASS & 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 & COLLECTIVE PITCH CHANNELS) & 1
DUAL-CHAMBER/DUAL BODY REAR SERVO-UNIT (ON TAIL ROTOR PITCH CONTROL CHANNEL)
1 SFIM PA155D DUPLEX-TYPE AUTO PILOT

AVIONICS
VHF-AM ROCKWELL COLLINS
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 & TEMP 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
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 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 & 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)
1 LANDING GEAR POSITION SELECTOR & INDICATOR
1 AFCS CONTROL PANEL

CABIN
1 CABIN FLOOR CAPABLE OF THE VARIOUS OPTIONAL TYPES OF ARRANGEMENTS
2 REMOVABLE PILOT & CO-PILOT HIGH BACK-REST SEATS, ADJUSTABLE IN REACH & HEIGHTEACH FITTED WITH A SAFETY BELT & SHOULDER 4-POINT HARNESS
11 STANDARD SEAT LAYOUT
4 POINTS HARNESSES FOR 11 ST&ARD SEAT LAYOUTS
2 PILOT & CO-PILOT JETTISON ABLE DOORS, EACH FITTED WITH A BAD WEATHER WINDOW & AN INTERNAL STORAGE UNIT. DOORS WITH AIR INLETS
2 HINGED JETTISON ABLE CABIN FRONT DOORS
2 ENLARGED & BUBBLED REAR SLIDING DOORS WITH JETTISON ABLE WINDOW FROM INSIDE & OUTSIDE
2 RETRACTABLE FOOTSTEPS
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 UPPER TINTED PANES
2 FRONT PLEXIGLASS PANES
2 WINDSHIELD WIPERS
2 ILLUMINATED CHART HOLDERS
2 HEADSET HOLDERS
1 PORTABLE FIRE-EXTINGUISHER
1 FLIGHT MANUAL
1 FIRST-AID KIT EU-OPS COMPLIANT

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 CLASS2 (272KG) FIXED PARTS
CARGO SLING WITH DYNAMOMETER & ELECTRICAL MIRROR (1600KG) FIXED PARTS

GENERAL
FUSELAGE COMPRISING THE CABIN & LUGGAGE HOLD
LONG NOSE
LUGGAGE HOLD WITH FLOOR, TIE DOWN NET & ACCESS DOOR
TAIL BOOM WITH STABILIZER FITTED WITH 2X LATERAL FINS & 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 & CO-PILOTS STATION & 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 & GRIPPING POINTS