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

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

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

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

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