2009 EUROCOPTER AS365N 3

2009

EUROCOPTER

AS365N-3

Used

Price Reduced....contact us to discuss LOCATION BELGIUM AIRFRAME HOURS 4,325 AIRFRAME CYCLES 9,110 CONFIGURATION OIL & GAS

4325

AIRFRAME HOURS 4,325 AIRFRAME CYCLES 9,110 CONFIGURATION OIL & GAS

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

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 CLASS1 (272KG) FIXED PARTS CARGO SLING WITH DYNAMOMETER AND ELECTRICAL MIRROR (1600KG) FIXED PARTS

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 AA20-431 THALES AHV-16 RADIO ALTIMETER ATC TRANSPONDER MST67A (MODE-S) 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

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 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 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 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

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

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 1 FIRST-AID KIT EU-OPS COMPLIANT

Yes