1991 EUROCOPTER AS365 SOLD

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 CEILIN