1997 EUROCOPTER AS365N 3

1997

EUROCOPTER

AS365N-3

Used

Price Reduced.....contact us to discuss LOCATION NETHERLANDS AIRFRAME HOURS 9,858 AIRFRAME LANDINGS 21,306 CONFIGURATION SAR SAND FILTERS, FIXED PARTS AUXILIARY FUEL TANK IN THE HOLD, FIXED PARTS GOODRICH HOIST CLASS2 (272KG) FIXED PARTS SPECTROLAB SX-5 SEARCH LIGHT CARGO SLING WITH DYNAMOMETER AND ELECTRICAL MIRROR (1600KG) FIXED PARTS 1 AIRBORNE KIT STOWING BAG

9858

LOCATION NETHERLANDS AIRFRAME HOURS 9,858 AIRFRAME LANDINGS 21,306 CONFIGURATION SAR

2 SAFRAN ARRIEL 2C TURBINE ENGINES PROVIDING EACH 729 KW (990CH – 977 SHP) SUPER CONTINGENCY RATING, F ULL AUTHORITY DIGITAL ENGINES CONTROL SYSTEM NUMBER 2 X SAFRAN ARRIEL 2C LEFT - 72 L/H: 24,045 RIGHT - 72 R/H: 49,005 1 FUEL SYSTEM INCLUDING 5 TANKS SPLIT INTO 2 GROUPS, WITH A TOTAL USABLE CAPACITY OF 1,135 LITRES, 4 IMMERSED BOOSTER PUMPS, 1 TRANSFER PUMP AND AN INDICATION OF LOW LEVELS. OPTIONAL A LONG-RANGE TANK CAN BE ADDED. 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

VHF-AM ROCKWELL COLLINS 422C (8.33 KHZ) (2X) INTER COMMUNICATION SYSTEM TEAM TB 31 WITH 3 CONTROL BOXES 1976 (1 IN CABIN) PA WITH 4 LOUDSPEAKERS BAKER M1050 THALES AHV-16 RADIO ALTIMETER ATC TRANSPONDER GARMIN GTX-330 (MODE-S) VHF/FM MARITIME NAT NPX-138 CVR HONEYWELL AR COMBI UHF HONEYWELL KTR-909 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 155 FLIGHT DIRECTOR COUPLER TELEPHONICS RDR1400 WEATHER/SEARCH RADAR JEPPENSEN MAP SKYFORCE SKYMAP IIIC 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 2 FUEL PRESSURE INDICATORS 1 MAIN GEARBOX OIL PRESSURE AND TEMP IND 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 COPILOT’S SIDE 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 ICING DETECTOR 1 LANDING GEAR POSITION SELECTOR AND INDICATOR 1 AFCS CONTROL PANEL

DIRECTION FINDER CHELTON DF935 HELICOPTER EMERGENCY EGRESS LIGHTING (HEEL) HR-SMITH CPI-503 ADELT DUKANE DK120 ULB SAAB R4 AIS SYSTEM ICE DETECTION KIT OGP RECOMMENDED EQUIPMENT IFR CERTIFIED AUTOPLIOT OR AFCS 2 PRIMARY TRANSCEIVERS WITH 1 VHF MINIMUM MODE C OR S TRANSPONDER ELT WITH TSO 126 GPS (IFR TSO) 1 ADF 2 VOR/ILS & 1 DME INSTANTANEOUS VERTICAL SPEED INDICATOR (IVSI) RADIO ALTIMETER WITH AUDIO/VISUAL ALERT WITH ANALOGUE DISPLAY WEATHER RADAR WITH COLOUR SCREEN (MIN. SCALE 2,5NM) PUBLIC ADDRESS/INTERCOM SYSTEM WIRELESS CVR - AS MANDATED BY CAA AIRFRAME/ENGINE VIBRATION MONITORING SYSTEM UPPER TORSO RESTRAINTS, ALL SEATS 1 FIRST-AID KITS 2 FIRE EXTINGUISHERS WITH PRESSURE GAUGES PREFERRED EMERGENCY EXIT LIGHTING SYSTEM AIRCRAFT FLOTATION EQUIPMENT EMERGENCY POP-OUT WINDOW SONAR TRANSMITTER (PINGER) AUTO-INFLATION OF FUSELAGE FLOATS HEATING FOR CABIN LITTER KIT, CARGO HOOK, HOIST

FUSELAGE COMPRISING THE CABIN AND LUGGAGE HOLD LUGGAGE HOLDS WITH FLOOR, TIE DOWN NET AND ACCESS DOOR TAIL BOOM WITH STABILIZER FITTED WITH 2X LATERAL FINS AND 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 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

SAR

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 HEIGHTEACH FITTED WITH A SAFETY BELT AND SHOULDER 4-POINT HARNESS SAR LAY-OUT 3 POINTS HARNESSES 2 PILOT AND CO-PILOT JETTISONABLE DOORS, EACH FITTED WITH A BAD WEATHER WINDOW AND AN INTERNAL STORAGE UNIT. DOORS WITH AIR INLETS 2 HINGED JETTISONABLE CABIN FRONT DOORS 2 ENLARGED AND BUBBLED REAR SLIDING DOORS WITH JETTISONABLE WINDOW FROM INSIDE AND OUTSIDE 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 FIRST-AID KIT JAR-OPS COMPLIANT

Yes