2006 AIRBUS AS365N3

2006

AIRBUS

AS365N3

Used

Price Reduced only Euro2.0m Airframe PBH included TIME SINCE NEW 5,042 LANDINGS SINCE NEW 11,612 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. BUILT 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.

5042

Landings Since New 11,612

Component Times Item Retirement or OH Hours Remaining Hours Remaining % Remaining % Remaining MRB’s 20,000 14,919 75% MGB 3,000 968 32% Starflex 5,000 4,173 83% TGB 3,000 2,416 80% 2 x Arriel 2C No 1 No 2 No 1 No 2 TTSN 9,374 10,715 Engine MO3 3,500 3,007 2,633 86% 75% Engine MO3 Calendar 15 years 13.5 years 13 years 90% 87% Component Times Item Retirement or OH Hours Remaining Hours Remaining % Remaining % Remaining MRB’s 20,000 14,919 75% MGB 3,000 968 32% Starflex 5,000 4,173 83% TGB 3,000 2,416 80% 2 x Arriel 2C No 1 No 2 No 1 No 2 TTSN 9,374 10,715 Engine MO3 3,500 3,007 2,633 86% 75% Engine MO3 Calendar 15 years 13.5 years 13 years 90% 87% 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: 24396 RIGHT 72: R/H: 24057

VHF-AM ROCKWELL COLLINS VHF-422C (2X). INTER COMMUNICATION SYSTEM TEAM TB 31 WITH 3 CONTROL BOXES 1976 (1 IN CABIN.) PA WITH 4 LOUDSPEAKERS BAKER M1050. HEADSETS SILEC 4449-1 (2X). THALES AHV-16 RADIO ALTIMETER. ATC TRANSPONDER MST67A (MODE-S). HF/SSB BENDIX KING KHF950. VHF/FM MARITIME NAT NPX-138. SSCVFDR HONEYWELL AR COMBI. TCAS GOODRICH HP899. TCAS RYAN TAS600. ADF HONEYWELL KDF-806. DME HONEYWELL KDM 706A. VOR/ILS HONEYWELL KNR-634A (2X). AIR DATA COMPUTER SHADIN ADC-2000. FLIGHT MANAGEMENT SYSTEM UNIVERSAL UNS-1K (INCLUDING GPS). SFIM CDV 85 D3 FLIGHT DIRECTOR COUPLER. TELEPHONICS RDR1400 WEATHER/SEARCH RADAR. UMS. HUMS FULL (M’ARMS). JEPPENSEN MAP HONEYWELL KMD850. JEPPENSEN MAP SKYFORCE SKYMAP IIIC. 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.

EMERGENCY FLOATATION WITH AFDS. INTERNAL AERAZUR (SR-8) LIFE RAFT INSTALLATION. HELICOPTER EMERGENCY EGRESS LIGHTING (HEEL). HR-SMITH CPI-503 ADELT. DUKANE DK120 ULB. AVAD RACAL V694 100FT, CH, UC WARNING. ELT KANNAD 406AF. 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. 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.

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. FIRST-AID KIT JAR-OPS COMPLIANT.