manufacturer
Airbus
configuration
Search and rescue
condition
Used
year
1997
time
9858
helicopter location
Netherlands
listing ID
HT9669
Description
Price reduced.....contact us to discuss
This 1997 AS365N3 comes with Goodrich Hoist Class 2 fixed parts (272kg), cargo sling with dynamometer, and two independent hydraulic systems feeding the servo-units, landing gear actuation system and assisted brakes.
avionics
AVIONICS
- 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
equipment
FLIGHT CONTROLS
- 1 MAIN ROTOR WITH 4 GLASS AND CARBON-FIBRE BLADES WITH STARFLEX HEAD FITTED WITH GUSTAND 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
ADDITIONAL EQUIPMENT
- 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
PROVISIONS
- 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
interior
CABIN
- 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
- 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
general characteristics
- AIRFRAME LANDINGS: 21,306
- 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
GENERAL
- 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
TRANSMISSION
- 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
HYDRAULICS
- 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
