1997 Airbus/Eurocopter AS 365N-3 for sale, Netherlands

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

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

Yellow

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

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
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

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