EMERGENCY FLOATATION WITH AFDS
EXTERNAL AERAZUR (SR-10) LIFE RAFT INSTALLATION, INCLUDING CABIN FOOTSTEPS
HELICOPTER EMERGENCY EGRESS LIGHTING (HEEL)
HR-SMITH CPI-503 ADELT
DUKANE DK120 ULB
AVAD RACAL V694 100FT, CH, UC WARNING
FRONT GLASS INSTEAD OF PLEXIGLASS
RETROFITS
SATCOM (COMMUNICATION AND TRACKING) (SKYROUTER)
SSQAR INSTALLATION
VHF/FM INSTALLATION (NPX-138)
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
POWER PLANT
1 FUEL SYSTEM INCL. 5 TANKS SPLIT INTO 2 GROUPS, WITH A TOTAL USABLE
CAPACITY OF 1135 LITRES, 4 IMMERSED BOOSTER PUMPS, 1 TRANSFER PUMP
AND AN INDICATION OF LOW LEVELS
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
TRANSMISSION SYSTEM
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
HYDRAULIC SYSTEM
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
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
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
12 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
1 PORTABLE FIRE-EXTINGUISHER
1 FLIGHT MANUAL
FIRST-AID KIT EU-OPS COMPLIANT
