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
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
