ENGINE:

ENGINE MFG : PRATT & WHITNEY

ENGINE TYPE: PT6B-37A

ENGINE TTSN: 609.55

STANDARD CONFIGURATION (FAA / EASA VFR)

VFR AVIONIC PACKAGE :

ADF: BENDIX / KING KR-87

GYROCOMPASS: HONEYWELL C14A

ICS PILOT: AGUSTA / GEMELLI AG–06–1U

TRANSPONDER: BENDIX / KING KT-70

PILOT NAVIGATION INSTRUMENTS INCLUDING ADI & HSI

VHF–COM / GPS: 250XL GARMIN

VHF 2 COM / NAV: BENDIX / KING KX-165A

VHF–COM / GPS: 250XL GARMIN

ADDITIONAL AVIONIC EQUIPMENT :

AC POWER SUPPLY SYSTEM: 2 INVERTERS

AFCS 3-AXIS DUPLEX: HONEYWELL SP-711

RADAR ALTIMETER: HONEYWELL RT-300

GPS / MAP: GARMIN 795

INTERIOR AND COMFORT :

BLEED AIR HEATER

PRIMER FINISHED CABIN WALLS

TINTED PANELS

VIBRATION DAMPERS INSTALLATION

AIR CONDITIONING

VIP INTERIOR, LEATHER COVERING 6 PAX SEATS WITH ARMREST & 2 PILOTSEAT, LEATHERING

BAGGAGE COMPARTMENT EXTENSION (2.3m)

ADDITIONAL EQUIPMENT:

DUAL CONTROLS

ROTOR BRAKE

BIRD RESISTANT WINDSHIELD PILOT / CO-PILOT

WINDSHIELD WIPERS PILOT / CO-PILOT

27 AH BATTERY SAFT

230 US GALL . FUEL SYSTEM

RETRACTABLE 450 W LANDING LIGHT

SLIDING WINDOWS PILOT / CO-PILOT DOORS

DART STEPS ( SX / DX )

FUEL JET A1 CAPACITY 605L (159.8 USgal)

TOTAL CAPACITY WITH RIGHT SUPPLEMENTARY FUEL TANK 710L (187.5 US.Gal)

TOTAL CAPACITY WITH RIGHT AND LEFT SUPPLEMENTARY FUEL TANKS 870L (229.8 US.Gal).

MISCELLANEOUS :

AIR INTAKE / EXHAUST COVERS

GROUND TOOL KIT ( INCL. TOW BAR, GROUND WHEELS, LIFTING TOOL )

TIE DOWN FITTINGS

ROTORCRAFT FLIGHT MANUAL ( RFM ) TECHN. PUBLICATIONS

REMARKS:

NO KNOWN DAMAGE HISTORY

ALL MAINTENANCE BY AGUSTA SERVICE FACILITY