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AIRCRAFT DATA
Date of Manufacture: December 1998
Current Civil Registration Number: C- FHMQ
Total Time, Airframe: 4734 Hours as of April 15, 2017
Number and Type of Engines: Two (2)
Turbomeca Arriel 2S1, Turboshaft
ENGINE ON SBH
TTE(1): 3,431:25 Hours since new
TSO(1): 125 Hours since overhaul
NO. 2 ENGINE SERIAL NO.: 20719
TTE(2): 3,221:31 Hours since new
TSO(2): 125 Hours since overhaul
MAXIMUM GROSS WEIGHT: 11,700 POUNDS
Equipped Weight Empty / CG: 8201.0 Lbs. @ STA 206.1
Basic Mission Configuration: VVIP transportation, six cabin seats
ConFIGURATION FEATURES
Equipped with these standard features:
Two Turbomeca Arriel 2S1 turboshaft engines
Four blade fully articulated Main Rotor system with a high-visibility paint scheme
Bifilar vibration absorber (3P) at the Main Rotor Head
Four blade Tail Rotor system
Hinged cockpit doors for Pilot (right) and Copilot (left)
Hinged cabin doors, left and right, with key locks
Fully retractable tricycle landing gear with independent main wheel brakes
Pneumatic emergency landing gear extension system
Glass windshields with dual washers and wipers
Two integral fuel tanks with 281 U.S. Gallon total capacity; gravity filled
38 cubic foot baggage compartment with left and right doors aft of the main cabin
Dual pilot flight controls with redundant dual hydraulic servo systems
Dual Honeywell SPZ-7600 Digital Automatic Flight Control System
Dual 4-tube Electronic Flight Instrument System (Honeywell EDZ-756 EFIS)
Integrated Instrument Display System (Parker-Gull IIDS)
Attitude Heading Reference System (Litef AHRS)
Dual pilot instruments, dual Internal Communication System (ICS), and standby compass
Dual 28 Volt DC Electrical System with two 200 Amp Starter/Generators
AC Electrical system with Main Gearbox-driven 10-KVA generator and inverter
Exterior lighting including position lights, landing, and controllable search lights
Cabin and cockpit Bleed-air Heating system with fresh air ventilation