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