A109E. Highlights. General Overview A109E COMMERCIAL IN CONFIDENCE. The A109E is a twin-engine helicopter

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1 A109E The A109E is a twin-engine helicopter Year of Manufacture 2006 Mission Configuration VIP Engine Type 2x PW206C Availability Immediate Registration EASA Highlights UK Royal fleet Fixed part Cargo hook, Hoist, Search light 221 USG Aux tank Fresh 3,200 hours inspection LHD warranty 3 months/250 hours Training, 1 pilot and 1 technician Crew/Passenger Seats Airframe TT General Overview 2 crew/6 passengers 3,153 hours/6,106 landings 1

2 Overhaul Timetable Designation TBO/SLL REM Cal Airframe Main Servo 1,800 Hours Main Servo 1,800 Hours Main Servo 1,800 Hours Transmission Assy 4,800 Hours 1, Gearbox 3,000 Hours 1,442 - Tail Rotor Hub 3,000 Hours 2,798 - Starter Generator 1 1,000 Hours Starter Generator 1 1,000 Hours Engine 1 TSN: 2900 Hours Reduction Gearbox 3,500 Hours Turbomodule 3,500 Hours Engine 2 TSN: 3154 Hours Reduction Gearbox 3,500 Hours Turbomodule 3,500 Hours 346-2

3 Basic and Optional Equipment Avionics Single Pilot IFR (EASA/FAA) avionic package (King Additional Avionic Equipment silver crown line) AC system (2 inverters) Co-pilot flight/ navigation instruments 1 ADF KR-87 King (including LCD EADI & EHSI, barometric AFCS 3 Axis Duplex SP-711 Honeywell altimeter, airspeed indicator, VSI) DME KDM 706A King EFIS Pilot/Co-pilot on Command Switch Gyrocompass C14 A Honeywell E.L.T. C406-2 HM Artex ICS Pilot/Co-pilot AG-06-1U Flight Director FZ-702 Honeywell with auto Agusta/Gemelli trim Pilot navigation instruments (including LCD GPS 2101 I/O Trimble interfaced with EFIS EADI & EHSI, standby ADI) and B-RNAV function Marker Beacon KMR 675 King Moving Map KMD 540 Bendix/King Transponder (mode S) KT-73 Bendix/King Radio altimeter AA-300 Honeywell Vertical gyros (No.1) Flightline TAS (Traffic Collision Avoidance System ) Vertical gyros (No.1) Flightline SkyWatch 497 BF Goodrich Vertical gyros (No.2) VG 208 Jet Electronics Weather Radar RDR 2000 Bendix-King 2 VHF/COM/NAV KX-165 Bendix/King Moving Map KMD 540 Bendix/King Flight instruments pilot Air speed indicator Instantaneous vertical speed indicator Barometric encoding altimeter Magnetic compass indicator Instrumentation (on IDS displays) Dual gas generator speed (N1%) Dual turbine outlet temperature (TOT C) Dual torque meter (TRQ%) Dual power turbine speed (N2%) Rotor speed (NR%) Transmission oil temperature ( C) and pressure (PSI) Two engine oil temperature ( C) and pressure (PSI) Two fuel pressure (PSI) Two fuel quantity (kg) Two engine fuel flow (kg/hr) Two flight controls hydraulic system pressure (PSI) Two utility hydraulic system pressure (PSI) Outside air temperature ( C) Dual DC ammeter Dual DC voltmeter Dual AC voltmeter 3

4 Airframe Equipment Electrical Aluminium alloy and bonded panel fuselage 27 Ah, 24 volt DC nickel cadmium battery Semi-monocoque aluminium alloy tail boom with temperature probe Two hinged jettisonable high crew doors (LH 160 Ampere self-cooled starter generators & RH) (2) Two passenger sliding doors (LH & RH) with Voltage regulators (2) jettisonable window Battery relay Acrylic windshield and side windows Interconnecting bus relay (2) Acrylic overhead windows External power relay Removable fiberglass tail rotor gearbox Distribution buses (1 battery, 2 essential, 2 fairing main) Quick removable tail rotor drive shaft cover External power receptacle Three-wheel retractable landing gear Position lights Interchangeable landing gear tires Anti-collision lights (2) Separate baggage compartment with Taxing lights (2) and landing lights (2) on hinged door landing gear sponsons Three jacking points Utility cockpit lights (2) Removable fairing and cowlings providing complete accessibility to the controls and drive components Swiveling front wheel provided with tow bar attachment Quick opening hinged inspection doors to allow visual check of engine oil levels and maintenance inspection points Instrument lights with dimming switch Radio master switch Caution and warning advisory Master warning lights (MWL) Master caution lights (MCL) Grounding point Warning, caution & advisory messages (on Rotors and controls Titanium metal main rotor hub, corrosion protected, fully articulated with four composite grips, four elastomeric bearings, four individually interchangeable composite blades, swept tips, and dampers Steel metal tail rotor hub, corrosion protected, delta hinged type, semi rigid, with two composite blades individually interchangeable Dynamic flapping stop mechanism Cyclic and collective controls powered by two hydraulic systems Hydraulically powered anti torque system Adjustable friction devices on cyclic and collective system IDS displays) Engine fire detection system with remote fire warning lights Standard Equipment Active Noise Reduction (ANR) headsets (pilot and co-pilot) Baggage compartment lights Crew open door actuators First aid kit Fuel drain electrical valves Shoulder harness with inertial reels (pilot and co-pilot) Internal structural provisions for utility equipment (cargo hook, rescue hoist, search light, AFCS) Portable fire extinguisher Portable fire extinguisher Force trim and artificial feel system Portable fire extinguisher Adjustable directional control pedals Tail boom strake 4

5 Additional equipment Equipment Optional equipment 1 retractable landing light 450 W Increased internal gross weight (3 tons Airframe hour meter MTOW) Baggage compartment extension (2.3 m) Central single drawer Dual Control Foldable central armrest on passenger seats Engine compartment fire extinguishers with see-through modification Fuel cap with key-lock Emergency floats provision Pulsed chip detectors 221 USG fuel system (in lieu of 160 USG) Radio master switch with ground function Passenger ANR headsets 6 pairs Windshield wipers (pilot/co-pilot) with wiper Customized painting scheme 2-3 metallic switch on cyclic grips colours from painting Company selection Rotor brake 2 Sliding door VLE & VLO Extension up to 140 KIAS Interior Exterior Reclined rear cabin bulkhead Primer exterior painting Two individual pilot seats, fore and aft Finishing in accordance with manufacturer adjustable, with lap belts specification NTA 893 A Aluminium alloy honeycomb reinforced floor with anti-skid finish Ventilation ram air inlets Anti-reflection instrument panel Air conditioning Garret ECU Primer finished cabin walls Vibration dampers installation VIP interior 6 places Soundproofing Paulstra Leatherette covered liners Seats covered with leather 3 aft facing seats ( central bench) 3 fwd facing seats (aft bench) Blue leather VVIP seating for 6 with blue carpets and white contrasting trim 3 points shoulder harness with inertia reels and safety belts for all passenger seats Coordinated VIP pilot/ co-pilot seats with headrest Pilot multipurpose holder Pilot console tray Reading light Advisory light Floor courtesy light Carpeting protection Leather bellows on flight controls 5

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