AW 169 Commercial in Confidence AW 169 VIP CONFIGURATION Airframe Transmission Drive System and Hydraulic System Electrical Systems

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1 AW 169 VIP Year of Manufacture 2017 Airframe Total Time Brand new Configuration VIP Engines PW210A Availability July 2017 LHD Warranty 3 years / 2000 hours CONFIGURATION Airframe Airframe structure including nose radome, cockpit, manin cabin with flat floor and baggage compartment, tail boom, vertical fin, horizontal stabilizers, fuel tank housing Attachments for main gearbox and engines Upper deck cowlings Landing gear attachments Heated pilot tubes (2) Forced fan ventilation Bleed air heater and defroster with air noise supression Cockpit air adjustable outlets Cockpit instrument panel, overhead panel and interseat console Cockpit Windshields Pilot and co- pilot windshield wipers Overhead cockpit windows Lower cockpit windows Pilot doors with emergency exit windows and storm window onpilot side. Lower pilot/co- pilot doors windows Plug in sliding doors (2) for passengers cabin access with four emergency exit windows Baggage compartment (one door- access from left hand side) Baggage compartment cargo tie- down fitting Lockable baggage compartment doors Landing Gear Wheeled fixed tricyle landing gear with two wheels on nose gear, one wheel with brakes on main landing gears and mooring rinhgs. Rotor and Controls Main rotor system with composite blades Tail rotor system with composite blades Rotating M/R and T/R flight controls Pilot fixed flight controls Copilot fixed flight controls Force trim system Four parallel actuators (4-axis autopilot) Power plant and fuel system Two pratt & whitney Canada 210A turboshaft engines APU mode on left hand side engine Two anti-icing fuel systems and two magnetic chip detectors Engines control panel Engine bay group Fire detection system Fire extinguisher system Fire detection and extinguisher control panel Crashworthy fuel cells Filler port for gravity refuelling (on left hand side) Fuel quantity gauging system Transmission Drive System and Hydraulic System Main transmission gearbox with two direct drive engine inputs, lubrication system with oil ducts integrated in the casing and oul cooling system. Three main transmission chip detectors/debris collectors with burning capability Intermediate gearbox with sight gauge and magnetic drain plug/chip detector with burning capability Tail gearbox with sight gauge and magnetic drain plug/chip detector with burning capability Dual independent, redundant hydraulic system Two main transmission driven hydraulic mechanical pumps for controls and wheel brake actuation Two hydraulic power control modules (PCMs) Three main rotor dual servo actuator One T/R actuator shut off valve Electrical Systems DC primary power generation system: 28 V DC provided by two independent 300 A stater generators One heavy duty battery (33AH) One auxiliary battery (13AH) 28 V DC external power receptacle DC power distribution system (including bus bars, circuit breaker panels and controls). Lighting System Internal lighting - Instrument cockpity panel lighting - Inter sear cockpit console lighting - Overhead cockpit console lighting - Cockpit dome light (1),(2),(3) - Baggage compartment light External Lighting - Anti collision light (1) - Navigation lights (red,white,green) - Retractable swivelling landing/taxiing lights (2) - External emergency lights (2) - External lights night vision goggles friendly. Standard Avionics Package Cockpit display system (CDS) One integrated standby instrument system (ISIS) Two display control panels Two cursor control devices One reversionary contorl panel One display dimming panel Two master caution lights Two master warning lights Two avionics full duplex ethernet switches Aircraft monitioring & management system Four axis automatic flight control system Radio comm and navigation system 1

2 Interphone Communication system Primary flight instruments Interior Cockpit compartment utility finishing interior Cockpit panel sun0glare shields Pilot/Co- pilot crashworthy adjustable seats 28V DC/10A cockpit/cabin utility power socket Baggage compartment utility finishing interior rear tail separation Baggage smoke sensor Pilot/Co- pilot headsets Painting Standard colour scheme from company paint selection, solid colours. Optional Equipment Steps for cockpit/ cabin access Rotor brake system Second radar altimeter One solid state cockpit and voice flight data recorder with ULB One emegency locator transmitter (ELT- 3 Frequencies) (fixed) Overhead cockpit windows sun shadesfirst aid kit One cockpit and one one cabin fire extinguisher USB interseat console socket Additional Navigation and Fleet Management System ADS- B out Health usage monitoring system Flight data monitoring system Helicopter terrain avoidance and warning system Synthetic vision system Miscellaneous / Ground equipment Extension headset Covers and flags for engines, pilot and connectors Manuals and parts catalogue Tie down assemblies for main rotor blades Tail rotor blades flapping block (1) Main rotor blades sock pole (1) Main landing gear wheel chocks (2) Landing gear handle locking pin(1) Tow bar(1) Losse equipment bag(1) Baggage compartment cargo net Proposed Configuration Interior equipment - cabin Enviromental control system dual zone air conditioning Corporate interior Corporate layout silver Interior equipment - cockpit Approach plates chart holders with lights for pilot and co- pilot Co- pilot hinged window Tablet cradle for chart holders Windshield washing system Cockpitcabinet Pen, Pencil, torch holder Carpet for cockpit & cabin Second fire extinguisher in cockpit Leather boots on cyclic and collective Carpet on cockpit floor with metal scuff plates under pilot feet Avionics Equipment TCAS II rockwell collins TCAS provision TCAS II rockwell collins TCAS removable Moving map Weather radar rockwell collins RTA multiscan provision Weather radar roclwell collins RTA multiscan removable Utility Equipment Camera on the tail fin Emergency floats provision Engine air particle separators provision Engine air particle seprators romovable Hinged fuel cap Grab handles in cabin both sides Mission Equipment Increased gross weight (4800 KG MTOW) Enhanced vision system maxviz EVS Finishing Painting Customized painting scheme Main and tail rotor high visibility painting All engine cowls inside painted heat resistant white polyurethane Loose Equipment 2

3 CARPET AND CEILING 3

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5 PAINTING SCHEME AND FINAL DRAWING 5