2018 AGUSTA AW169

2018

AGUSTA

AW169

New

New Delivery - 2018 Agusta AW169 VIP Delivery delayed pending final specification of paint and any option changes. Can be delivered quickly as new helicopter delivery following this finalization. Aircraft Highlights: • Pilot (flight and ground) and Technician (maintenance) training provided by Seller • Silver 4+2+2 VIP Corporate layout • ADS-B Out • HUMS • FDM • HTAWS • SVS • MaxViz EVS-1500 • Increased Gross Weight- 4800kg MTOW Pilot Training – Flight and Ground: • Glass Cockpit and Automation Management (GLAM) for 5 students • AW169 VFR/IFR Type Rating for 5 students • AW169 Type Rating Instructor for 2 students Technician Training – Maintenance: • AW169 (PWC 210) Airframe Maintenance Type Training Course B1.3 - Theoretical Elements for 3 students • AW169 (PWC 210) Airframe Maintenance Type Training Course B1.3 - Practical Elements for 3 students • AW169 (PWC 210) Avionic Maintenance Type Training Course B1.3 - Theoretical Elements for 3 students • AW169 (PWC 210) Avionic Maintenance Type Training Course B1.3 - Practical Elements for 3 students

EASA and FAA IFR compliant BASELINE AIRCRAFT Airframe: • Airframe structure including nose radome, cockpit, main 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 • 2 heated Pitot tubes • Forced fan ventilation • Bleed air heater and defroster with air noise suppression • Cockpit air adjustable outlets • Cockpit instrument panel, overhead panel and interseat console • Cockpit windshields • Pilot and copilot windshield wipers • Overhead cockpit windows • Lower cockpit windows • Pilot doors with emergency exit windows and "storm window" on pilot side • Lower pilot/copilot doors windows • 2 plug in sliding doors for passengers’ cabin access with four emergency exit windows • Baggage compartment (left hand side door access) • Baggage compartment cargo tiedown fittings • Lockable baggage compartment doors Landing Gear: • Wheeled fixed tricycle landing gear with two wheels on nose gear, one wheel with brakes on main landing gears and mooring rings Rotors and Controls: • Main rotor system with composite blades • Tail rotor system with composite blades • Rotating M1R and T IR flight controls • Pilot fixed flight controls (cyclic, collective, anti-torque pedals) • Copilot fixed flight controls (cyclic, collective, anti-torque pedals) • Force trim system • Four parallel actuators (4-axis autopilot) • Main rotor hub beanie Power Plant and Fuel System: • 2 Pratt & Whitney Canada 210A turboshaft engines • APU mode on left hand side engine • 2 anti-icing fuel systems and two magnetic chip detectors (one per engine) • 2 independent dual-channel FADEC systems (one per engine) • Engines control panel • Engine bay group (engine mounts, firewalls, cowlings, drains, exhausts) • Fire detection system • Fire extinguisher system • 1 fire detection and extinguisher control panel • Crashworthy fuel cells • Filler port for gravity refueling (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 oil cooling system • 3 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 systems • 2 hydraulic power control modules • Two main transmission driven hydraulic mechanical pumps for controls and wheel brake actuation • Three main rotor dual servo actuators • One tail rotor dual servo actuator • One T/R actuator shut off valve Electrical Systems: • DC primary power generation system: 28V DC provided by two independent 300Ah starter generators • One heavy duty battery (33Ah) • One auxiliary battery (13Ah) • 28V DC external power receptacle • DC power distribution system (including bus bars, circuit breaker panels and controls) Lighting Systems: Internal Lighting • Instrument cockpit panel lighting • Interseat cockpit console lighting • Overhead cockpit console lighting • 1 cockpit dome light • 2 cockpit utility lights • 2 cockpit storm lights • Baggage compartment light External Lighting • 1 anti-collision light • Navigation lights (red, white, green) • 2 retractable swiveling Landing I taxiing lights • 2 external emergency lights • External lights (night vision goggles friendly) Additional Baseline Equipment: • Cockpit/cabin steps • Rotor brake system • 2nd RA • 1 solid state CVFDR w/UL • 1 fixed ELT - 3 frequencies • Cockpit sun shields • 28V DC/10Ah utility power socket • Separate baggage compartment • Baggage smoke detector • First aid kit (per JAR OPS 3) • 2 fire extinguishers (cabin & cockpit per JAR OPS 3) • Pilot/copilot headsets

• Two Pratt & Whitney 210A Turboshaft Engines

Retrofit After Delivery: • 2nd transponder • Fuel transfer pump • Retractable landing gear • Tail logo light • LED lighting for cabin step area • 2 USB 2.1 mAh outlets and 2 115V outlets in cabin • Cabin windows tinted • Tinted upper eyebrow cockpit windows • Tinted cockpit side windows

• 3 Rockwell Collins display units 10”x8” color AMLCD with LED backlight and NVIS compatibility: 2 PFD’s and 1 MFD • 1 integrated standby instrument system • 2 display control panels • 2 cursor control devices • 1 reversionary control panel • 1 display dimming panel • 2 master caution lights • 2 master warning lights • 2 avionics full duplex ethernet switches • Aircraft monitoring and management system: 2 aircraft monitoring and management computers; 1 data transfer device; 2 touchscreen control panels • 4 axis automatic flight control system: flight control computer; flight control system control panel • Radio comms and navigation system: 2 VHF-AM radios; 2 NAV (B|VOR/ILS/MB) receivers; 1 ADF; 1 DME; 1 transponder w/ESM (Mode S); 2 SBAS GNSS (GPS’s) • Interphone comms system: 2 audio control panels (pilot & copilot stations); 1 audio management unit interfacing external transceivers; 1 passenger intercom amplifier • Primary flight instruments: 2 flux valves; 2 ADAHRS; 1 RA; pilot & copilot clocks; 1 standby magnetic compass • Rockwell Collins TCAS II 4100 • Moving maps • Rockwell Collins RTA 4112 weather radar Additional Avionics: • Automatic Dependent Surveillance – Broadcast • Health and Usage Monitoring System • Flight Data Monitoring System • Helicopter Terrain Avoidance and Warning System • Synthetic Vision System

Ground Equipment: • Extension headset • Covers & flags for engines, pitot and connectors • Manuals and parts catalogues • Tiedown assemblies for main rotor blades • Tail rotor blades flapping block • Main rotor blades sock pole • Main landing gear wheel chocks • Landing gear handle locking pin • Tow bar • Loose equipment bag • Baggage compartment cargo net Cockpit Equipment: • Approach plates chart holders with lights for pilot and co-pilot (USB power outlet included) • Copilot hinged window (storm window) • Tablet cradle for chart holders (loose equipment) • Windshield washing system • Cockpit Cabinet (including 2 USB 2.1 mAh) • Pen, pencil, torch holder • Carpet for cockpit & cabin • Second Fire extinguisher in cockpit* *If not allowed by certification regulation, provide additional fire extinguisher and relative mounting bracket as loose equipment • Leather Boots on cyclic and collective pedals • Carpet on cockpit floor with metal scuff plates under pilots' feet Utility Equipment: • Camera on the tail fin • Emergency floats - provision • Engine air particle separators - provision • Engine air particle separators- removable (additional standard engine cowlings - loose equipment) • Hinged fuel cap • Grab handles in cabin both sides (to be verified compatibility with Silver interior) Loose Equipment: • Emergency floats - removable • Emergency floats rigid covers as per painting scheme • 3 spare cabin and spare cockpit carpets • Spare fabrics and materials to include 1 roll of each fabric, 3 hides of each color leather and 1 pint of leather dye for touch up of each color of leather • Spare internal lights to include 3 of each type light (reading, led strip, etc.) • 1 spare latch for each drawer • Full set of spare door seals • Tail blade covers • Horizontal stabilizer padded covers • Cabin protective seat covers (maintenance covers) • Cockpit protective seat covers (maintenance covers) • Center pedestal protective covers (maintenance covers) • Baggage compartment carpet or padding • Spare seat belts for all helicopters + belt extenders in matching materials • 11 iPad mini 3Gs

• Customized painting scheme (in lieu of Agusta Westland painting scheme) • Main and tail rotor high visibility painting • All engine cowls inside painted heat resistant white "polyurethane"

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• Corporate layout “Silver 4+2+2”: 6 comfortable VIP seats (18” fixed); 2 additional seats in the rear cabin bay; cabin carpet; 8 ANR headsets- charging when plugged in the helicopter; 4 point seat belts for passengers • Helicopter Comfort package: environmental control system dual zone- air conditioning; full active comfort enhancer VIP • Corporate Interior: extended cabin liners on cockpit side; passenger cabin ambient LED lights; PSU w/reading lights and ventilation outlets; emergency lights; emergency exit signs; passenger advisory lights (safety belt chimes); passenger addressing loudspeakers • Medium soundproofing • Read cabin windows- left and right • Inter-communication system for all passengers • Corporate cabin management system for ECS, ICS & lights management