2017 AGUSTA AW169

2017

AGUSTA

AW169

Used

• 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

PW210A

• 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 • Interphone Communication system • Primary flight instruments ADDITIONAL NAVIGATION AND FLEET MANAGEMENT SYSTEM • ADS-B out • Health usage monitoring system (HUMS) • Flight data monitoring system • Helicopter terrain avoidance and warning system • Synthetic vision system

• 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 LANDING GEAR • Wheeled fixed tricyle landing gear with two wheels on nose gear, one wheel with brakes on main landing gears and mooring rinhgs. 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. 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-1500

PAINTING • Standard colour scheme from company paint selection, solid colours. FINISHING - PAINTING • Customized painting scheme • Main and tail rotor high visibility painting • All engine cowls inside painted heat resistant white “polyurethane”

• Cockpit compartment utility finishing interior • Cockpit panel sun-glare shields • Pilot/Co-pilot crashworthy adjustable seats • 28V DC cockpit/cabin utility power socket • Baggage compartment utility finishing interior rear tail separation • Baggage smoke sensor • Pilot/Co-pilot headsets