HB-ZUV - 2009 AGUSTA AW139

2009

AGUSTA

AW139

31236

HB-ZUV

Used

ROTORS AND CONTROLS: Fully articulated Main Rotor (MJR) with five composite blades, five elastomeric bearings and five hydraulic dampers Rotating MIR flight controls Main rotor hub beanie Three main dual servo actuators Fully articulated Tail Rotor (T/R) with foul' composite blades, four elastomeric bearings and foul' elastomeric dampers Rotating TIR flight controls One T/R dual servo actuator Force trim system Pilot fixed flight controls (cyclic, collective, anti-torque pedals) Copilot fixed flight controls (cyclic, collective, anti-torque pedals) Dual digital 3- axis linear actuators Rotor brake Provision for main rotor tracking (magnetic pick-up)

347.0

Aluminum alloy fuselage Polycarbonate Windshields Overhead cockpit windows Lower cockpit windows Cockpit ram air adjustable outlets Forced fan ventilation Bleed air heater and defroster with air noise suppressions Heated Pitot tubes (2) with Pitot heat failure warning (2) Heated static intakes (2) One cockpit and one pilot cabin fire extinguisher Pilot doors (2) with push-out emergency exit window (with "storm window" on pilot side) Plug in sliding doors (2) for passengers cabin access with foul' locking latches Six cabin push-out emergency exit windows (two on each passenger cabin door) Baggage compartment with 2 lockable baggage compartment doors, LH & RH side. Baggage compartment cargo tie-down fittings Wheeled retractable tricycIe landing gear (two wheels on nose gear and brakes on main landing gear) Structural provisions for nose landing gear doors Landing gear mooring Upper deck mooring provisions Hoisting and jacking fittings Tail boom and vertical fin Stabilizers with composite "winglets" Pilot and copilot windshield wipers Maintenance steps for access to upper deck on both sides Upper deck cowlings (one front forward sliding, two side opening for engine access) Steps for cockpit access Anti-vibration masses (2) under cabin floor

Fully articulated Main Rotor (MJR) with five composite blades, five elastomeric bearings and five hydraulic dampers Rotating MIR flight controls Main rotor hub beanie Three main dual servo actuators Fully articulated Tail Rotor (T/R) with foul' composite blades, four elastomeric bearings and foul' elastomeric dampers Rotating TIR flight controls One T/R dual servo actuator Force trim system Pilot fixed flight controls (cyclic, collective, anti-torque pedals) Copilot fixed flight controls (cyclic, collective, anti-torque pedals) Dual digital 3- axis linear actuators Rotor brake Provision for main rotor tracking (magnetic pick-up)

Engine Serial Numbers PCE-KB0495 & PCE-KB0479 Engine Flight Hours 347:08 Flight Hours (both engines) Engine Compr. Cycles LH 601 Cycles RH 498 Cycles

No Modifications made

1st PFD as part of Honeywell Primus Epic System for visualization of flight and navigation data 2nd PFD as part of Honeywell Primus Epic System for visualization of flight and navigation data 1st MFD as part of Honeywell Primus Epic System for visualization of flight and navigation data 2nd MFD as part of Honeywell Primus Epic System for visualization of flight and navigation data Two Attitude Heating Feference Systems Two Air Data Modules Two flux valves Two Cursor Control devices (For more Informations, please ask by e-mail)

(Ask by E-Mail)

Two colors polyurethane painting in accordance with AgustaWestland standard painting scheme

Cabin, cockpit and baggage compartment utility finishing interior Pilot/Copilot crashworthy seats with interial reels and safety belts Cockpit dome/storm lights Cockpit utility lights 28V DC Cockpit/cabin power outlet Cockpit panel sun glare shields Overhead cockpit windows sun sheads floor provisions for 15 seat configuration Fluorescent lighted emergency signs Cockpit map and data case in central console Two flash lights for pilot and copilot Map and data case in pilot and copilot doors First aid kid

50 FH Inspection 397 Flight Hours 100 FH Inspection 447 Flight Hours 150 FH Inspection 429 Flight Hours 300 FH Inspection 579 Flight Hours 600 FH Inspection 600 Flight Hours 1,200 FH Inspection 1,200 Flight Hours 1 Year Inspection 08. July 2012 2 Year Inspection 08. July 2013 4 Year Inspection 16. July 2013 300 FH / 1 Year Inspection 579 Flight Hours / 08. July 2012 Tailboom modification completed 08. July 2011