2013 Agusta AW109SP
| Overview | |
| Weather Radar, 4 Cell Auxiliary Fuel Tank, Low Hours | |
| Price: | Contact Seller |
| Offered By: | Individual |
| Registration: | NA |
| S/N: | NA |
| Location: |
Thailand
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| Days Active: | Today |
| Airframe | |
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Aluminium alloy and bonded panel fuselage Jacking and hoisting points Semi-monocoque aluminium alloy tail boom Grounding points Three wheel retractable landing gear Two hinged jettisonable high crew doors (LH & RH) Quick opening hinged inspection doors to allow visual check of engine oil levels and maintenance inspection points Two passenger sliding doors (LH & RH), 1.40 m opening, with jettisonable windows Swivelling front wheel provided with tow bar attachment Acrylic windshield and side windows Removable fairing and cowlings,for complete accessibility to the controls and drive components Acrylic transparent overhead windows Separate baggage compartment with hinged door Quick removable tail rotor drive shaft cover |
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| Total Time: | 820 Hours |
| Landing Cycles: | 3,184 |
| Avionics | |
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Pilot flight/navigation EFIS (2 displays) with embedded FMS, Synthetic Vision (SVS), HTAWS (Helicopter Terrain Awareness and Warning System), slip indicator and Remote Bug Panel (RBP) (*)ln lieu of basic pilot flight/navigation EFIS(1 display) with slip indicator and remote bug panel(RBP) (*) In lieu of basic Pilot flight/navigation EFIS (1 display) with slip indicator and Remote Bug Panel (RBP) (**) Data services subscription for the update of the navigation databases from Jeppesen is under customer's responsibility. Co-pilot flight/navigation EFIS (2 displays) with embedded FMS, Synthetic Vision (SVS), HTAWS (Helicopter Terrain Awareness and Warning System), slip indicator and Remote Bug Panel (RBP) Dual controls ELT C406-N HM Artex (with Navigation Interface Module embedded) Second magnetic compass indicator Reversionary Control Panel (RCP) EFIS pilot/co-pilot navigation synchronization switch (FMS data) Second electronic clock Second Radio Management System (RMS) RTU-4210 Collins Electronic Standby Instrument System (ESIS) Second VHF/AM VHF-4000E Collins DME DME-4000 Collins Second Attitude Heading Reference System (AHRS) Second Air Data Unit (ADU) |
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| Additional Equipment | |
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Airframe hourmeter (*) It may be affected by avionic customization. Engine compartment fire extinguishers (Qty 2) Reinforced windshields Rotor brake Fuel cap with key-lock Windshield wipers (pilot and co-pilot) with wiper switch on cyclic grips Pulsed chip detectors (in lieu of quick disconnecting chip detectors) Baggage compartment extension (1.9 m) Retractable/rotating landing light (nose mounted) |
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| Engines | |
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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. Cyclic and collective controls powered by two hydraulic systems Adjustable directional control pedals Power plant and fuel system Two Pratt & Whitney Canada PW207C turbo-shaft engines Force trim and artificial feel system Engine control panel emergency and training operation modes and auto-start Hydraulically powered anti torque system Engine mounted fuel pump and filter assembly Adjustable friction devices on cyclic and collective system Steel metal tail rotor hub, corrosion protected, semi-rigid delta hinged type, with two composite blades, individually interchangeable Engine mounted oil pump and filter assembly Engine mounted fuel control and governor Two independent Full Authority Digital Electronic Control (FADEC) with normal Lubrication and cooling system Engine oil chip detectors (2) Dynamic flapping stop mechanism Two independent fuel system with cross-feeding valvecontrol panel Airframe mounted easy access fuel filter 3-cell crash-resistant fuel system (5751 —152 USgal) Submerged fuel boost pump (2) RH refuelling point Ground fuel drains |
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| Engine 1 Hours: | 820 SNEW |
| Engine 2 Hours: | 820 SNEW |
| Interior & Exterior | |
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Crash-resistant pilot seat, fore and aft adjustable, with lap belts and headrests Ventilation ram air inlets Aluminium alloy honeycomb reinforced floor with anti skid finish Exterior finishing Anti reflection instrument panel |
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| Year Interior: | 2013 |
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Primer exterior painting Finishing in accordance with manufacturer specification NTA 893 A |
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| Year Painted: | 2013 |
| Other Info | |
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Inspection Status: Strictly Per the Working Manuals |
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| Damage: | No known current or historical damage |
