2015 Agusta AW139
| Overview | |
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Well maintained, high price performance, immediately available Phase 7 |
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| Price: | Contact Seller |
| Offered By: | Individual |
| Registration: | B-70CF |
| S/N: | NA |
| Location: |
Malaysia
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| Days Active: | Today |
| Airframe | |
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Airframe-Aluminiumalloyfuselage-Acrylicwindshields-Overhead cockpit transparent windows -Lower cockpit transparent windows -Bleed air heater and defroster with air noise suppressions -Heated Pitot tubes (2) -Heated static intakes (2) -One cockpit and one passenger cabin fire extinguisher -Pilot doors (2) with push-out emergency exit window (with “storm window”on pilot side) -Plug-in sliding doors (2) for passenger cabin access with four locking latches -Passenger doors stop in fully open position -Six cabin push-out emergency exit windows (two on each passenger cabin door) -Baggage compartment with two lockable baggage compartment doors (LH and RH) -Baggage compartment cargo tie-down fittings for increased load capacity (up to 300 kg)-Wheeledretractabletricycle landing gear (two wheelson nose gearand brakes onmain 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 -Horizontal stabilizers with composite “winglets”-Pilot and co-pilot 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) (2) under cabin floor |
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| Total Time: | 981 Hours |
| Avionics | |
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navigation data -One Electronic Standby Instrument System (ESIS) (attitude, airspeed, altitude, vertical speed, compass, and ILS data) -TwoAttitude and Heading Reference Systems (AHRS) -TwoAir Data Modules (ADM) -Two flux valves -Two Display Controllers (DC) -Two Cursor Control Devices (CCD) -One Reversion Control Panel (RCP) -One Display Dimming Control Panel (DCP) -1st PFD (Pilot Primary Flight Display) 8" ×10" (external) colourActive Matrix Liquid Crystal Display as part of Honeywell Primus Epic System for visualization of flight and navigation data -2nd PFD (Co-pilot Primary Flight Display) 8" ×10" (external) colour Active Matrix Liquid Crystal Display as part of Honeywell Primus Epic System for visualization of flight and navigation data -1stMFD(PilotMultiFunctionDisplay) 8"×10"(external)colourActiveMatrixLiquidCrystal Display as part of Honeywell Primus Epic System for visualization of flight and navigation data -2nd MFD (Co-pilot MultiFunction Display) 8" ×10" (external) colour Active Matrix Liquid Crystal Display as part of Honeywell Primus Epic System for visualization of flight and -One StabilityAugmentation System (SAS) control panel -Two Remote Instrument Controllers (RIC) -Two Modular Avionic Units (MAU) incorporating the following major subsystems and/orfunctions: -One VHF Comm.-One VOR/LOC/GS/MB -Right Modular Radio Cabinet (MRC) with the following modules:-One VHF Comm.-One Mode S diversity transponder with Extended Squitter (ADS-B out 1090 MHz) -One VOR/LOC/GS/MB -OneADF -One DME -Two pedestal mounted Multifunction Control Display Units (MCDU) )-1st radar altimeter RT-300 -2nd radar altimeter RT-300 -Emergency Locator Transmitter (ELT) -One flight guidance controller -Two Honeywell GPS modules (WAAS -Vehicle Monitoring System (VMS) dual -Monitor Warning System (MWS) dual -Aural Warning Generator (AWG) single -Central Maintenance Computer (CMC) single -4-axis dual DigitalAutomatic Flight Control System (DAFCS) Basic-Provision for CVR/FDR data interface (single) -Flight Director System (dual) -Pilot and co-pilot headsets -Pilot and co-pilot interphone control (cyclic grip and floor switches) -Left Modular Radio Cabinet (MRC) with the following modules: |
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| Additional Equipment | |
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–the 5th display–132USG Auxiliary fuel –Increase the gross weight to 6,800kg–Cockpit tinted upper window –Approach plates chart holders with lights for pilot/co-pilot–Enhanced Ground Proximity Warning System (EGPWS)–TCAS I KTA-970 Honeywell Bendix/King TACAS I KTA-970 –Moving Map EuroavionicsEuroNav V–Weather radar Primus 660 Honeywell –Emergency floats provisi |
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| Engines | |
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-Two Pratt & Whitney Canada PT6C-67C turbo-shaft engines -Two integrated and independent engine oil coolers -Separation firewall protection for each engine -Fire detection system -Fire extinguisher system (2 bottles) -Steel engine exhausts and ejectors -Two independent crashworthy fuel cells -Two independent FADEC systems with auto-start and engine control functions for normal, emergency and training operations -Two magnetic chip detectors -Three main transmission chip detectors/debris collectors with burning capability -Two freewheel units -Four strut rods for upper deck attachment and one anti-torque plate -Intermediate gearbox with sight gauge and magnetic drain plug/chip detector -Tail gearbox with sight gauge and magnetic drain plug/chip detector -Dual independent, redundant hydraulic systems -Two hydraulic Power Control Modules (PCM) -One electrical pump for control checks on ground (engines off) -Air conditioning compressor quill -Two fuel filter assemblies -Two engine back-up controls, mechanical and electrical -Two manual engine start and ignition systems -Transmission drive system and hydraulic system -Main transmission with two direct drive engine inputs -Three main transmission driven hydraulic mechanical pumps for controls, landing gear andwheel brake actuation -Two supply pumps on engines -Two submerged booster pumps in fuel tank |
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| Engine Hours: | 981 SNEW |
| Interior & Exterior | |
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Pilot and co-pilot crashworthy seats (with inertial reels and safety belts) -28 V DC cockpit/cabin power outlet -Overhead cockpit windows sun shades -Cockpit map and data case in central console -Two flash lights for pilot and co-pilot -Map and data cases in pilot and co-pilot doors -ICS panel with plug for one headset (LH side) -Air ventilation system -First aid kit -Cockpit utility lights (2) -Fluorescent emergency exit signs |
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| Year Interior: | 2015 |
| Metallic colours from Company selection, customized painting scheme, | |
| Year Painted: | 2015 |
| Other Info | |
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Inspection Status: Strictly per the working manuals |
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| Damage: | No known current or historical damage |
