2018 Agusta AW139 for sale, China

Price: USD $11,499,000
Asia, China
Year
2018
S/N
31793
Reg
-
TT
19

Aircraft Description

Aircraft like new.

Always Hangered.

Very Few Hours – Only test flight hour and daily maintenance engine run.

Oil & Gas Offshore Mission Qualified.

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AIRFRAME / ENGINES / APU / WEIGHT / TOTAL LANDING

AIRFRAME

MTOW: 7,000 kg
Fuel Capacity: 1,568 L
VNE: 310 km/h
Max Cruise Speed: 306 km/h
Max Operation Altitude: 6,096 m
Max Range: 1,061 km (with Aux Fuel Tank, No reserve)
Max Endurance: 5h13 min (with Aux Fuel Tank, No reserve)

ENGINES

Make: Pratt & Whitney Canada
Model: PT6C-67C
Serial: # 1: PCE-KB1997 # 2: PCE-KB2009
Times : # 1: 19 hrs # 2: 19 hrs
Cycles: # 1: 34 # 2: 34
  • AVIONICS & CONNECTIVITY
    • 1st PFD (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
    • 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
    • 1st MFD (Pilot Multi-Function Display) 8" × 10" (external) colour Active Matrix Liquid Crystal Display as part of Honeywell Primus Epic System for visualization of flight and navigation data
    • 2nd MFD (Co-pilot Multi-Function Display) 8" × 10" (external) colour Active Matrix Liquid Crystal Display as part of Honeywell Primus Epic System for visualization of flight and navigation data
    • One Electronic Standby Instrument System (ESIS) (attitude, airspeed, altitude, vertical speed, compass, and ILS data)
    • Two Attitude and Heading Reference Systems (AHRS)
    • Two Air 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)
    • One Stability Augmentation System (SAS) control panel
    • Two Remote Instrument Controllers (RIC)
    • " Two Modular Avionic Units (MAU) incorporating the following major subsystems and/or functions: - Vehicle Monitoring System (VMS) dual- Monitor Warning System (MWS) dual- Aural Warning Generator (AWG) single- Central Maintenance Computer (CMC) single- Provision for CVR/FDR data interface (single)"
    • 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:- One VHF Comm.- One VOR/LOC/GS/MB"
    • " Right Modular Radio Cabinet (MRC) with the following modules:- One VHF Comm.- One VOR/LOC/GS/MB- One ADF- One DME"
    • Two pedestal mounted Multifunction Control Display Units (MCDU)
    • Emergency Locator Transmitter (ELT)
    One flight guidance controller
    • Pilot and co-pilot digital audio panels with remote ICS audio port for ground operation
    • Pilot clock (digital)
    • Co-pilot clock (digital)
    • One magnetic compass
    • One outside air temperature indicator
    • Two Master Warning Lights (MWL)
    • Two Master Caution Lights (MCL)
    • Engine 1 fire light
    • Engine 2 fire light
    • Baggage compartment smoke detector light
    • Dual electrical power connection for CVR/FDR (FAA requirement compliant)
    • 1st radar altimeter RT-300
    • 2nd radar altimeter RT-300
    • 4-axis dual digital automatic flight control system(DAFCS) Basic incorporated into Modular Avionics Units(MAUs)
    • Flight Director System (Dual) incorporated into the Modular Avionics Unites(MAU)
    • Two Honeywell GPS modules with Flight Plan Management System(FPMS)
    • One Model S diversity transponder with Extended Squitter (ADSB-Out 1090MHz) incorporated into the Modular Radio Cabinet(MRC)
    • Cockpit Voice Recorder & Flight Data Recorder (CVR/FDR) with Underwater Locator Beacon (ULB)
    • Health & Usage Monitoring System (HUMS)
    • Enhanced Ground Proximity Warning System(EGWPS) Provision
    • Enhanced Ground Proximity Warning System(EGWPS) removable
    • ADELT (2-frequency Automatic Deployable ELT w/ GPS interface) (*) In lieu of standard ELT
    • TCAS I KTA-970 Honeywell Bendix/King provision
    • TCAS I KTA-970 Honeywell Bendix/King removable (*) Required for VFR night single pilot operations."
    • Weather Radar Primus 660 Honeywell provision
    • Weather Radar Primus 660 Honeywell removable
  • Interior & Entertainment
    Number of Passenger: 12 Pax seats / Single Stretcher
  • Additional Equipment & Information
    • Forced fan ventilation
    • Bleed air heater and defrosters with air noise suppressions
    • Cockpit air ventilation system
    • Baggage compartment cargo tie-down for increased load capacity(up to 300KG)
    • Rotor brake
    • Air conditioning system
    • Emergency floats provision
    • Emergency floats removable
    • Life rafts up to 14 passengers each provision (Qty 2)
    • Life rafts up to 14 passengers each removable (Qty 2)
    • Auxiliary transversal fuel tank 132 USgal provision
    • Auxiliary transversal fuel tank 132 USgal removable
    • External louderspeakers(400W) Provision
    • External louderspeakers(400W)removable
    • "Rescue hoist (Goodrich) provision - single type(*) Including ICS AV900 Honeywell, wireless ICS Polycon and swivelling light for rescue hoist (belly mounted)"
    • Rescue hoist (Goodrich) removable - single type
    • Maritime protection
    • Aerolite single stretcher(installed transversally)

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