2004 Agusta AW139 for sale, Kyrgyzstan

SINGLE/DUAL PILOT IFR
-Electronic Standby Instrument System (ESIS) (attitude, airspeed, altitude, vertical speed, compass and ILS data)
-Second PFD (co-pilot display)
-Second Master Warning Light
-Second Master Caution Lights
-Co-pilot clock
-Dual control
-Second display controller
-Remote Instrument Controller
-Second cursor control device
-Left modular radio cabinet with following modules: - 1 VHF Comm - VOR/LOC/GS/MB
-Right modular radio cabinet with the following modules:
1. 1 VHF Comm - 1 Mode-C diversity transponder
2. 1 VOR/LOC/GS/MB
3. 1 ADF
4. 1 DME
-Emergency communication panel
-RMU – Radio Management Units
-Radio Altimeter (RT – 300)
-Cockpit digital audio panel with remote ICS audio port for ground operation
-PAX audio panel for 1 headset

FLIGHT/ENGINE INSTRUMENTATION
-PFD (Pilot Primary Flight Display 8 x 10 color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data
-MFD (Pilot Multifunction Display 8 x 10 color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data
-AHRS (Attitude and Heading Reference System)
-ADM (Air Data Module)
-Flux valve
-Display Controller
-Cursor Control Device
-Reversion Control Panel
-Display Dimming Control Panel
-Stability Augmentation System (SAS) Controller
-Modular Avionics Units (MAUs) - Vehicle Monitoring System – VMS (dual) - Monitor Warning System – MWS (dual) - Aural ---Warning Generator – AWG (single) - Central Maintenance Computer – CMC (single) - 4-axis Digital Automatic Flight Control System – DFACS (dual) with Autotrim function - Flight Data Acquisition Unit – FDAU (single)
-Clock (digital)
-Magnetic Compass
-Free air temperature indicator
-Master Warning Light (MWL)
-Master Caution Light (MCL)
-Engine 1 fire light
-Engine 2 fire light
-Baggage fire light

COMMUNICATION SYSTEM
-Microphone and headset (2)
-Interphone control (cyclic grip and floor switches) (2)
-Stand-alone VHF/AM radio equipment
-Intercommunication control panel
-Primus Epic HF 1050 long-range system

Standard cabin and cockpit liners with soundproofing
Pilot/Co-pilot crashworthy seats
12 padded crashworthy utility passenger seats
Windshield wipers
Steps for cabin access
Pilot steps for cockpit access

ADDITIONAL STANDARD EQUIPMENT
-Second radar altimeter system
-Flight plan management system (FPMS) and GPS module with MCDU
-Dual flight director system integrated with MAU
-Steps for passenger cabin access and cockpit access
-Rotor brake
-ELT
-Air conditioning and heating
-EAPS - Engine Air Particle Separator
-Slope Operation Envelope Extension to 10º
-Cargo hook and cargo camera provision
-Aux Fuel Tank

ROTORS & CONTROLS
-Fully-articulated main rotor with five composite blades, five elastomeric bearings and five hydraulic dampers
-Rotating main rotor flight controls
-Three main dual servo actuators
-Fully-articulated tail rotor with four composite blades, four elastomeric bearings and four elastomeric dampers
-Rotating tail rotor flight controls
-One tail rotor dual servo actuator
-Force trim system
-Pilot fixed flight controls (cyclic, collective, rudder)
-Co-pilot fixed flight controls (cyclic, collective, rudder – provisions for)
-Engine mechanical back-up control (2)
-Dual digital three-axis linear actuators (6)

ELECTRICAL SYSTEMS
-DC primary power generation: 28-volt DC regulated voltage provided by two independent 300-amp starter generators
-DC external power receptacle
-One nickel-cadmium battery 40 Ah plus one 13 Ah auxiliary battery
-DC starter generator control unit (2)
-Manual engine start and ignition system (2)
-Navigation lights
-Anti-collision lights
-Landing light/search light
-Utility lights
-Pilot cabin dome light
-PAX cabin lights (dome or reading lights according to interior configuration)
-Tritium-lighted emergency exit signs
-Seatbelt/no smoking signs
-Baggage compartment light & fire/smoke sensor
-AC static inverters system (provisions for)

TRANSMISSION / DRIVE SYSTEM & HYDRAULIC SYSTEM
-Main transmission with chip detectors/debris collectors with burning capability
-Four strut rods for upper deck attachment and anti-torque plate
-Intermediate gearbox (sight gage and magnetic drain plug/chip detector)
-Tail gearbox (sight gage and magnetic drain plug/chip detector)
-Two hydraulic power control modules (PCMs)
-Three hydraulic mechanical pumps for controls (2 independent sys) and one electrical pump for controls check on ground (engines off)
-Upper-deck cowlings
-Provisions for BCS compressor

POWER PLANT & FUEL SYSTEM
-Two Pratt & Whitney Canada PT6C-67C engines
-EEC (Electronic Engine Control)
-Overriding clutches
-Two magnetic chip detectors
-Two integrated and independent engine oil coolers
-Separate firewall protection for each engine
-Fire detecting system
-Cowlings
-Engine exhausts and ejectors
-Two independent crashworthy fuel cells
-Pumps on engines (2) and submerged in fuel tanks (2)
-Fuel filter assembly