2004</span> Leonardo <span>AB139

2004 Leonardo AB139

S/N: 31010 | HB-ZGC

Total Hours
3477 hours since new

Engines

# TSN TSO
PCE-KB0073 2665 2665
PCE-KB0119 3018 3018

Highlights

  • One Owner Since New
  • Dual Pilot IFR Cockpit
  • 12 Passenger.Layout
  • 4-Axis DAFCS

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Details

AIRFRAME

  • Aluminum alloy fuselage
  • Acrylic Windshields
  • Overhead windows
  • Fresh air adjustable outlets
  • Forced fan ventilation (provision for)
  • Bleed air header and defroster with air noise suppression
  • Heated Pitot tubes w/ Pitot heat failure warning (2)
  • Heated static intakes (2)
  • Cargo tie-down fittings
  • Pilot cabin fire extinguisher
  • Pilot’s doors (2 for pilot’s cabin)
  • Plug-in sliding doors (2) for PAX cabin access with emergency exit windows on each door
  • Baggage compartment
  • Wheeled retractable tricycle Landing Gear (2 wheels on nose gear)
  • Mooring and jacking fittings
  • Tail-boom and vertical fin
  • Stabilizer

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

COMMUNICATION SYSTEM

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

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

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 VHF Comm - 1 Mode-C diversity transponder - 1 VOR/LOC/GS/MB - 1 ADF - 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

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

INTERIOR

  • 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
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