Agusta AW139

Aircraft Information

Serial Number: 
Registration Number: 
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Aircraft Description: 

Aircraft Highlights:
• Engines on ESP Gold Lite
• Avionics on Honeywell HAPP
• Camera on Tail Fin
• EVS-1500 MaxViz Enhanced Vision System
• Primus Epic Phase 7
• Auxiliary Transversal Fuel Tanks 132 Gallon
• Emergency Floats with Kevlar Covers
• 4 Axis DAFCS Enhanced with Hover Mode
• 48 Month Inspection Completed April 2017

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Aircraft Information sheet: 
Airframe Information

TTAF: 826

Landings: 2210

Aluminium alloy fuselage
Overhead cockpit trasparent windows
Lower cockpit trasparent windows
Cockpit ram air adjustable outlets
Forced fan ventilation
Bleed air heater and defroster with air noise suppressions
Heated Pitot tubes (2) with Pitot heat failure warning(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
Wheeled retractable tricycle landing gear (two wheels on nose gear and brakes on main 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
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)
Steps for cockpit access
Anti-vibration masses (2) under cabin floor

Engine(s) Information

Pratt & Whitney PT6C-67C

Engine 1: 826 Hours | Cycles 1083
Engine 2: 826 Hours | Cycles 1083

Rotors & Controls:
Fully articulated Main Rotor (M/R) with five composite blades, five elastomeric bearings and five hydraulic dampers
Rotating M/R flight controls
Main rotor hub beanie
Main dual servo actuators (3)
Fully articulated Tail Rotor (T/R) with four composite blades, four elastomeric bearings and four elastomeric dampers
Rotating T/R flight controls
One T/R dual servo actuator
Force trim system
Pilot fixed flight controls (cyclic, collective, anti-torque pedals)
Co-pilot fixed flight controls (cyclic, collective, anti-torque pedals)
Dual digital 3-axis linear actuators
Rotor brake
Provision for main rotor tracking (magnetic pick-up)

Powerplant & Fuel System:
Two Pratt & Whitney Canada PT6C-67C turbo-shaft engines
Two independent FADEC systems with auto-start and engine control functions for normal, emergency and training operations
Two magnetic chip detectors
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 supply pumps on engines
Two submerged booster pumps in fuel tank
Two fuel filter assemblies
Two engine back-up controls, mechanical and electrical
Two manual engine start and ignition systems

Transmission Drive System & Hydraulic System:
Main transmission with two direct drive engine inputs
3 main transmission chip detectors/debris collectors with burning capability
2 freewheel units
4 strut rods for upper deck attachment and one anti-torque plate
Intermediate gearbox w/ sight gauge & 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)
3 main transmission driven hydraulic mechanical pumps for controls, landing gear and wheel brake actuation
One electrical pump for control checks on ground (engines off)
Air conditioning compressor quill

Avionics / Radios Information
Avionics / Radios: 

•1st PFD (Pilot Primary Flight Display 8" × 10" color Active Matrix LCD) as part of Honeywell Primus Epic System for visualization of flight and navigation data
•2nd PFD (Co-pilot Primary Flight Display 8" × 10" color Active Matrix LCD) as part of Honeywell Primus Epic System for visualization of flight and navigation data
•1st MFD (Pilot Multifunction Display 8" × 10" color Active Matrix LCD) as part of Honeywell Primus Epic System for visualization of flight and navigation data
•2nd MFD (Co-pilot Multifunction Display 8" × 10" color Active Matrix LCD) 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
•4-axis dual Digital Automatic 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:
•One VHF Comm.
•Right Modular Radio Cabinet (MRC) with the following modules:
•One VHF Comm.
•One Mode S diversity transponder
•One ADF
•One DME

Two pedestal mounted Multi Control Function Display Units (MCDU)
1st radar altimeter RT-300
2nd radar altimeter RT-300
Emergency Locator Transmitter (ELT)
One flight guidance controller
Honeywell GPS module with Flight Plan Management System (FPMS)
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)
Cockpit Voice Recorder & Flight Data Recorder (CVR/FDR) with Underwater Locator Beacon (ULB)

Interior / Exterior Information

FIVESTAR Cabin Interior (7 seats), including:

  • 3 armchairs leather covered-forward looking, middle one can be folded forward (with inertial reels and safety belt, sliding inflight direction, reclining backrest)
  • 1 Divan seat leather covered (with 4 safety belts and understorage compartment)
  • 1 leather covered armrest installed in the middle of Divan seat)
  • 2 lateral covered armrests cabinets with metal cupholder, ICS control and multipurpose holder installed on the divan seat)
  • 2 lateral covered armrests cabinets with metal cupholder, ICS control and multipurpose holder installed on 3 armchairs)
  • Multipurpose Cubby with 3 sliding doors
  • Night curtain cabin separator
  • Passenger cabin sliding doors with liners leather/leathered covered with PSU
  • Super Silent soundproofing
  • Nose landing gear doors
  • Customized VIP cabin finishing
  • Decoration trim
  • Standard passenger carpet in lieu of High thickness passenger carpet
  • Environmental Control System (with control panel in passenger cabin - IFEEL control panel on armrests)
  • P.A. (Passenger Address) system (including loudspeakers and safety belts lights)
  • ICS in the cabin for all passengers including two additional seats in the middle
  • Passenger cabin thermo acoustic double layer tinted windows
  • Ripple dampers
  • AVCS complete installation
  • MGB Premium grade
  • MVA
  • Cyclic and collective leather gators (same color as cabin interior)
  • 2 metal finished cabin vertical handles on doorposts
  • Alternate current power outlet (Qty 3)
  • Coat hooks (Qty 4)
  • One ICS phone located inside the rear left armrest cabinet in the cabin for communicating with pilots
  • 2 additional comfortable seats leather covered with safety belts

Interior Equipment:
Pilot and co-pilot crashworthy seats (w/ inertial reels & safety belts)
Cockpit dome/storm light
Cockpit utility lights (2)
28 V DC cockpit/cabin power outlet
Cockpit panel sun-glare shields
Overhead cockpit windows sun shades
Floor provisions for 15-seat configuration
Fluorescent lighted emergency exit signs
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
Air ventilation system
First aid kit

Additional Information
Additional Information: 

Customized painting scheme, metallic colors from Company selection
Pilot/co-pilot adjustable seats (4G) in lieu of standard seats
Sheep skin cover for pilot and co-pilot seats
Pilot and co-pilot Glass windshield
Approach plates chart holders with lights for pilot and co-pilot
4-axis DAFCS (Digital Automatic Flight Control System) Enhanced with Hover Mode (HOV)
Auxiliary heavy duty battery 27 Ah (in lieu of 13 Ah)
Enhanced Ground Proximity Warning System (EGPWS) provision/removable
TCAS I KTA-970 Honeywell Bendix/King provision/removable
Weather Radar Primus 660 Honeywell provision/installation
Emergency floats provision/removable
Emergency floats Kevlar covers
Auxiliary transversal fuel tanks 132 USgal provision/removable
Increased gross weight - 6.800 kg
Co-pilot hinged window (storm window)
Pilot and co-pilot headsets Bose ANR type (in lieu of standard headsets)
Pilot headset hooks (Qty 2)
GPS 2nd unit
EVS-1500 MaxViz (dual field of view and image processing)
Maritime Protection
Engine air particle separators provision
Camera on the tail fin
Primus Epic Phase 7

Electrically operated pax steps LH / RH

Covers and flags: engine exhaust pipes (2), engine air inlets (2) and Pitot tubes (2), battery connector warning flag (1)
Manuals: aircraft log, engines operations, flight and maintenance and overhaul, illustrated parts catalogue
Tie-down assemblies for main rotor blades (5)
Tail rotor blades flapping block (1)
Main rotor blades sock pole (1)
Main landing gear wheel chocks (2)
Main rotor balance and tracking chart, tail rotor balance chart
Nose landing gear centre pin (1) and landing gear handle locking pin (1)
Jacking dome assy (1)
Tow bar (1)
Loose equipment bag (1)

Electrical Systems:

  • DC primary power generation: 28 V DC regulated voltage provided by two independent 300 A starter generators
  • DC external power receptacle
  • Two nickel-cadmium batteries: one 44 Ah main battery/one 13 Ah aux
  • DC starter generator control units (2)
  • Navigation lights (3)
  • Anti-collision light
  • Emergency landing lights on the sponsons (2) and Fixed landing/taxing lights on the sponsons (2), Retractable/rotating landing light
  • Baggage compartment lights (3) and smoke sensor

Contact Information

1118 Laurelwood Drive
McLean, Virginia, United States - 22102
International Phone: +49 1766 255 5634
Ph: (888) 337-3439

Email Altus Aviation