2018 Agusta AW139 

Description:

NEW AW139

12 passengers with comfort seats 

 

 

HELICOPTER CONFIGURATION

Airframe
– Aluminium alloy fuselage
– Acrylic windshields
– Overhead cockpit transparent windows
– Lower cockpit transparent 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 for increased load capacity (up to 300 kg)
– 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
– 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)
– Steps for cockpit access
– Anti-vibration masses (2) under cabin floor

 

Rotors and 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)

 

Power plant and 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 and hydraulic system
– Main transmission with two direct drive engine inputs
– 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)
– Three 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

 

Electrical system
– 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 (20-cell) main battery plus one 13 Ah auxiliary battery
– DC starter generator control units (2)
– Navigation lights (3)
– Anti-collision light
– External emergency landing lights on the sponsons (2)
– Retractable/rotating landing/taxing lights (2)
– Baggage compartment lights (3) and smoke sensor

 

Standard avionic package
– 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 MultiFunction 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 MultiFunction 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


- 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.


- 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


- One ADF


- 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/SBAS – Wide Area Augmentation System/Satellite Based Augmentation System) 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
– Pilot and co-pilot crashworthy seats (with inertial reels and 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
– Fluorescent 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 (LH side)
– Air ventilation system
– First aid kit

 

Painting
– Standard colour scheme from Company paint selection, solid colour

 

Miscellaneous/ground equipment
– Cargo net in baggage compartment for increased load capacity (up to 300 kg)
– 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)

 

 

Price

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