2012 AGUSTA WESTLAND AW139 VIP + FIPS
EASA CERTIFIED ?TTSN UNDER 300 HOURS
AGUSTA AW139 VIP + FIPS 2012 MODEL
BASIC
AIRCRAFT
ROTORS AND CONTROLS
POWER PLANT AND FULL SYSTEM
TRAMSMISSION DRIVE SYSTEM ANDHYDRAULIC SYSTEM
ELECTRICAL SYSTEMS
STANDARD AVIONIC PACKAGE:
STANDARD AVIONIC PACKAGE (follow)
INTERIOR
MISCELLANEOUS / GROUND EQUIPMENT
SPECIFICATION as per Dec 2014
Airframe : TT : 272 Hrs T Cycles 587 No Damage history
Engines : Pratt & Whitney PT6C ?67C w/ FADEC Engines under P&W ESP
Optional Avionics / Radios and Other features :
SPECIFICATION Interior and optional equipments:
AIRCRAFT
- Aluminium alloy fuselage Acrylic windshields Overhead cockpit windows Lower
- Cockpit windows
- Forced fan ventilation
- Cockpit ram air adjustable outlets
- 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
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 mam rotor tracking (magnetic pick?up)
POWER PLANT AND FULL SYSTEM
- Two Pratt & Whitney Canada PT6C?67C turboshaft engine
- Two independent FADEC systems with autostart 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
TRAMSMISSION DRIVE SYSTEM ANDHYDRAULIC 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 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 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)
- Fixed landing/taxing lights on the sponsons (2) Retractable/rotating landing light
- Baggage compartment lights (3) and smoke sensor
STANDARD AVIONIC PACKAGE:
- 1st PF D ( Pilot Primary Flight Display 8" * 10" colour Active Matrix Liquid Crystal Display ) as part of Honey well Primus Epic System for visualization of flight and navigation data.
- 2nd PFD (Co?pilot Primary Flight Display 8" x 10" colour Active Matrix Liquid
- Crystal Display ) as part of Honey well Primus Epic System for visualization of flight and navigation data
- 1st M FD (Pilot Multi function Display 8" * 10" colour Active Matrix Liquid Crystal Display) as part of Honey well Primus Epic System for visualization of flight and navigation data
- 2nd MFD (Co?pilot Multi function Display 8" x 10" colour Active Matrix Liquid Crystal Display) as part of Honey well 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 (A HRS)
- 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 A vionic Unit s (MAU) in corporating the following major sub systems 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/ FR data interface (single)
- Flight Director System (dual) Pilot and co?pilot headsets
- Pilot and co?pilot in terphone control (cyclic grip and floor switches)
- Left Modular Radio Cabinet (M RC) with the following modules:
STANDARD AVIONIC PACKAGE (follow)
- One VHF Comm .
- One VOR/LOC/ GS /M B
- Right Modular Radio Cabinet (MRC) with the following modules:
- One VHF Comm .
- One Mode S diversity transponder
- One VOR/ LOC/ GS /M B
- One ADF
- One DME
- Two pedestal mounted Multi Control Function Display Units ( MCDU)
- 1st radaral timeter RT ?300
- 2nd radaral timeter RT ?300
- Emerg ency Locator Transmitter (ELT)
- One flight guidance controller
- Honey well GPS module with Flight Plan Management System (FPMS)
- Pilot and co?pilot digital audio panels with remote ICS audio port for ground peration
- 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 firelight
- Engine 2 firelight
- Baggage compartment smoke detector light
- Dual electrical power connection for CVR/ FDR (FAA requirement com pliant)
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
- 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
MISCELLANEOUS / GROUND EQUIPMENT
- Covers and flags: engine exhaust pipes (2),
- Engine air inlets (2)
- 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)
SPECIFICATION as per Dec 2014
Airframe : TT : 272 Hrs T Cycles 587 No Damage history
Engines : Pratt & Whitney PT6C ?67C w/ FADEC Engines under P&W ESP
Optional Avionics / Radios and Other features :
- TCAS I KTA?970 Honeywell Bendix/King
- Weather Radar Primus 660 Honeywell removable
- Auxiliary trasversal fuel tanks 132 USG removable
- Approach plates chart holders with lights for pilot and co?pilot
- Slump protection pads provision
- MTOW extension up to 6 800 kg
- Full icing protection system/combined accessory gear box
- Moving map Euronav V
- 5th cockpit display for Euronav V EGPWS Enhanced Vision System
- Wire Strike Protection System
- Auxiliary Heavy duty battery 27 Ah
- 10? monitor on the separation wall
- CD, DVD, MP3 player + USB connection to an hard disk into the cabby area
- SATCOM installed in the document box on the backward bulkhead
SPECIFICATION Interior and optional equipments:
- 3 armchairs leather covered (with inertial reels and safety belts)
- 4 comfortable seats leather covered (with inertial reels, safety belts and under?seat skirts)
- Armrests for comfortable seats fwd (Qty 3 per row)
- Armrests?cabinets for comfortable seats fwd (LH and RH)
- Headsets Bose ANR type (Qty 7)
- Fashion cabinet (between two armchairs) with newspaper holder
- Multipurpose Cubby with 3 sliding doors
- Separation wall, closed by manual sliding glass window
- Passenger cabin sliding doors
- Super Silent soundproofing
- Sliding door liners leather/leatherette covered with Passenger Service Unit
- Electrically operated pax steps (RH and LH) with boarding lights (in lieu of fixed steps)
- Nose landing gear door
- Customized VIP cabin Finishing from Company selection as applicable i.a.w. prevailing airworthiness directives
- Decoration trim flat (for pax sliding doors)
- Passenger carpet (high thickness)
- Air conditioning system
- P.A. (Passenger Address) system (including loudspeakers and safety belts lights)
- ICS in cabin for all passengers
- Passenger cabin thermo acoustic double layer tinted windows
- Ripple dampers
- Active Vibration Control System (AVCS) provision
- MGB Premium grade
- Stat Com Iridium ST3100 Aircell I?pod dock station on cabinet
- AVCS removable Exterior :
- Customised painting scheme, metallic colours from company selection Maintenance : on CAMP