2015 Leonardo AW139 S/N 31708
LEONARDO AW139 · Systems Description
Overview
This document provides detailed specifications and descriptions of the 2015 Leonardo AW139 helicopter, including its configuration, engine details, and avionic systems. It serves as an introductory guide for potential purchasers and includes information on maintenance and optional equipment.
- Model: Leonardo AW139
- Year: 2015
- MTOW: 7,000 Kg
- Engine: Pratt & Whitney Canada PWC PT6C-67C
- Total Hours: 931:40 hrs
- VIP Five Star configuration with 3 + 4 passenger seating
- CAA compliant certification
- Includes advanced avionic systems and optional equipment
Document
Source
Originally published by helixel.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Systems Description
- Year ·
- 2015
- File size ·
- 4.0 MB
- Publisher ·
- helixel.com
- Language ·
- en
Specifications & performance
Extracted from this document.
Specifications
- Mtow kg ·
- 7000
Performance
- Total hours ·
- 931:40
What is the 2015 Leonardo AW139 S/N 31708?
The 2015 Leonardo AW139 S/N 31708 is a systems description for the LEONARDO AW139, dated 2015.
Where does the 2015 Leonardo AW139 S/N 31708 come from?
This copy of the 2015 Leonardo AW139 S/N 31708 was originally published by helixel.com and is hosted on Sprinkle as a free, searchable reference copy.
What year was the 2015 Leonardo AW139 S/N 31708 published?
The 2015 Leonardo AW139 S/N 31708 — the LEONARDO AW139 systems description on file — is dated 2015.
Most owners only have the POH. Here's the essential set for the LEONARDO AW139.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
More LEONARDO AW139manuals & documents
In this document
Specifications
The helicopter is a 2015 Leonardo AW139 with a maximum takeoff weight of 7,000 Kg and a total flight time of 931:40 hours.
Engine Details
Equipped with Pratt & Whitney Canada PWC PT6C-67C engines, each with a time between overhaul (TBO) of 5000 hours.
Interior Configuration
Features a VIP Five Star interior layout with a total of 7 seats, including 3 forward-looking VVIP crashworthy armchairs.
Avionic Package
Includes a single pilot configuration with Honeywell Primus Epic Avionics Suite and multiple displays for navigation and flight data.
Optional Equipment
Offers various optional features such as an inlet barrier filter, auxiliary fuel tanks, and enhanced safety systems.
Maintenance History
4 / 8 years maintenance inspections have been completed.
Safety notes
- Specifications are for introductory information only and do not constitute warranties.
- Verification of specifications is the sole responsibility of the purchaser.
- The aircraft is subject to prior sale.
Full document text
Vincent Dulbecco info@helixel.com +39 349 689 8491 helixel.com Specifications and/or descriptions are provided as introductory information only and do not constitute representations or warranties. Verification of specifications remain the sole responsibility of purchaser. The Aircraft is subject to prior sale. Pictures for display purpose only. 2015 Leonardo AW139 S/N 31708 2015 Leonardo AW139 S/N 31708 Helicopter Specifications OEM Leonardo Model Variant AW139 Year 2015 S/N 31708 Reg G-LXRY Configuration VIP FIVE STAR 3 + 4 Pax Certification CAA compliant TOTAL HOURS T.S.N (August 2023) 931:40 hrs Cycles NA ENGINE Engines Model Pratt & Whitney Canada PWC PT6C-67C TBO 5000 Hrs Engine #1 TT 931:40 hrs S/N PCE-KB1754 Cycles NA Engine #2 TT 931:40 hrs S/N PCE-KB1771 Cycles NA SPECS Empty Weight NA MTOW 7.000 Kg Highlights , ESP GOLD & Honeywell Program , VVIP Ultra silent Soundproofin" , Increased Gross Weight 7000 K" , Hinged VVIP Cabin door , Air Conditioning Syste! , Emergency Floats FP& R , 4 / 8 Years Maintenance Inspection completed AW139 Baseline helicopter configuration will be provided on request. Baseline configuration is composed of: r Airfram| r Rotors and controly r Power plant and fuel syste r Transmission drive system and hydraulic syste r Electrical syste r Standard avionic Package (reported here underl r Interior (reported here underl r Painting (reported here underl r Avionic Premium Equipment (reported here under) Optional equipment r Inlet Barrier Filter Provisiony r Electrically operated step (Left & Right) with boarding lighty r Auxiliary transversal fuel tanks 132 US gallon (FP& RPº r Emergency floats FP Kevlar covery r 1 X Camera on tail fin and 2 X Belly cameray r Increased Gross weight 7.000 k² r Liferaft provisiony r Auxiliary heavy-duty battery 28 Ah in lieu of 13 A° r Strobe lighty r Pilot & Copilot Glass windshieldy r Main rotor tracking signal connector in cockpiÏ r AVCS Active Vibration Control Syste r Pilot/ Co-pilot adjustable seats with sheep shin covers Interior Completion VIP Transport: Five Star Customized cabi% r Five Star Interior Layout – 7 seaty r 3 X VVIP crashworthy armchairs leather covered-forward looking: r 4 X VIP crashworthy armchairs leather covered r 2 X additional aft facing Comfortable seat leather covered installed in the central raw (not installedl r Air Conditioning Syste r Mast Vibration Absorber (MVAº r VVIP ultra silent soundproofin² r Night curtain separato3 r Headsets Bose ANR type with Bluetooth capable (X 2º r Multipurpose cubby with hinged cabi% r Night curtain cabin separato3 r Passenger cabin hinged doory r ICS in the cabin for all passengers (ICS phone to speak with pilotsl r Passenger cabin thermos acoustic double layer tinted windowy r Cockpit tinted upper windows (smoked colourl r Co-pilot hinged windo r 2 X Pilot headset hooky r Approach plates chart holders with lights for pilot and co-piloÏ r Cockpit air ventilation syste r 02 X 115V AC power outlets in cabin and one 28V DC power outlet in cockpiÏ r Baggage compartment cargo tie-down fittings (up to 300 kg) Vincent Dulbecco helixel.com info@helixel.com +39 349 689 8491 Tec Spec Q3/ 2023 2015 Leonardo AW139 S/N 31708 Avionic Package: Single Pilot Configuration Night VFR/IFR (EASA/ FAA) r Epic Primus Avionics Suite Software Phase K r 1st PFD (Pilot Primary Flight Display 8" × 10" colour Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation datc r 2nd PFD (Co-pilot Primary Flight Display 8" × 10" colour Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation datc r 1st MFD (Pilot Multi-Function Display 8" × 10" colour Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation datc r 2nd MFD (Co-pilot Multi-Function Display 8" × 10" colour Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation datc r 1 X Electronic Standby Instrument System (ESIS) (attitude, airspeed, altitude, vertical speed, compass, and ILS dataB r 2 X Attitude and Heading Reference Systems (AHRS> r 2 X Air Data Modules (ADM> r 2 X flux valvem r 2 X Display Controllers (DC> r 2 X Cursor Control Devices (CCD> r 1 X Reversion Control Panel (RCP> r 1 X Display Dimming Control Panel (DCP> r 1 X Stability Augmentation System (SAS) control panej r 2 X Remote Instrument Controllers (RIC> r 2 X Modular Avionic Units (MAU) incorporating the following major subsystems and/or functions9 r Vehicle Monitoring System (VMS) duaj r Monitor Warning System (MWS) duaj r Aural Warning Generator (AWG) singl` r Central Maintenance Computer (CMC) singl` r Provision for CVR/FDR data interface (single) r Pilot and co-pilot headsetm r Pilot and co-pilot interphone control (cyclic grip and floor switchesB r Left Modular Radio Cabinet (MRC) with the following modules9 r 1 X VHF Comm r 1 X VOR/LOC/GS/M} r Right Modular Radio Cabinet (MRC) with the following modules9 r 1 X VHF Comm r 1 X VOR/LOC/GS/M} r 1 X AD r 1 X DM{ r 2 X pedestal mounted Multi-function Control Display Units (MCDU> r Emergency Locator Transmitter (ELT> r 1 X flight guidance controlle r Pilot and co-pilot digital audio panels with remote ICS audio port for ground operatio£ r Pilot clock (digitalB r Co-pilot clock (digitalB r 1 X magnetic compasm r 1 X outside air temperature indicato r 2 X Master Warning Lights (MWL> r 2 X Master Caution Lights (MCL> r Engine 1 fire ligh r Engine 2 fire ligh r Baggage compartment smoke detector ligh r Dual electrical power connection for CVR/FDR Avionic Premium Equipment Installed r 2 X Radar Altimeter RT-30 r 4 Axis Digital Automatic Flight Control System DAFCS with HOV mode incorporated into the Modular Avionic Units MA r Flight Director System (dual) incorporated into the MA
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r 2 X Honeywell GPS modules (WASS/SBAS) with Flight Plan Management System FPM r 1 X Mode S diversity Transponder with extended Squitter (ADSB-Out 1,090 MHz) incorporated into the Right Modular Radio Cabinet MR r CVR /FDR with underwater locator beacon ULB Avionic Optionals Installed r HUMS Health & Usage Monitoring Syste\ r TCAS IT r Enhanced Ground Proximity Warning System EGPW r Weather Radar Primus 660 Honeywell Painting r Metallic Paint (beige) with black and gold stripes Specifications and/or descriptions are provided as introductory information only and do not constitute representations or warranties. Verification of specifications remain the sole responsibility of purchaser. The Aircraft is subject to prior sale. Pictures for display purpose only. Vincent Dulbecco helixel.com info@helixel.com +39 349 689 8491 Tec Spec Q3/ 2023 Helixel Limited Ingles Manor Castle Hill Av CT20 2RD Folkestone, United Kingdom Vincent Dulbecco info@helixel.com +39 349 689 8491 helixel.com