2018 leonardo helicopter aw139 by - jet 8 – we

11
12A, 68 Connaught Road, Central, Hong Kong Contact: Adrien Chazottes Mobile: +6012 707 1477 Email: [email protected] PRIVATE AVIATION CONSULTANCY ACQUISITIONS - RESALES 2018 Leonardo Helicopter AW139 by Specifications and descriptions are provided as introductory information. They do not constitute representations or warranties of Jet 8 Aviation or Jet 8 Aviation’s Client. Buyers should rely on their own inspection of the aircraft and its records. Aircraft remains subject to prior sale, lease or withdrawal from the market without notice.

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Page 1: 2018 Leonardo Helicopter AW139 by - Jet 8 – We

12A, 68 Connaught Road,

Central, Hong Kong

Contact: Adrien ChazottesMobile: +6012 707 1477

Email: [email protected]

PRIVATE AVIATION CONSULTANCYACQUISITIONS - RESALES

2018 LeonardoHelicopter AW139

by

Specifications and descriptions are provided as introductory information. They do not constitute representations or warranties of Jet 8 Aviation or Jet 8 Aviation’s Client. Buyers should rely on their own inspection of the aircraft and its records. Aircraft remains subject to prior sale,

lease or withdrawal from the market without notice.

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AIRCRAFT DETAILS

Airframe (as of August 2020)

Entry into Service: August 2019

Manufactory Date: July 2018

Serial: 31793

Location: China

Total Time: 19 Hours

Landings: 42

Engines

Make: Pratt & Whitney Canada

Model: PT6C-67C

Serial: # 1: PCE-KB1997 # 2: PCE-KB2009

Times : # 1: 19 hrs # 2: 19 hrs

Cycles: # 1: 34 # 2: 34

Specifications and descriptions are provided as introductory information. They do not constitute representations or warranties of Jet 8 Aviation or Jet 8 Aviation’s Client. Buyers should rely on their own inspection of the aircraft and its records. Aircraft remains subject to

prior sale, lease or withdrawal from the market without notice.

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HIGHLIGHTS

Almost New.

Always Hangered.

Very Few Hours – Only test flight hour and daily maintenance engine run.

Oil & Gas Offshore Mission Qualified.

Floorplan

Number of Passenger: 12 Pax seats / Single Stretcher

Specifications and descriptions are provided as introductory information. They do not constitute representations or warranties of Jet 8 Aviation or Jet 8 Aviation’s Client. Buyers should rely on their own inspection of the aircraft and its records. Aircraft remains subject to

prior sale, lease or withdrawal from the market without notice.

Performance

MTOW: 7,000KG

Fuel Capacity: 1,568L

VNE: 310kM/H

Max Cruise Speed: 306kM/H

Max Operation Altitude: 6,096M

Max Range: 1,061kM (with Aux Fuel Tank, No reserve)

Max Endurance: 5h13min (with Aux Fuel Tank, No reserve)

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AVIONICS

Specifications and descriptions are provided as introductory information. They do not constitute representations or warranties of Jet 8 Aviation or Jet 8 Aviation’s Client. Buyers should rely on their own inspection of the aircraft and its records. Aircraft remains subject to

prior sale, lease or withdrawal from the market without notice.

• 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 Multi-Function 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 Multi-Function 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- Provision for CVR/FDR data interface (single)"

• 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 VOR/LOC/GS/MB- One ADF- One DME"

• Two pedestal mounted Multifunction Control Display Units (MCDU)

• Emergency Locator Transmitter (ELT)

• One flight guidance controller

• 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)

• 1st radar altimeter RT-300

• 2nd radar altimeter RT-300

• 4-axis dual digital automatic flight control system(DAFCS) Basic incorporated into

Modular Avionics Units(MAUs)

• Flight Director System (Dual) incorporated into the Modular Avionics Unites(MAU)

• Two Honeywell GPS modules with Flight Plan Management System(FPMS)

• One Model S diversity transponder with Extended Squitter (ADSB-Out 1090MHz)

incorporated into the Modular Radio Cabinet(MRC)

• Cockpit Voice Recorder & Flight Data Recorder (CVR/FDR) with Underwater

Locator Beacon (ULB)

• Health & Usage Monitoring System (HUMS)

• Enhanced Ground Proximity Warning System(EGWPS) Provision

• Enhanced Ground Proximity Warning System(EGWPS) removable

• ADELT (2-frequency Automatic Deployable ELT w/ GPS interface) (*) In liieu of

standard ELT

• TCAS I KTA-970 Honeywell Bendix/King provision

• TCAS I KTA-970 Honeywell Bendix/King removable (*) Required for VFR night single

pilot operations."

• Weather Radar Primus 660 Honeywell provision

• Weather Radar Primus 660 Honeywell removable

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EQUIPMENT

• Forced fan ventilation

• Bleed air heater and deforster with air noise

suppressions

• Cockpit air ventilation system

• Baggage compartment cargo tie-down for increased

load capacity(up to 300KG)

• Rotor brake

• Air conditioning system

• Emergency floats provision

• Emergency floats removable

• Life rafts up to 14 passengers each provision (Qty 2)

• Life rafts up to 14 passengers each removable(Qty 2)

• Auxiliary transversal fuel tank 132 USgal provision

• Auxiliary transversal fuel tank 132 USgal removable

• External louderspeakers(400W) Provision

• External louderspeakers(400W)removable• "Rescue hoist (Goodrich) provision - single type(*)

Including ICS AV900 Honeywell, wireless ICS Polycon

and swivelling light for rescue hoist (belly mounted)"

• Rescue hoist (Goodrich) removable - single type

• Maritime protection

• Aerolite single stretcher(installed transversally)

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Page 11: 2018 Leonardo Helicopter AW139 by - Jet 8 – We

PRIVATE AVIATION CONSULTANCYACQUISITIONS - RESALES

12A, 68 Connaught Road,

Central, Hong Kong

Adrien Chazottes

+60127071477

[email protected]

Diana CHOU

+852 [email protected]