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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.

2018 Leonardo Helicopter AW139 by - Jet 8 – We

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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]