by - jet8.com

2018 LEONARDO

AW139

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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.

12A, 68 Connaught Road,

Central, Hong Kong

Contact: Dominique JAUBERTMobile: +1.438.345.0217

Email: [email protected]

PRIVATE AVIATION CONSULTANCYACQUISITIONS - RESALES

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AIRCRAFT DETAILS

Airframe

Entry Into Service: October 2018

Total Time: 241 Hours (As of January 2021)

Cycles: 334

Hoist operation: 60

Serial Number: 41542

Registration: B-704S

Location: China

Engines

Manufacturer: Pratt & Whitney Canada

Model: PT6C-67C

#1 #2

Serial Number: PCE-KB2120 PCE-KB2118

Total Time: 241 Hours 241 Hours

Cycles: 334 334

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.

Inspection Status

Next 1Yr Inspection Due in September 2021

Highlights

HEMS/SAR Configuration

Increased Gross Weight

Low hours

Well maintained

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AW139 Standard Equipment

⁻ Forced fan ventilation

⁻ Bleed air heater and defroster with air noise suppressions

⁻Cockpit air ventilation system

⁻ Baggage compartment cargo tie-down fittings for increased load

capacity (up to 300 kg)

⁻ Rotor brake

⁻ 1st radar altimeter RT-300

⁻ 2nd radar altimeter RT-300

⁻ 4-axis dual Digital Automatic Flight Control System (DAFCS) Basic

incorporated into Modular Avionic Units (MAUs)

⁻ Flight Director System (dual) incorporated into the Modular Avionic

Unit (MAU)

⁻ Two Honeywell GPS modules (GNSS/SBAS – Global Navigation

Satellite System/Satellite Based Augmentation System) with Flight

Plan Management System (FPMS)

⁻One Mode S diversity transponder with Extended Squitter (ADSB-Out

1090 MHz) 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)

⁻ Increased Payload Package - Increased Gross Weight - 6,800 kg

Additional Optional Equipment

⁻AgustaWestland painting scheme, metallic colour from Company

selection

⁻Main rotor blades high visibility painting

⁻Cockpit tinted upper window (*)Smoked colour

⁻Co-pilot hinged window (storm window)

⁻Approach plates chart holders with lights for pilot and co-pilot

(*) Required for single pilot IFR operations. Alternative to central

approach plate chart holder

⁻Air conditioning system

⁻ (*) Accessory drive is required if the air conditioning system is

installed in conjunction with FIPS

⁻Weather Radar Primus 660 Honeywell - Provision

⁻Weather Radar Primus 660 Honeywell - Removable

⁻Cargo hook (2200 kg / 4850 lb) - Provision

⁻ (*) Including cargo hook monitoring cameras provision

⁻ Emergency floats - Provision

⁻ Rescue hoist (Breeze) - provision

⁻ (*) Including: ICS AV-900 Honeywell and Wireless ICS Polycon

⁻ Rescue hoist (Breeze) - Removable

⁻ (*) Including light

⁻ Strobe lights on the winglets

⁻ Bubble cabin window (LH and RH)

⁻ (*) Not compatible with passenger cabin vertical sliding windows on

fixed windows

⁻ - Increased gross weight 7,000 Kg

EQUIPMENT



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Additional Optional Equipment (Cont’d)

⁻ Power outlet 110V

⁻Cabin Door Lighting

⁻ Ice Detector (RAD)

⁻ Standard roof liners with dome lights

⁻Composite liners – painted(no soundproofing)

⁻Rail Floor

⁻Qty 3 Foldable passenger seats – 3rd row

⁻Qty 1 lightweight crashworthy passenger seat – 1st row

⁻ 4-axis DAFCS (Digital Automatic Flight Control System) Enhanced

with Hover Mode (HOV)

⁻Auxiliary transversal fuel tanks 132 USgal provision

⁻Auxiliary transversal fuel tanks 132 USgal Removable

⁻ Engine wash kit

Standard Avionics 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 Multi-Function Display) 8" × 10" (external) colour Active


for visualization of flight and navigation data

Standard Avionics Package (Cont’d)

⁻ 2nd MFD (Co-pilot Multi-Function Display) 8" × 10" (external) colour


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

EQUIPMENT



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Standard Avionics Package (Cont’d)

⁻ 1st PFD (Pilot Primary Flight Display) 8" × 10" (external) colour Active


for visualization of flight and navigation data⁻ 2nd PFD (Co-pilot Primary Flight Display) 8" × 10" (external) colour


System for visualization of flight and navigation data⁻ 1st MFD (Pilot Multi-Function Display) 8" × 10" (external) colour Active


for visualization of flight and navigation data

⁻ 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

Standard Avionic Package(Cont’d)

⁻ Engine 2 fire light

⁻ Baggage compartment smoke detector light

⁻Dual electrical power connection for CVR/FDR (FAA requirement

compliant)

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)

EQUIPMENT



PRIVATE AVIATION CONSULTANCYACQUISITIONS - RESALES

12A, 68 Connaught Road,

Central, Hong Kong

Adrien Chazottes

+60127071477

[email protected]

Diana CHOU

+852 [email protected]

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