Aircraft Specification Sheet ACJ319 MSN1485aeroclassifieds.com/Media/ListingPDF/Airbus_ACJ319_2… · · 2016-08-09RVSM!Compliant!–!Triple!Air!Data/Inertial!Reference!System!

AIRCRAFT SPECIFICATION SHEET

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AIRCRAFT TYPE

AIRBUS ACJ319

SERIAL NUMBER AND REGISTRATION

1485 / VQ-‐BKK

AIRCRAFT HIGHLIGHTS

Ø This ACJ319 is configured for Head of State or Corporation operations. It can accommodate up to 32 passengers in Executive /First class configuration. The cabin is certificated for public transport.

Ø The cabin completion has been performed by Air France Industries in Paris in 2001. The aircraft has been refurbished in January 2013 to increase comfort on board by reducing seating capacity.

Ø IFE includes Audio video (CD, DVD), Multi-‐channel Satcom and Airshow. The aircraft is fitted with 4 Additional Center Tanks and it can perform missions of more than 9 Hours (4500 nm). Typical missions: Singapore to Hong Kong: 3hrs 20min Los Angeles to London : 10hrs London to Dubai : 7hrs 30 min


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GENERAL Year of manufacture 2001 Entry into service February 2002 Design Weights Maximum Taxi Weight: 75,900 Kg Maximum Takeoff Weight: 75,500 Kg Maximum Zero Fuel Weight: 58,500 Kg Maximum Landing Weight: 62,500 Kg Airframe Total Time: 5469 hrs. as of March 2015 Total Landings: 5615 ldg as of March 2015 Engines Engine Model: CFM 56-‐5B7/P Engine 1 S/N: 57554 TSN/CSN: 5255.3 hrs. /5270 cycl. Engine 2 S/N: 57553 TSN/CSN: 5162.1 hrs. /5293 cycl. APU APU Model: APIC APS3200 APU S/N / Part: 1785/4500001B TSN/CSN: 6317hrs. / 5829 cycl. MAINTENANCE ACJ319 VQ-‐BKK maintenance provider is Singapore Airlines Engineering Company (SIAEC) • Landing gear overhauled in July 2011 by SIAEC • 12 Year check carried out in December 2012 at SIAEC in Singapore • Latest refurbishment carried out by SIAEC in January 2014 (from 47 seats to 32 seats) • C Check Carried out in December 2014 at SIAEC in Singapore Due checks: • Next C Check due in January 2016 • Engines and APU are “condition monitored”


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INTERIOR

The aircraft has 32 seats with an AFM supplement to reduce the capacity to 28 when operating into China. The cabin is certificated for public transport. Aircraft entrance • Galley area (Chiller, Storage drawers and ice container, Sink, Water Boiler, Espresso Coffee Maker, fan oven and cupboards) • Forward lavatory Forward VIP Section • 2 Club-‐4 with foldable tables ( 8 passengers) – convertible in 2 twin beds • 2 x 21” Television Monitors •2 Medium sized storage VIP Bathroom • Full Height Shower with sliding door • Sink with lighted vanity mirror • Flushing Lavatory Main cabin • 16 Lie-‐Flat First class seats 60” pitch • 10” IFE Screen and electrical Power Outlet for each seat • Overhead stowage Aft VIP section • 2 Club-‐4 with foldable tables ( 8 passengers) – convertible in 2 twin beds • 2 x 21” Television Monitors •2 Medium sized storage Rear cabin: • galley (Sink,Water Boiler, Coffee Maker,Two Fan Assisted Ovens, Full size Work Surface, Storage) • 2 lavatories EXTERIOR White background with a red and blue stripe from the tail to the front of the Aircraft


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PICTURES


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AVIONICS Auto Flight System 2 Flight Augmentation Computers – FAC (Thales) 2 Flight Management & Guidance Computers – FMGC (Thales) 2 Multipurpose Control & Display Units -‐ MCDU (Honeywell) Flight Control Unit – FCU (Thales) Communication systems 2 HF Radio Systems (Rockwell Collins) 2 VHF Radio Systems (Rockwell Collins) 2 Radio Management Panels (Thales) 1 SELCAL (Selective Calling System -‐ Team) 1 Solid State Cockpit Voice Recorder (L-‐3-‐C) Emergency Location Transmitter Honeywell ( 1 fixed + 2 portable) 1 tape reproducer PRAM Matsushita 1 AMU Team 1 Satellite Communication System (Rockwell Collins) 8.33 hz Channel Spacing Cabin Intercommunication Data System – CIDS Indication & Recording Systems 6 X Identical 7.25 X 7.25 LCD Multi-‐Function Electronic Displays Centralised Fault Display System – CFDS (Thales) 1 Digital Flight Data Recording System – DFDRS (Honeywell) Aircraft Integrated Data System – AIDS (SAGEM) 1 FDIU Sagem 1 FDMU Sagem Electronic Flight Instrument System – EFIS consisting of: 3 X Data Management Computers – DMC 2 X Flight Warning Computer – FWC 2 X System Data Acquisition Concentrators – SDAC Multifunction Printer Navigation Equipment RVSM Compliant – Triple Air Data/Inertial Reference System (ADIRS) Honeywell Enhanced Ground Proximity Warning (EGPWS) Honeywell 1 TCAS II – Traffic Alert & Collision Avoidance System Rockwell Collins 2 X Multimode Receivers (MMR) Rockwell Collins comprising Instrument Landing System (ILS), Global Positioning (GPS) Receiver 2 X Weather Radar Systems 2X Radio Altimeter with Automatic Call Out Thales 2 X Distance Measuring Equipment (DME) Interrogators Rockwell Collins 2 X Mode S Air Traffic Control (ATC) Transponders Rockwell Collins Automatic Direction Finding (ADF) Receiver Rockwell Collins ADS-‐B ACARS


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COMLUX AICRAFT SALES TEAM CONTACT DETAILS

Americas

[email protected] +297 594 78 52

Asia Pacific

Philippe Karam [email protected]

+852 5598 8552

Europe & Africa Jean-‐Michel Champredonde

Jean-‐[email protected] +41 79 602 77 77

Middle East & India Claire Brugirard

[email protected] +973 38 320 038

Russia & CIS Mikhail Kirillov

[email protected] +7 (916)244 48 82

Documents

Aircraft Specification Sheet ACJ319 MSN1485aeroclassifieds.com/Media/ListingPDF/Airbus_ACJ319_2… · · 2016-08-09RVSM!Compliant!–!Triple!Air!Data/Inertial!Reference!System!