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 Page 1
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 Page 2
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 Page 3
PICTURES Page 4
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 Page 5
COMLUX AICRAFT SALES TEAM CONTACT DETAILS Americas christophe.lapierre@comluxaviation.com +297 594 78 52 Asia Pacific Philippe Karam philippe.karam@comlux.com +852 5598 8552 Europe & Africa Jean- Michel Champredonde Jean- michel.champredonde@comlux.com +41 79 602 77 77 Middle East & India Claire Brugirard claire.brugirard@comluxaviation.com +973 38 320 038 Russia & CIS Mikhail Kirillov mikhail.kirillov@comluxaviation.com +7 (916)244 48 82 Page 6