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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. 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. 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 around 9 Hours (4200 nm).
Engine Model: CFM 56-5B7/P
Engine 1 S/N: 575154 TSN/CSN: 5278 hrs. /5276 cycl.
Engine 2 S/N: 575153 TSN/CSN: 5185 hrs. /5299 cycl.
APU Model: APIC APS3200
APU S/N / Part: 1785/4500001B TSN/CSN: 6525 hrs. / 5654 cycl.
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
White background with a red and blue stripe from the tail to the front of the Aircraft
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
Inspection Status
All maintenance due till April 2016 has been performed
ACJ319 VQ-BKK major maintenance provider : 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
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