5
Airbus ACJ
YEAR:
2012
S/N:
TBD
REG:
TTAF:
New
LOCATION:
NC, USA
UPDATED: 3/31/2012 3:58:38 AM
AIRFRAME / ENGINES / APU
Airframe
Airframe Highlights:
• EASA Certification
• 5 ACT Auxiliary Fuel Tanks
• MTOW Increase – 76.5 Tons
• EASA Certification
• 5 ACT Auxiliary Fuel Tanks
• MTOW Increase – 76.5 Tons
Engines
GUARANTEED LONDON TO LOS ANGELES RANGE!
Left & Right:
Engine Make: IAE International Aero Engines
Engine Model : V2527M-A5 w/SelectOne Product Upgrade
Description: Two-shaft high-bypass turbofan engine
Thrust: 26,500 lbs per engine
Left & Right:
Engine Make: IAE International Aero Engines
Engine Model : V2527M-A5 w/SelectOne Product Upgrade
Description: Two-shaft high-bypass turbofan engine
Thrust: 26,500 lbs per engine
APU
AVIONICS
Standard Avionics:
Digital Automatic Flight System (AFS) consisting of:
• Two (2) Flight Augmentation Computers
• Two (2) Flight Management & Guidance Computers
• Two (2) Multipurpose Control & Display Units
• Flight Control Unit
• Dual Autopilot & Flight Director
• Dual Autothrust
• Fail Operational Automatic Landing
• Aircraft Communication Addressing & Reporting system (ACARS)
• Dual Radio Altimeters
• Air Data/Inertial Reference system (ADIRS)
Digital Automatic Flight System (AFS) consisting of:
• Two (2) Flight Augmentation Computers
• Two (2) Flight Management & Guidance Computers
• Two (2) Multipurpose Control & Display Units
• Flight Control Unit
• Dual Autopilot & Flight Director
• Dual Autothrust
• Fail Operational Automatic Landing
• Aircraft Communication Addressing & Reporting system (ACARS)
• Dual Radio Altimeters
• Air Data/Inertial Reference system (ADIRS)
• Global Positioning Unit (GPS)
• Digital Flight Data Recording system (DFDRS)
• Centralized Fault Display system (CFDS)
• Aircraft Integrated Data system (AIDS)
• Electronic Instrument System (EIS)
• Integrated Standby Instrument system (ISIS)
• Two (2) HF Data Radio systems (HFDR)
• Three (3) VHF Data Radio systems (VDR)
• Audio/SELCAL & Call systems
• Solid State Cockpit Voice Recorder (SSCVR)
• System Provisions and limited installation for the CIDS
• Two (2) Radio Management Panels w/8.33 kHz spacing (RMP)
• Emergency Locator Transmitter
• Dual Distance Measuring Equipment (DME)
• Automatic Direction Finder (ADF)
• Digital Flight Data Recording system (DFDRS)
• Centralized Fault Display system (CFDS)
• Aircraft Integrated Data system (AIDS)
• Electronic Instrument System (EIS)
• Integrated Standby Instrument system (ISIS)
• Two (2) HF Data Radio systems (HFDR)
• Three (3) VHF Data Radio systems (VDR)
• Audio/SELCAL & Call systems
• Solid State Cockpit Voice Recorder (SSCVR)
• System Provisions and limited installation for the CIDS
• Two (2) Radio Management Panels w/8.33 kHz spacing (RMP)
• Emergency Locator Transmitter
• Dual Distance Measuring Equipment (DME)
• Automatic Direction Finder (ADF)
• Weather Radar system
• Traffic & Collision Avoidance systems (TCAS II)
• Multifunction Printer
• Up & Down Data Loading system
• Central Warning System (CWS)
• Enhanced Ground Proximity Warning system (EGPWS)
• ATC Transponder – Mode S
Avionics Options (SCN’s):
• Additional wiring for single HFDL function
• Activation of HFDL function for HFDR
• System provisions for SRT2100 SATCOM
• ECAM – OEB reminder function activation on FWC
• Traffic & Collision Avoidance systems (TCAS II)
• Multifunction Printer
• Up & Down Data Loading system
• Central Warning System (CWS)
• Enhanced Ground Proximity Warning system (EGPWS)
• ATC Transponder – Mode S
Avionics Options (SCN’s):
• Additional wiring for single HFDL function
• Activation of HFDL function for HFDR
• System provisions for SRT2100 SATCOM
• ECAM – OEB reminder function activation on FWC
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