Sunday, July 7, 2013

Airbus, seats 20

$84,000,000



Airframe:
-EASA Certification
-5 ACT Auxiliary Fuel Tanks for estimated 5,250NM range.
-MTOW Increase – 76.5 Tons
-V2527M-A5 engines
-Two-Shaft High-Bypass Turbofan
-Engine Thrust 26,500 Lbs per Engine
Engine Specs:
-V2527M-A5 engines
Avionics/Radios:
-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)
-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
-Additional wiring for single HFDL function
-Activation of HFDL function for HFDR
-System provisions for SRT2100 SATCOM
-ECAM – OEB reminder function activation on FWC
Additional Equipment:
-Installation on electrical outlets in the cockpit
-Fourth (4) occupant seat in cockpit
-Installation of electrical foot warmers for pilots
Exterior:
2013 Green
Interior:
NEW 2013

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