OEABC - 2010 AIRBUS A318
Aircraft Summary
General
Year
2010
Manufacturer
AIRBUS
Model
A318
Serial Number
1234
Registration #
OEABC
Condition
Used
FlightRules
IFR
Description
Green Delivery will be in November 2010. Outfitting is planned at Lufthansa Technik in Tulsa (duration 5 to 6 months). Interior changes are still possible. New Airbus A318Elite
Engine Program
Engine Program Notes
CFM56-5B9/P
Avionics
Avionics/Radios
* Flight Augmentation Computer: Thales, Avionics SA
* Flight control unit: Thales, Avionics SA
MCDU Honeywell
* Flight Management Guidance Computer: Thales / Honeywell
* VDR/COMM transceiver VHF-900B: Rockwell Collins
* Radio Management Panel: Thales, Avionics SA
* ADIRU: Honeywell
* Standby altimeter: Thales, Avionics SA
* Standby airspeed indicator: Thales, Avionics SA
* Standby compass: SIRS Navigation
* Standby horizon: Thales, Avionics SA
* Multi-mode receiver: Rockwell Collins
* Weather radar antenna: Honeywell
* Weather radar antenna, dual mount: Honeywell
* Weather radar dual control panel: Honeywell
* Weather radar transceiver: Honeywell
* Weather radar dual transceiver mount: Honeywell
* Radio altimeter transceiver: Thales, Avionics SA
* Enhanced Ground Proximity Warning Computer: Honeywell
* DME interrogator, DME-900. Rockwell Collins
* ATC transponder / DME antenna: Rayan
* ATC/TCAS dual control panel: Thales, Avionics SA
* ATC mode S transponder: Honeywell
* ADF antenna: EAS
* ADF receiver, ADF 900: Rockwell Collins
* VOR antenna: Rayan
* Marker antenna: Rayan
* VOR/Marker receiver (VOR-900): Rockwell Collins
* DDRMI :Thales, Avionics SA
Additional Equipment
Additional Equipment
* 2 Additional Center Tanks are installed (can be removed easily)
* Polar navigation function
* Steep approach capability
* EASA JAR 25 and compliance with JAR OPS1 – subpart K and L
* Partial compliance with FAA type certificate requirement
*Increased design weight to 66t MTOW
*Operation on runways with reduced width
Air conditioning
• Floor panel heating for forward door area
Auto Flight
• Polar navigation function
• Steep approach capability
• Flight management kits
Communications
• Emergency Locator Transmitter
• Dual HF system and activation of data link function
• VHF data radio
• Cockpit Voice Recorder
• Radio Management Panel
Electrical Power
• Installation of additional electrical outlets 115V/60Hz in flight deck
Equipment/furnishings
• Fourth occupant seat in flight deck
• Electrical foot warmers for pilots
• Cargo Floor panels: Rubber seal & Reinforced for heavy bulk usage
• Slide rafts at forward service and entry doors
• Cabin configuration prior to outfitting (including G2 structural provisions)
Exterior
Year Painted
2010
Exterior Notes
New Aircraft
Interior
Year Interior
2010
Number of Seats
19
Interior Notes
Outfitting will be at Luftahnsa Technik in Tulsa, USA
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