Airbus A318 Elite for Sale
External Livery :
White fuselage, standard grey wings
White fuselage, standard grey wings
General aircraft design criteria :
A318-112 increased design weights - MTOW to 66 t, MLW to 57.5 t, MZFW to 54.5 t
Avionics ventilation air filter alternate equipment
Installation of ozone catalytic converters
A318-112 increased design weights - MTOW to 66 t, MLW to 57.5 t, MZFW to 54.5 t
Avionics ventilation air filter alternate equipment
Installation of ozone catalytic converters
Auto Flight :
FM kits (FMGC P1C12A) / MCDU alternative equip - with CFM engines
Introduction of polar navigation function
FM kits (FMGC P1C12A) / MCDU alternative equip - with CFM engines
Introduction of polar navigation function
Communication :
Automatic programmable ELT with programmable dongle associated with remote control panel in cockpit
Installation of dual HF system (data link capable)
Installation of third RMP with turbo tuning of VHF channels and HF data activation capability -
Thales avionics
Installation of SATCOM AERO I system - Rockwell collins SAT 2000-6 (6 channels)
CN23.28.147/16 Cockpit voice interface - SATCOM AERO I Rockwell Collins with basic ACP installation
Automatic programmable ELT with programmable dongle associated with remote control panel in cockpit
Installation of dual HF system (data link capable)
Installation of third RMP with turbo tuning of VHF channels and HF data activation capability -
Thales avionics
Installation of SATCOM AERO I system - Rockwell collins SAT 2000-6 (6 channels)
CN23.28.147/16 Cockpit voice interface - SATCOM AERO I Rockwell Collins with basic ACP installation
Electrical Power :
Installation of additional electrical outlets 115 V/60 Hz in cockpit
Installation of additional electrical outlets 115 V/60 Hz in cockpit
Equipment / Furnishing :
Floor panel heating for forward passenger/crew/service door area
Pilots seats alternate cover - sheepskin
Installation of fourth occupant seat in cockpit
Installation of electrical foot warmers for pilots (increased setting)
Cabin configuration prior to outfitti ng (incl. G2 structural provision)
Instal. of slide rafts at fwd pax/crew/service doors
Install of document pouch in cockpit
Installation of heated floor panel with inserts for threshold in fwd door area
Install of heating panel on/off control function on FAP
Installation of rubber seal profiles for floor panels in fwd and aft cargo holds
Reinforced floor panels in fwd & aft cargo holds - with full bulk configuration
Floor panel heating for forward passenger/crew/service door area
Pilots seats alternate cover - sheepskin
Installation of fourth occupant seat in cockpit
Installation of electrical foot warmers for pilots (increased setting)
Cabin configuration prior to outfitti ng (incl. G2 structural provision)
Instal. of slide rafts at fwd pax/crew/service doors
Install of document pouch in cockpit
Installation of heated floor panel with inserts for threshold in fwd door area
Install of heating panel on/off control function on FAP
Installation of rubber seal profiles for floor panels in fwd and aft cargo holds
Reinforced floor panels in fwd & aft cargo holds - with full bulk configuration
Fire Protection :
Cargo holds fireextinguishers extended duration for ETOPS 120 min (A318)
Cargo holds fireextinguishers extended duration for ETOPS 120 min (A318)
Ice and rain protection :
Water/Waste protection - Install freezing protection (A318)
Water/Waste protection - Install freezing protection (A318)
Indicating / Recording systems :
Activati on of ECAM OEB reminder function on FWC
Indication of metric altitude on PFD
Installation of V-bar flight director
Activati on of ECAM OEB reminder function on FWC
Indication of metric altitude on PFD
Installation of V-bar flight director
Navigation :
QNH/QFE BARO settings
ADIRU 4MCUNORTHROP GRUMMAN
Installation of ISIS
Structural andwiring provisions for single HUD system installation
W/R COLLINS PWS activated
Dual WXR (ARINC 708A) with PWS activation - ROCKWELL COLLINS
Radio Al timeters COLLINS
TCAS change 7 - ROCKWELL COLLINS 921 / ATC ELS, EHS - ROCKWELL COLLINS 901
DDRMI VOR/ADF/DME - Rockwell Collins
Installation of dual ADF system - Rockwell Collins 900
QNH/QFE BARO settings
ADIRU 4MCUNORTHROP GRUMMAN
Installation of ISIS
Structural andwiring provisions for single HUD system installation
W/R COLLINS PWS activated
Dual WXR (ARINC 708A) with PWS activation - ROCKWELL COLLINS
Radio Al timeters COLLINS
TCAS change 7 - ROCKWELL COLLINS 921 / ATC ELS, EHS - ROCKWELL COLLINS 901
DDRMI VOR/ADF/DME - Rockwell Collins
Installation of dual ADF system - Rockwell Collins 900
Information Systems :
AIRBUS standard AOC software from ROCKWELL COLLINS with units in kg (by default)
AIRBUS standard AOC software from ROCKWELL COLLINS with units in kg (by default)
Structures :
Alternate paint systems (CF primer ) on fuselage and vertical stabilizers
Alternate paint systems (CF primer) on nacelles
Alternate paint systems (CF primer ) on fuselage and vertical stabilizers
Alternate paint systems (CF primer) on nacelles
Doors :
Installation ofentrance stairs at forward LH passenger/crew/service door
Installation ofentrance stairs at forward LH passenger/crew/service door
Windows :
Alternate front windows - PPG
Alternate front windows - PPG
Engines :
CFMI engines - CFM56-5B9/P (SAC) at 23 300 lbf nominal thrust (A318-112)
CFMI engines - CFM56-5B9/P (SAC) at 23 300 lbf nominal thrust (A318-112)
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