• Airbus A320 Technical Training Manual

Crew 2 Passengers 150 / 179 Propulsion 2 Turbofan Engines Engine Model IAE International Aero Engines V2527-A5 Engine Power (each) 110,3 kN 24800 lbf alternative Engine Variant Engine Model CFM Intl. CFM56-5B4 Engine Power (each) 120,1 kN 27000 lbf Speed 904 km/h 488 kts 562 mph Mmo (max. Mach) Mach 0.82 Service Ceiling 12.131 m 39.800 ft Range 5.700 km 3.078 NM 3.542 mi.

Airbus A320 Technical Training Manual

Empty Weight 37.230 kg 82.078 lbs max. Takeoff Weight 77.000 kg 169.756 lbs max. Landing Weight 64.500 kg 142.198 lbs Wing Span 34,09 m 111 ft 10 in Wing Area 122,6 m² 1320 ft² Length 37,57 m 123 ft 3 in Height 11,76 m 38 ft 7 in First Flight Production Status in production ICAO Code A320 IATA Code 320 32A FAA TCDS A28NM EASA TCDS A.064 Data for (Version) Airbus A320-232 Variants A320-111, A320-211, A320-212, A320-214, A320-215, A320-216, A320-231, A320-232, A320-233. Flugzeuginfo.net The web portal flugzeuginfo.net includes a comprehensive civil and military aircraft encyclopedia. It provides code tables for aerodromes, air operators including the world's major airlines and for ICAO and IATA codes for aircraft. The website has also a photo gallery and gives you an overview of all aviation museums worldwide. The website was updated on flugzeuginfo.net 2016 beta The website is currently in the process of optimizing and will have further functions added in order to improve the usability.

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Level 1 General Familiarisation A brief overview of the airplane, systems and powerplants as outlined in the Systems Description section of the Aircraft Maintenance Manual. Level 2 Ramp and Transit Basic System overview of controls, indicators, principal components including their location and purpose, servicing and minor trouble shooting. Level 3 Line and Base Maintenance In addition to the information contained in level 1 and level 2 training, upon completion of the level 3 training, the participant will be able to:. Describe how to perform system, component and functional checks as specified in the maintenance. manual. Correlate information for the purpose of making decisions in respect of fault diagnosis and.

rectification to the maintenance manual level. Describe procedures for replacement of components unique to the aircraft to maintenance manual level.