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General Secretary

2018, Sangaya

Abstract

Amsterdam Schiphol Airport is referred to as Schiphol airport in this report. 2 The preliminary report that was published by the Board on 28 April 2009 made mention of 83 injured passengers instead of 117. This difference is caused by becoming available, during the investigation, of accurate data concerning the injuries of occupants and the application of another injury classification (see Appendix E). 106 C-check: regular maintenance on the aircraft that takes place every 7000 flight hours or 2 years (whichever occurs first). This varies with regard to each aircraft type and use. The maintenance is performed by taking the aircraft out of service. 107 A-check: regular maintenance on the aircraft that takes place every 600 flight hours or 2 months (whichever occurs first). This varies with regard to each aircraft type and use. This maintenance can take place at night at the gate without having to take the aircraft out of service. 108 Certified to be used in models 737-600, 737-700, 737-700C, 737-800, 737-900 and BBJ (Boeing Business Jet). 109 Certified to be used in models 737-600, 737-700, 737-700C, 737-800, 737-900 and BBJ (Boeing Business Jet).

Key takeaways

  • Remarkably though, in spite of this safety programme, the Flight Safety Department of Turkish Airlines received 550 flight safety reports from cockpit crews in 2008, but none of these reports mentioned problems with the radio altimeter system, unintentional landing gear warnings and autothrottle 'RETARD' mode during approach.
  • This happens during every flight when the aircraft is above the height range of the radio altimeter system.
  • The radio altimeter system did not operate correctly causing anomalous behaviour of the automatic flight system and other systems on the aircraft during flight TK1951.
  • The Boeing 737-800 Flight Crew Operations Manual on board of the accident aircraft, of which the Quick Reference Handbook forms part, does not include these procedures either.
  • Assuming an average flight time of 3 hours, the failure rate of the radio altimeter system on this aircraft was once per 23.2 flight hours.