Flight with disabled controls: Difference between revisions

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Controls damaged by engine failure: added link to IL-62 article
Controls damaged by engine failure: added link to DC-10 article
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*[[LOT Polish Airlines Flight 5055]], an [[Ilyushin Il-62]]M, on 9 May 1987. According to the Polish investigatory commission, the cause of the crash was the disintegration of an engine shaft due to faulty bearings inside engine No. 2, which seized, causing extensive heat. This in turn caused the consequent damage to engine No. 1, [[rapid decompression]] of the fuselage, and a fire in the cargo hold, as well as the loss of elevator controls and progressive electrical failures. Zygmunt Pawlaczyk decided to return to [[Warsaw Frederic Chopin Airport|Warsaw Okecie Airport]] using only [[trim tab]]s to control the flight of the aircraft. He lost his struggle to land about 5&nbsp;km from the runway in the Kabacki Forest. All 172 passengers and 11 crew members perished.<ref>Gero 1997, p. 199.</ref>
*[[United Airlines Flight 232]], a [[McDonnell Douglas DC-10]], on 19 July 1989. A fan disk in the No. 2 engine fractured, severing most of the flight controls. [[Dennis E. Fitch|Dennis Fitch]], a [[Deadheading (aviation)|deadheading]] DC-10 instructor who had studied the case of [[Japan Airlines Flight 123|JAL Flight 123]], was able to help the pilots steer the aircraft using throttle differential. Despite the break-up of the aircraft on landing, 175 of 285 passengers and 10 of the 11 crew members survived.<ref>Gero 1997, p. 210.</ref>
 
===Controls damaged by structural failure===