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AIA Flight 808 was the first aviation accident where pilot fatigue was cited as a probable cause. [4] The NTSB issued a recommendation to the Federal Aviation Administration to review and update regulations on crew scheduling and duty time limits to incorporate the latest research into the effects of fatigue. [1]
Pages in category "Airliner accidents and incidents involving in-flight depressurization" The following 22 pages are in this category, out of 22 total. This list may not reflect recent changes .
Implementation of fatigue prediction models, such as the Sleep, Activity, Fatigue, and Task Effectiveness model, optimize scheduling by being able to predict pilot fatigue at any point in time. Although the mathematical model is limited by individual pilot differences it is the most accurate existing prediction because it takes into account ...
At this point, sounds of increased wind noise were heard on the CVR. Cabin oxygen masks deployed. The captain declared an emergency to air traffic control, and received clearance to make an emergency descent. The pilots performed a rapid descent to 11,000 feet (3,353 m), where atmospheric pressure is sufficient to prevent hypoxia. [3]
The National Transportation Safety Board (NTSB) determines that the probable cause of this accident was a low-cycle fatigue crack in the dovetail of fan blade No. 13, which resulted in the fan blade separating in flight and impacting the engine fan case at a location that was critical to the structural integrity and performance of the fan cowl ...
Aloha Airlines Flight 243 (IATA: AQ243, ICAO: AAH243) was a scheduled Aloha Airlines flight between Hilo and Honolulu in Hawaii. On April 28, 1988, a Boeing 737-297 serving the flight suffered extensive damage after an explosive decompression in flight, caused by part of the fuselage breaking due to poor maintenance and metal fatigue.
List of aircraft accidents and incidents caused by structural failure; Date Accident/incident Location Aircraft Cause Fatalities Notes 1913-08-07 Death of S F Cody: UK Cody Floatplane "inherent structural weakness" 2 Broke up 1919-08-02 Airliner crash at Verona: Italy Caproni Ca.48: Wing flutter followed by wing collapse 14, 15, or 17 (sources ...
A range of measures is implemented in aviation to enhance safety and prevent accidents. These measures encompass rigorous design standards, continuous monitoring, and comprehensive training. Aircraft Design and Maintenance: Rigorous design and engineering standards are implemented to ensure the structural integrity of aircraft.