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The list of aircraft accidents and incidents caused by structural failures summarizes notable accidents and incidents such as the 1933 United Airlines Chesterton Crash due to a bombing and a 1964 B-52 test that landed after the vertical stabilizer broke off. Loss of structural integrity during flight can be caused by:
United Airlines Flight 328 N772UA, the aircraft involved in 2012 Incident Date February 20, 2021 13:08 MST (2021-02-20UTC20:08Z) Summary Engine failure caused by metal fatigue Site Over Broomfield, Colorado, U.S. 39°55′44″N 105°03′18″W / 39.929°N 105.055°W / 39.929; -105.055 Aircraft Aircraft type Boeing 777-222 [a] Operator United Airlines IATA flight No. UA328 ICAO ...
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 ...
The aircraft experienced complete loss of electrical power shortly after takeoff and eventually crashed into terrain while trying to navigate in the dark without instrumentation; the captain was blamed for attempting to continue to the flight's destination rather than executing an emergency landing at the departure airport.
A Eurocopter AS350D helicopter lost power and crash landed in an open field.The sole survivor reported that the pilot reset an engine chip light 5-10 times 20–25 minutes prior to the crash. 3 1 Pilot's decision to continue flight after known engine problem and the subsequent seizure of the number two engine bearing. [54] 1991-07-05
The subsequent loss of control killed all but one of the 103 people on board, the deadliest aviation disaster in Algeria until the 2018 Algerian Air Force Ilyushin Il-76 crash, in which a Ilyushin Il-76 crashed shortly after take-off on 11 April 2018, killing all 257 people on board.
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 ...
The aircraft crash investigation mainly focused on a fuel leak caused by fatigue failure of an experimental fuel pipe in the power plant zone. The pipe was instrumented with a temperature sensor. The official report concluded the fuel leak likely started at 18:18 hours at a rate of 220 kg/min, totaling an estimated 8000 kg fuel loss.