Air Crash Daily | American Airlines Flight 1420 News Reports @AirCrashDaily | Uploaded September 2024 | Updated October 2024, 26 minutes ago.
Accident Description:
instagram.com/p/CeQg1BGvg9T/?igshid=ZTcxMWMzOWQ1OA==
๐๐บ๐ฒ๐ฟ๐ถ๐ฐ๐ฎ๐ป ๐๐ถ๐ฟ๐น๐ถ๐ป๐ฒ๐ ๐๐น๐ถ๐ด๐ต๐ ๐ญ๐ฐ๐ฎ๐ฌ was a scheduled domestic passenger flight from Dallas to Little Rock, operated by a McDonnell Douglas MD-82 (Reg. N215AA) on ๐๐๐ป๐ฒ ๐ญ, ๐ญ๐ต๐ต๐ต.
The plane departed Dallas at 22:40. At 23:50:20, the plane touched down on runway 4R at Little Rock National Airport. Over a 7-second period after touchdown, both thrust reversers were deployed and the left and right enginesโ engine pressure ratios (EPR) reached settings of 1.89 and 1.67, respectively. The thrust reversers were subsequently moved to the unlocked status (neither deployed nor stowed). The left brake pedal was relaxed at 23:50:34 before returning to its full position 2 seconds later. About the time that the left brake pedal was relaxed, the reversers were returned to the unlocked status. As the right thrust reverser was being moved to the unlocked status, the right engine reached a maximum setting of 1.74 reverse EPR.
At 23:50:40, the left thrust reverser was moved back to the deployed position, but the right reverser was moved to the stowed position. After departing the end of the runway at 23:50:44, the plane struck several tubes extending outward from the left edge of the instrument landing system localizer array, located 411 feet beyond the end of the runway; passed through a chain link security fence and over a rock embankment to a flood plain, located approximately 15 feet below the runway elevation; and collided with the structure supporting the runway 22L approach lighting system.
๐ฃ๐ฟ๐ผ๐ฏ๐ฎ๐ฏ๐น๐ฒ ๐๐ฎ๐๐๐ฒ:
"The flight crew's failure to discontinue the approach when severe thunderstorms and their associated hazards to flight operations had moved into the airport area and the flight crew's failure to ensure that the spoilers had extended after touchdown. Contributing to the accident were the flight crew's (1) impaired performance resulting from fatigue and the situational stress associated with the intent to land under the circumstances, (2) continuation of the approach to a landing when the company's maximum crosswind component was exceeded, and (3) use of reverse thrust greater than 1.3 engine pressure ratio after landing."
Accident Description:
instagram.com/p/CeQg1BGvg9T/?igshid=ZTcxMWMzOWQ1OA==
๐๐บ๐ฒ๐ฟ๐ถ๐ฐ๐ฎ๐ป ๐๐ถ๐ฟ๐น๐ถ๐ป๐ฒ๐ ๐๐น๐ถ๐ด๐ต๐ ๐ญ๐ฐ๐ฎ๐ฌ was a scheduled domestic passenger flight from Dallas to Little Rock, operated by a McDonnell Douglas MD-82 (Reg. N215AA) on ๐๐๐ป๐ฒ ๐ญ, ๐ญ๐ต๐ต๐ต.
The plane departed Dallas at 22:40. At 23:50:20, the plane touched down on runway 4R at Little Rock National Airport. Over a 7-second period after touchdown, both thrust reversers were deployed and the left and right enginesโ engine pressure ratios (EPR) reached settings of 1.89 and 1.67, respectively. The thrust reversers were subsequently moved to the unlocked status (neither deployed nor stowed). The left brake pedal was relaxed at 23:50:34 before returning to its full position 2 seconds later. About the time that the left brake pedal was relaxed, the reversers were returned to the unlocked status. As the right thrust reverser was being moved to the unlocked status, the right engine reached a maximum setting of 1.74 reverse EPR.
At 23:50:40, the left thrust reverser was moved back to the deployed position, but the right reverser was moved to the stowed position. After departing the end of the runway at 23:50:44, the plane struck several tubes extending outward from the left edge of the instrument landing system localizer array, located 411 feet beyond the end of the runway; passed through a chain link security fence and over a rock embankment to a flood plain, located approximately 15 feet below the runway elevation; and collided with the structure supporting the runway 22L approach lighting system.
๐ฃ๐ฟ๐ผ๐ฏ๐ฎ๐ฏ๐น๐ฒ ๐๐ฎ๐๐๐ฒ:
"The flight crew's failure to discontinue the approach when severe thunderstorms and their associated hazards to flight operations had moved into the airport area and the flight crew's failure to ensure that the spoilers had extended after touchdown. Contributing to the accident were the flight crew's (1) impaired performance resulting from fatigue and the situational stress associated with the intent to land under the circumstances, (2) continuation of the approach to a landing when the company's maximum crosswind component was exceeded, and (3) use of reverse thrust greater than 1.3 engine pressure ratio after landing."