Air Crash Daily | Midwest Express Flight 105 ATC Recording @AirCrashDaily | Uploaded May 2024 | Updated October 2024, 1 hour ago.
Credits: @elsopaipilla315
Accident Description: instagram.com/p/CiKyEcyBK9t/?igsh=dmVyaGd0dGJjYjF3
Photos Archive:
https://x.com/aircrashdaily/status/1567157752040157184?s=19
๐ ๐ถ๐ฑ๐๐ฒ๐๐ ๐๐ ๐ฝ๐ฟ๐ฒ๐๐ ๐๐น๐ถ๐ด๐ต๐ ๐ญ๐ฌ๐ฑ was a scheduled domestic passenger flight from Milwaukee to Atlanta, operated by a McDonnell Douglas DC-9 (Reg. N100ME) on ๐ฆ๐ฒ๐ฝ๐๐ฒ๐บ๐ฏ๐ฒ๐ฟ ๐ฒ, ๐ญ๐ต๐ด๐ฑ.
Flight 105 was cleared for takeoff at 15:20:28. At 15:21:26 the plane was about 7,600 feet down the runway, reaching a height of 450 feet above the ground. At that moment there was a loud noise and a noticeable decrease in engine sound. The captain then remarked "What the # was that?" At 15:21:29, the local controller transmitted, "Midex 105, turn left heading 175." At the time of his transmission he observed smoke and flame emanating from the right engine. The captain asked the first officer, "What do we got here, Bill?" The first officer did not respond to the captain but advised the local controller, "Midex 105, roger, we've got an emergency here."
Two seconds later, the captain said, "Here"; again there was no response. Neither pilot made the call outs for "Max Power" or "Ignition Override-Check Fuel System," which were part of the airline's "Engine Failure after V1" emergency procedure. Meanwhile, the plane began to deviate substantially to the right and the heading changed from 194ยฐ to 260ยฐ in 8 seconds. At that point the plane stalled at a speed of 156 KIAS, barrel-rolled at least once, and crashed into an open field in a wildlife preserve just several hundred meters from runway 19R.
๐ฃ๐ฟ๐ผ๐ฏ๐ฎ๐ฏ๐น๐ฒ ๐๐ฎ๐๐๐ฒ:
"The flight crew's improper use of flight controls in response to the catastrophic failure of the right engine during a critical phase of flight, which led to an accelerated stall and loss of control of the airplane. Contributing to the loss of control was a lack of crew coordination in response to the emergency. The right engine failed from the rupture of the 9th to 10th stage removable sleeve spacer in the high pressure compressor because of the spacer's vulnerability to cracks."
Credits: @elsopaipilla315
Accident Description: instagram.com/p/CiKyEcyBK9t/?igsh=dmVyaGd0dGJjYjF3
Photos Archive:
https://x.com/aircrashdaily/status/1567157752040157184?s=19
๐ ๐ถ๐ฑ๐๐ฒ๐๐ ๐๐ ๐ฝ๐ฟ๐ฒ๐๐ ๐๐น๐ถ๐ด๐ต๐ ๐ญ๐ฌ๐ฑ was a scheduled domestic passenger flight from Milwaukee to Atlanta, operated by a McDonnell Douglas DC-9 (Reg. N100ME) on ๐ฆ๐ฒ๐ฝ๐๐ฒ๐บ๐ฏ๐ฒ๐ฟ ๐ฒ, ๐ญ๐ต๐ด๐ฑ.
Flight 105 was cleared for takeoff at 15:20:28. At 15:21:26 the plane was about 7,600 feet down the runway, reaching a height of 450 feet above the ground. At that moment there was a loud noise and a noticeable decrease in engine sound. The captain then remarked "What the # was that?" At 15:21:29, the local controller transmitted, "Midex 105, turn left heading 175." At the time of his transmission he observed smoke and flame emanating from the right engine. The captain asked the first officer, "What do we got here, Bill?" The first officer did not respond to the captain but advised the local controller, "Midex 105, roger, we've got an emergency here."
Two seconds later, the captain said, "Here"; again there was no response. Neither pilot made the call outs for "Max Power" or "Ignition Override-Check Fuel System," which were part of the airline's "Engine Failure after V1" emergency procedure. Meanwhile, the plane began to deviate substantially to the right and the heading changed from 194ยฐ to 260ยฐ in 8 seconds. At that point the plane stalled at a speed of 156 KIAS, barrel-rolled at least once, and crashed into an open field in a wildlife preserve just several hundred meters from runway 19R.
๐ฃ๐ฟ๐ผ๐ฏ๐ฎ๐ฏ๐น๐ฒ ๐๐ฎ๐๐๐ฒ:
"The flight crew's improper use of flight controls in response to the catastrophic failure of the right engine during a critical phase of flight, which led to an accelerated stall and loss of control of the airplane. Contributing to the loss of control was a lack of crew coordination in response to the emergency. The right engine failed from the rupture of the 9th to 10th stage removable sleeve spacer in the high pressure compressor because of the spacer's vulnerability to cracks."