Supriya Ghosh (Editor)

TWA Flight 400

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Survivors
  
14

Registration
  
N40403

Operator
  
Trans World Airlines

Survivor
  
14

Location
  
Moon

Aircraft type
  
Martin 4-0-4

Date
  
1 April 1956

Fatalities
  
22 (passengers:21 crew:1)

Passenger count
  
33

Summary
  
Mechanical failure followed by pilot error

Site
  
Moon Township, Allegheny County, near Pittsburgh, Pennsylvania

Flight origin
  
Pittsburgh International Airport, PA (PIT/KPIT)

Similar
  
TWA Flight 513, 1965 Carmel mid‑air co, TWA Flight 903, TWA Flight 159, TWA Flight 599

On April 1, 1956, a Martin 4-0-4, registration #N40403, operating as TWA Flight 400, crashed on takeoff from Greater Pittsburgh International Airport (PIT). Twenty-two of the 36 people aboard the aircraft, including one crewmember, perished in the crash.

Flight 400 was to be an IFR flight to Newark International Airport (EWR) in Newark, NJ. On this particular flight, the first officer was in the left seat, as he was being line-checked by the captain. As the aircraft became airborne, a sharp yaw was experienced while the first officer reduced power at an altitude of approximately 100 feet (30 m). Almost immediately, the fire warning light for the number one engine illuminated, however, the fire warning bell never sounded. At this point, the first officer most likely throttled down the number one engine. The captain had only noted the loss of power shown by the BMEP gauge, but never saw the fire warning light. He pulled the mixture to idle cutoff. As the first officer reached for the manual feathering button, the captain stopped him. The captain indicated that the autofeather device would feather the no. 1 prop. This never occurred, due to the throttle lever being retarded to a position aft of the switches that arm the auto-feathering system. The no. 1 prop created sufficient drag, causing the aircraft to continue to yaw to the left. At only 1,690 feet (515 m) past the runway's end, at 7:20 PM, the aircraft crashed.

The fire warning appears to have been caused by an exhaust connector clamp failure. Hot exhaust gases were blown directly onto an overheat detector.

Probable cause of the crash has been determined as: "Uncoordinated emergency action in the very short time available to the crew, which produced an aircraft configuration with insurmountable drag".

References

TWA Flight 400 Wikipedia