Narrative:Mohawk Flight 40 took off from Elmira at 14:39 EDT for a flight to Washington, DC. At 14:44 the aircraft was cleared to climb to FL160. Eyewitnesses observed the aircraft a little later near Blossburg when large sections of the tail separated from the aircraft in flight, after which fire and smoke emitted from the tail as the aircraft dove into the ground.
Probable Cause:
PROBABLE CAUSE: "The loss of integrity of empennage pitch control systems due to a destructive in-flight fire which originated in the airframe plenum chamber, fueled by hydraulic fluid, progressed up into the vertical tail fin. The fire resulted from engine bleed air flowing back through the malfunctioning nonreturn valve and an open air delivery valve, through the auxiliary power unit in a reverse direction, and exiting into the plenum chamber at temperatures sufficiently high to cause the acoustics linings to ignite."
Accident investigation:
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Investigating agency: | NTSB  |
Status: | Investigation completed |
Duration: | 300 days (10 months) | Accident number: | NTSB File No.1-0004 | Download report: | Final report
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Classification:
Inflight fire
Wing failure
Loss of control
Follow-up / safety actions
FAA issued 1 Airworthiness Directive
NTSB issued 3 Safety Recommendations
Issued: 25-JUL-1967 | To: | N1116J (1) |
It is recommended that a fireproof barrier of appropriate width be provided at the top fuselage skin between Fuselage Stations 936 and 958 in order to provide effective isolation of the vertical fin, particularly the area aft of the rear spar wherein is located electrical circuits, hydraulic lines and mechanical devices for directional and longitudinal control. (Closed - Acceptable Action) |
Issued: 25-JUL-1967 | To: | N1116J (2) |
It is recommended that the aluminum alloy wall separating the hydraulics bay and the airframe plenum chamber be replaced with a suitable fire-proof material. (Closed - Acceptable Action) |
Issued: 25-JUL-1967 | To: | N1116J (3) |
It is recommended that inflight use of the APU be restricted as a precautionary measure until such time as the suitable barriers recommended above are provided. (Closed - Acceptable Action) |
Issued: 03-JAN-1968 | To: BAC 1-11-200, -400 | AD 68-01-01 |
Measures to prevent heat damage or fire in the airframe plenum of the auxiliary power unit (APU) installation. |
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Photos
Map
This map shows the airport of departure and the intended destination of the flight. The line between the airports does
not display the exact flight path.
Distance from Elmira Regional Airport, NY to Washington-National Airport, DC as the crow flies is 365 km (228 miles).
Accident location: Exact; as reported in the official accident report.
This information is not presented as the Flight Safety Foundation or the Aviation Safety Network’s opinion as to the cause of the accident. It is preliminary and is based on the facts as they are known at this time.