34 fatalities

1967-06-23: BAc 111 (N1116J) — Mohawk Airlines — Blossburg, United States of America

Blossburg, United States of AmericaTakeoff (climb)

On June 23, 1967, a BAc 111 (registration N1116J) operated by Mohawk Airlines was involved in an aviation accident near Blossburg, United States of America during takeoff. 34 people were killed. Investigators recorded the probable cause as: 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. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 3 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781239820Data APIEditorial standards
Aircraft registered N1116J
Aircraft registered N1116J. Photo: Original Photographer Unknown / Public domain, via Wikimedia Commons

A scheduled flight from Elmira to Washington crashed near Blossburg, PA, after entering a nose-down descent. Official investigation found an in-flight fire in the empennage pitch control systems due to overheated engine bleed air igniting acoustic linings.

Incident Overview

On the day of the accident, a commercial aircraft departed Elmira-Corning Airport at 1439 local time on a scheduled flight to Washington-National Airport. The flight carried 30 passengers and a crew of four. After takeoff, air traffic control cleared the crew to climb to flight level 160. Shortly thereafter, the airplane assumed a nose-down attitude, plunged into the earth, and crashed with a massive explosion in a wooded area located one mile east of Blossburg, Pennsylvania. The aircraft disintegrated on impact, and none of the 34 occupants survived.

Investigation Findings

The official investigation determined the probable cause of the accident. According to the final report, the crash resulted from the loss of integrity of empennage pitch control systems. This loss was caused by a destructive in-flight fire that originated in the airframe plenum chamber. The fire was fueled by hydraulic fluid and progressed upward into the vertical tail fin.

Origin of the Fire

The fire itself originated from engine bleed air flowing back through a malfunctioning non-return valve and an open air delivery valve. This reverse flow passed through the auxiliary power unit and exited into the plenum chamber at temperatures sufficiently high to ignite the acoustic linings. The resulting fire compromised the aircraft's pitch control systems, leading to the loss of control and subsequent crash.

Aftermath

Emergency responders arrived at the crash site to find the wreckage scattered across the wooded area. The impact and ensuing fire left no survivors. The investigation concluded without any additional causal factors beyond those stated. The accident remains a significant event in aviation safety history.