1 fatality

1972-06-22: Beechcraft E18 (N42A) — Quaker City Airways — Cleveland-Hopkins, United States of America

Cleveland-Hopkins, United States of AmericaTakeoff (climb)

On June 22, 1972, a Beechcraft E18 (registration N42A) operated by Quaker City Airways was involved in an aviation accident near Cleveland-Hopkins, United States of America during takeoff. One person was killed. Investigators recorded the probable cause as: Structural failure and detachment of the left wing during initial climb and uncontrolled descent due to the presence of fatigue cracks. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 1 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781233954Data APIEditorial standards

Shortly after liftoff, the aircraft's left wing separated during initial climb. The uncontrolled airplane crashed, resulting in a post-impact fire and destruction. The sole pilot was killed. Fatigue cracks and inadequate maintenance inspection were cited.

Incident Description

Just after liftoff, while in the initial climb phase, the left wing of the aircraft detached. The airplane, now out of control, descended and crashed. The impact and subsequent post-crash fire destroyed the aircraft. The pilot, who was the sole occupant, was killed.

Investigation Findings

The official investigation determined that the accident resulted from a structural failure and detachment of the left wing during initial climb and uncontrolled descent. This failure was attributed to the presence of fatigue cracks. The investigation also identified contributing factors: inadequate inspection of the aircraft by maintenance personnel, the wing spars, fatigue fracture, the left wing's failure and upward folding, and the presence of a fatigue crack that had existed during a prior inspection but was not detected.

Probable cause

Structural failure and detachment of the left wing during initial climb and uncontrolled descent due to the presence of fatigue cracks. Factors: inadequate inspection of the aircraft on part of the maintenance personnel, wings spars, fatigue fracture, left wing failed, folded up, fatigue crack was present during prior inspection but was not detected.