No fatalities

1966-04-15: Lockheed C-130 Hercules (10304) — Royal Canadian Air Force - RCAF — North Battleford, Canada

North Battleford, CanadaFlight

On April 15, 1966, a Lockheed C-130 Hercules (registration 10304) operated by Royal Canadian Air Force - RCAF was involved in an aviation accident near North Battleford, Canada in flight. No fatalities were reported. Investigators recorded the probable cause as: The door opened in flight and detached due to material failure and maintenance error. The number 1 eyebolt fractured from overloading, exacerbated by a pre-existing crack from rough machining and likely misalignment during door rigging. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781241132Data APIEditorial standards

A cargo door detached in flight from an aircraft en route from Rivers AFB, Manitoba, to North Battleford. The crew performed a belly landing in a field; no injuries occurred. The aircraft was damaged beyond repair. Investigation cited material failure and maintenance error.

Accident Overview

On a flight from Rivers Air Force Base in Manitoba to North Battleford, a technical failure occurred involving the front cargo door. The door detached in flight, prompting the crew to reduce altitude and attempt an emergency landing. The aircraft executed a belly landing in a field near North Battleford, slid several yards, and came to rest. No injuries were reported among the crew, but the aircraft was considered damaged beyond repair. After the accident, engine number one could not be stopped, likely due to debris impact.

Incident Sequence

During the flight, the front cargo door unexpectedly opened and separated from the aircraft. The crew responded by lowering altitude and initiating an emergency landing procedure. The belly landing was carried out in a field, where the aircraft slid before stopping. Post-accident, engine number one continued running uncontrollably, suspected to have been struck by debris from the door detachment.

Investigation Findings

Investigators determined that the door opened in flight, detached, and was later found 15 miles from the accident site. The cause was attributed to both material failure and maintenance error. The latching mechanism consisted of four eyebolts; failure occurred when the number 1 eyebolt ruptured due to over-stressing, subsequently causing the number 2 eyebolt to fail as the load was transferred. The number 1 eyebolt had been cracked for some time, with only two-thirds of its cross-sectional area carrying the load at the time of failure. Analysis indicated that both the initial crack and the ultimate failure resulted from overloading, with rough machining during manufacture contributing to crack formation. Misalignment during door rigging was strongly suspected as the source of the overload.

Probable cause

The door opened in flight and detached due to material failure and maintenance error. The number 1 eyebolt fractured from overloading, exacerbated by a pre-existing crack from rough machining and likely misalignment during door rigging.