Incident Overview
During maneuvering near a refueling site in hilly and mountainous terrain, the 90-degree gearbox separated from the aircraft. The pilot subsequently attempted a run-on forced landing on a nearby logging road.
Landing and Post-Impact Damage
During the flare, the aircraft landed hard. The impact resulted in a collapse of the skids and separation of the remaining portion of the tail boom.
Metallurgical Findings
Metallurgical analysis of the gearbox attach bolts revealed that all six bolts had experienced reverse-bending fatigue failure.
Component History
Operator records indicated that the gearbox was a new surplus part that had accumulated 136 hours of operation since new. Historical records that would confirm the unit's total time since being shipped to the Philippines as a new surplus part in 1981 could not be located.