Casualties unknown

Wing Spar Fracture During Takeoff Results in Collision with Tree (N731PP)

Houston, MS, US

On March 24, 1983, a Cessna 188B (registration N731PP) was involved in an aviation accident near Houston, MS. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-06-10Data APIEditorial standards

A pilot experienced a loss of altitude and airspeed after feeling the aircraft 'give' during flap retraction at 100 ft AGL. Examination revealed a rusted fracture of the right wing rear spar at a welded joint, where prior damage had been repaired.

Pilot Report

The pilot reported that during takeoff, after reaching an altitude of approximately 100 feet above ground level (AGL), he reduced power and began retracting the flaps from the takeoff setting. At that moment, he felt the aircraft 'give.' He immediately re-extended the flaps, applied full throttle, and dumped his load, but the aircraft continued to lose altitude and airspeed until it struck the top of a tree and crashed.

Post-Crash Examination

An examination of the wreckage revealed that the top member of the right wing tubular rear spar was broken at the cluster joint where the spar attaches to the fuselage stub wing. The fracture surfaces were severely rusted. The fracture occurred where the wing had been welded.

History

Reportedly, the right wing tip had been damaged approximately three years prior to the accident and was subsequently repaired.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001214X42347. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.