Casualties unknown

1992-08-03: Cessna 152 (N49016) — Action Technical Associates — Maricopa, AZ

Maricopa, AZ, US

On August 3, 1992, a Cessna 152 (registration N49016) operated by Action Technical Associates was involved in an aviation accident near Maricopa, AZ. Investigators recorded the probable cause as: THE PILOT EXCEEDED THE DESIGN STRESS LIMITS OF THE AIRPLANE STRUCTURE BY ATTEMPTING AN ABRUPT MANEUVER AT A SPEED IN EXCESS OF THE MANEUVERING SPEED. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

A pilot renting an airplane for ground reference maneuvers in VMC conditions experienced a structural failure. The lower wing strut attach points failed due to overstress, with calculations indicating an airspeed of 153.2 mph was needed to generate the load. No eyewitnesses were present.

Accident Summary

There were no eyewitnesses to the accident. According to the operator, the pilot rented the airplane to practice ground reference maneuvers in the south practice area. The weather was VMC, and other pilots flying in the vicinity reported no significant weather phenomena.

Pilot Information

Twelve months prior to the accident, at the pilot's third-class medical certificate renewal, he reported 480 total flight hours with no hours in the preceding six months. According to flight school records, he received about 2.7 hours of dual instruction and a biennial flight review after his medical. The pilot then flew solo through July 7, 1992, for about 8.7 hours.

Structural Failure Analysis

According to the metallurgist's factual report, the wings lower strut attach points failed due to overstress. Cessna Aircraft tested a 150K fuselage during certification work on the A152 model and found that the lower lift strut attach fitting failed at 8.28 G's. Engineers calculated that an airspeed of 153.2 mph was required at gross weight to generate the 8.28 G load which caused the strut attach failure. The maneuvering speed for the aircraft is 103 mph.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001211X15427. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.