Casualties unknown

2000-07-04: Cessna 152 (N89043) — Murfreesboro, TN

Murfreesboro, TN, US

On July 4, 2000, a Cessna 152 (registration N89043) was involved in an aviation accident near Murfreesboro, TN. Investigators recorded the probable cause as: the flight instructor's failure to maintain an airspeed above the aircraft's stall speed, which resulted in a stall/mush, and an inflight loss of control while maneuvering to return to a landing area during an emergency, resulting in an uncontrolled descent… 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

During a student's third lesson and first flight in a Cessna 152, the aircraft failed to climb after takeoff. The instructor took control and initiated a turn, during which the stall warning sounded. The aircraft then descended. No mechanical issues were found.

Accident Overview

A student pilot on his third flight lesson was flying a Cessna 152 for the first time. He reported that after takeoff, at an altitude of approximately 50 to 100 feet, the aircraft seemed to lack sufficient power to continue climbing. The engine was developing normal rpm and sounded normal, with no malfunction detected. The flight instructor immediately assumed control and turned the aircraft back toward the airport. During the turn, the stall warning horn activated, and the aircraft subsequently descended.

Aircraft Information

The aircraft was a Cessna 152. According to the student, he chose this model because it was less expensive than the Cessna 172 he had previously flown. He believed the fuel tanks had been topped off before the flight.

Investigation

Witnesses confirmed the engine was operating at impact. Post-accident examination of the aircraft and engine revealed no mechanical failure or malfunction in any system. The flaps were found set at 20 degrees. A post-accident analysis calculated the aircraft weight at approximately 1,713 pounds and the density altitude at about 2,000 feet. Two propeller slash marks at the scene, 14 inches apart, indicated a ground speed of about 41 knots and an engine speed of approximately 1,774 rpm at impact.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X21529. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.