Casualties unknown

2000-08-15: Cessna 152 (N93589) — Philair Flight Center, Inc. — Gainesville, FL

Gainesville, FL, US

On August 15, 2000, a Cessna 152 (registration N93589) operated by Philair Flight Center, Inc. was involved in an aviation accident near Gainesville, FL. Investigators recorded the probable cause as: The flight instructor's failure to identify a partial loss of engine power during takeoff roll, and his failure to maintain airspeed while attempting to return to the airport after takeoff resulting in the airplane stalling and descending uncontrolled until… 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 flight instructor and student experienced engine power loss during climb after takeoff. The instructor attempted a return but landed in trees. Postcrash examination revealed fouled spark plugs and a bent propeller.

Incident Overview

During climb after takeoff, the engine lost power and the rpm dropped to about 2,100. The flight instructor, who was with a student, took control and initiated a left turn back toward the airport. When he realized he could not make the airport, he landed in trees.

Witness Observations

A witness stated that the engine did not sound like it was producing full power from the beginning of the takeoff roll. The airplane used approximately two-thirds of the 4,158-foot runway during the takeoff roll. After liftoff, the airplane climbed slowly and the pilot initiated a left turn with a nose-high attitude. The airplane stalled, the left wing dropped, and the aircraft descended and crashed into trees. The witness heard the engine continue to run until impact.

Postcrash Examination

Postcrash examination of the engine showed the spark plugs were fouled with carbon and lead deposits, and the propeller blades were bent forward. The engine was started and operated roughly to 1,700 rpm. After cleaning the spark plugs and replacing the bent propeller, the engine was started and operated to 2,200 rpm, achieving full static rpm.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X21799. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.