Casualties unknown

2000-04-14: Piper PA-28-161 (N81019) — Palo Alto Flying Club — Palo Alto, CA

Palo Alto, CA, US

On April 14, 2000, a Piper PA-28-161 (registration N81019) operated by Palo Alto Flying Club was involved in an aviation accident near Palo Alto, CA. Investigators recorded the probable cause as: The loss of engine power for undetermined reasons during takeoff climb. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 15 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 post-maintenance test flight, an airplane's engine lost power twice during climb out at 300 ft. The pilot attempted to return but landed short in a marsh. Subsequent examination found no mechanical anomalies, and the engine ran normally after replacement of the propeller and removal of the damaged carburetor heat box.

Incident Overview

Following an engine oil change, the operator's practice was to conduct a test flight before releasing the aircraft for student use. The pilot, a flight instructor, reported that the engine start, taxi, and run-up were normal. The engine operated smoothly during the initial climb, but at approximately 300 feet above ground level (agl) during the takeoff climb, the engine abruptly quit. Power was regained momentarily, then lost again.

Forced Landing

Unable to sustain flight, the pilot attempted to return to the departure runway but landed short in a marsh area. At the accident site, the propeller did not appear to have been rotating at the moment of impact.

Post-Accident Examination

Investigators noted fuel in both wing tanks, and fuel samples from the sumps showed no contamination. Emergency responders had instructed the pilot to turn the fuel selector to the 'off' position; the fuel pump functioned audibly. The engine contained clean oil, rotated freely, and exhibited good compression. After recovery, the cowling was removed, and a thorough examination of the engine revealed no anomalies. The propeller was replaced, and the carburetor heat box was removed because it was damaged.

Engine Run Test

Following the replacement of the propeller and removal of the damaged carburetor heat box, the engine was started promptly. It ran normally during the run-up and delivered full power. No further issues were encountered.

The source does not specify a probable cause for the power loss.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X20853. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.