Casualties unknown

1999-08-21: Bellanca 7ECA (N88408) — Attitude Aviation — Livermore, CA

Livermore, CA, US

On August 21, 1999, a Bellanca 7ECA (registration N88408) operated by Attitude Aviation was involved in an aviation accident near Livermore, CA. Investigators recorded the probable cause as: The number 3 exhaust valve was broken, and the head was embedded in the piston, resulting in a partial loss of engine power. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 3 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 takeoff climb, a partial loss of power occurred with rpm dropping to 1,500 and engine roughness. The CFI took control, performed a 180-degree turn, and landed hard on a taxiway. Examination revealed a broken number 3 exhaust valve embedded in the piston.

Event

During the initial climb after takeoff, the aircraft experienced a partial loss of power. The engine's revolutions per minute (rpm) decreased to 1,500, accompanied by roughness. The certified flight instructor (CFI) took control from the student pilot, executed a 180-degree turn back toward the runway, and landed hard on a taxiway.

Both pilots reported no discrepancies during preflight, engine start, taxi, or run-up.

Engine Examination

Post-incident examination of the engine revealed that the number 3 exhaust valve was broken, and the valve head was found embedded in the piston.

Maintenance History

Review of the engine logbook showed that the engine had accumulated 3,711.0 hours since its last major overhaul, which occurred on November 30, 1993. According to the engine manufacturer, the maximum recommended time between overhauls is 2,400 hours or 12 calendar years.

A Lycoming Mandatory Service Bulletin addresses the need to inspect exhaust valves and valve guides to prevent sticking and possible failure due to excessive guide wear. The bulletin recommends inspections at 400-hour intervals. No record of compliance with this bulletin was found in the logbooks.

Probable cause

The number 3 exhaust valve was broken, and the head was embedded in the piston, resulting in a partial loss of engine power.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X19562. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.