Casualties unknown

2003-05-22: Bellanca 7GCBC (N68567) — T. Brill — Reno, NV

Reno, NV, US

On May 22, 2003, a Bellanca 7GCBC (registration N68567) operated by T. Brill was involved in an aviation accident near Reno, NV. Investigators recorded the probable cause as: a loss of engine power for undetermined reasons. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

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

A training flight ended in a hard landing after engine power loss during climb. The left main landing gear sheared off. Post-accident examination found a restriction in the mixture control arm travel.

Incident Summary

A certified flight instructor and a student pilot experienced a loss of engine power during the initial climb after takeoff, resulting in a hard landing. The accident occurred when the airplane was on a training flight from an airport. The instructor decided to attempt a return to the runway after the engine failed completely. The airplane touched down while still in a turn, causing the left main landing gear to shear off. The airplane slid to a stop in gravel on the south side of the runway.

Flight Details

Before departure, the flight instructor added 10 gallons of fuel to the airplane. The instructor and student then taxied to the hold short line and completed an uneventful run-up for runway 26. The airplane rotated at 60 miles per hour (mph) indicated airspeed (IAS), and the instructor instructed the student to pitch for the best rate of climb speed. At approximately 500 feet above ground level (agl), as the student was turning crosswind, the engine "coughed." The flight instructor told the student to apply full throttle and mixture; the tachometer then read 2,100 rpm. The engine coughed again, and the rpm decreased to 1,500 rpm. Subsequently, the engine completely lost power. The flight instructor decided to try to return to the runway. The airplane was in a right turn at 500 feet agl. As the airplane approached runway 8, the airspeed was 61 mph IAS. The airplane touched down on the runway, still in the turn, resulting in the left main landing gear shearing off.

Engine Examination

Post-accident examination of the engine revealed that the mixture control arm could not reach the "FULL RICH" position. This anomaly could not be explained by impact damage. Considering the elevation of the airport and the likely 7,600-foot density altitude, investigators were uncertain about the relationship between the mixture control travel limit and the loss of engine power. No other discrepancies were noted with the engine.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20030609X00819. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.