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NTSB investigation record

WPR09CA030

Completed

Piper Pa-38-112· N2346G

NTSB Report
Date
October 31, 2008
Location
Friant, CA
Conditions
VMC
Record
Published September 25, 2020

Primary finding

Probable cause

The student pilot's failure to execute a go-around in timely manner, which resulted in a collision with terrain. Also causal was the instructor's inadequate supervision of the flight and delayed remedial actions.

Investigator assessment

Analysis narrative

The purpose of the dual instructional flight was for the student pilot to practice simulated engine failures under the direction of his certified flight instructor (CFI). After completing three simulated engine failures without mishap, and the student setup for a fourth attempt. The airplane descended to about 100 feet above ground level (agl) and the student configured the airplane for a go-around by adding power and pitching the nose upward. Several seconds later the airplane collided with terrain. The CFI stated that accident could have been prevented if the go-around was initiated at a higher altitude. The CFI further added that there were no preimpact mechanical malfunctions or failures with the airframe or engine.

Source record

Factual narrative

In a written statement, the certified flight instructor (CFI) reported that the purpose of the flight was for the student pilot to practice simulated engine failures. The flight proceeded to mountainous area about 15 miles from the base airport. Three simulated engine failures were performed without mishap and the student setup for a fourth attempt. The airplane descended to about 100 feet above ground level (agl) and the student configured the airplane for a go-around by adding power and pitching the nose upward. Several seconds later the airplane collided with terrain. In the section titled "RECOMMENDATION" in the NTSB Pilot/Operator Report, form 6120.1/2, the CFI stated that accident could have been prevented if the go-around was initiated at a higher altitude. The CFI further added that there were no preimpact mechanical malfunctions or failures with the airframe or engine.

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