Forced landing following simulated engine failure and gear malfunction

Casualties unknown • Las Cruces, NM, US

A flight instructor and student were involved in a forced landing on desert terrain after an engine power loss occurred during a simulated emergency procedure.

What happened

During an approach, the flight instructor (CFI) initiated a training maneuver by simulating a loss of power in the right engine. As part of this simulation, the CFI pulled the circuit breaker for the normal landing gear extension system. The student attempted to extend the landing gear using the alternate system; however, the left gear failed to reach the down-and-locked position.

The instructor attempted to reset the situation by reinserting the circuit breaker and cycling the gear, but the left gear remained unlatched. Due to the gear malfunction, the CFI ordered a go-around. At approximately 300 feet above ground level (AGL), the crew advanced the throttles, at which point the instructor noted an actual lack of power in the right engine and took control of the aircraft.

While the instructor attempted to restore full power to the right engine, the engine produced only limited thrust. The propeller was not feathered. Although the aircraft initially maintained level flight, it was unable to climb and eventually began to descend. This resulted in a forced landing on rough desert terrain. There were no injuries reported.

The investigation

A subsequent investigation was conducted to determine why the right engine lost power. Investigators found no reason for the reported loss of engine power.

Frequently asked questions

What happened in the 1989-01-24 Piper PA-34-200T accident near Las Cruces, NM?

A flight instructor and student were involved in a forced landing on desert terrain after an engine power loss occurred during a simulated emergency procedure.

What aircraft was involved and where did it happen?

The accident on 1989-01-24 involved a Piper PA-34-200T, registration N3070M, at Las Cruces, NM.

What was the probable cause of the accident?

THE LOSS OF RIGHT ENGINE POWER FOR UNDETERMINED REASON(S), AND THE FAILURE OF THE INSTRUCTOR PILOT TO FEATHER THE RIGHT ENGINE. FACTORS RELATED TO THE ACCIDENT WERE: FAILURE OF THE LEFT MAIN GEAR LOCKING MECHANISM TO ENGAGE AND THE UNPREPARED (ROUGH/UNEVEN) TERRAIN.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001213X27577. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.

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