Piper Cub L4A Crash During Training Landing

Casualties unknown • Militärflugplatz, CH

A Piper Cub L4A sustained heavy damage after a student pilot lost control during a towed landing at a military airfield.

What happened

On May 8, 1965, a Piper Cub L4A, registration HB-ODN, was involved in an accident during a training maneuver at a military airfield. The aircraft was performing a towed landing, a procedure used for flight instruction, when the pilot lost control of the aircraft's flight path.

The investigation

The investigation established the sequence of events leading to the impact. During the landing phase, the student pilot attempted to manage the aircraft's descent by simultaneously applying a correction to the elevator and reducing engine power. This combination of inputs caused the aircraft to lose sufficient lift and sink toward the ground.

Findings

As the aircraft descended, it struck the ground and subsequently overturned. The primary cause of the accident was the simultaneous application of altitude control corrections and power reduction by the student pilot, which resulted in the aircraft dropping abruptly to the surface.

Results

The pilot involved in the incident escaped without any injuries. However, the Piper Cub L4A suffered significant structural damage, estimated at approximately 25 percent of its total value.

Probable cause

The student pilot's simultaneous reduction of engine power and manual elevator correction caused the aircraft to lose altitude rapidly and capsize during a towed landing.

Frequently asked questions

What happened in the 1965-05-08 PIPER AIRCRAFT CORPORATION J3C-65/L-4. accident near Militärflugplatz, CH?

A Piper Cub L4A sustained heavy damage after a student pilot lost control during a towed landing at a military airfield.

What aircraft was involved and where did it happen?

The accident on 1965-05-08 involved a PIPER AIRCRAFT CORPORATION J3C-65/L-4., registration HB-ODN, at Militärflugplatz, CH.

What was the probable cause of the accident?

The student pilot's simultaneous reduction of engine power and manual elevator correction caused the aircraft to lose altitude rapidly and capsize during a towed landing.

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/250.pdf. This page is a structured re-presentation; facts and quotes are in the Swiss Transportation Safety Investigation Board (STSB), Switzerland.

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