Casualties unknown

Piper L-4 HB-OGZ Accident at Lommis on 4 October 1962

Lommis Flugplatz (LSZT), TG, CH

On October 4, 1962, a PIPER AIRCRAFT CORPORATION J3C-65/L-4. (registration HB-OGZ) was involved in an aviation accident near Lommis Flugplatz (LSZT), TG, CH. Investigators recorded the probable cause as: The accident is due to a sharp drop in engine power during takeoff; its cause could no longer be determined. This summary draws on records from the Swiss Transportation Safety Investigation Board (STSB / SUST).

Sourcesthe Swiss Transportation Safety Investigation Board (STSB / SUST)Primary reportUpdated 2026-09-13Data APIEditorial standards

A Piper L-4 (HB-OGZ) experienced a sharp drop in engine power shortly after takeoff at Lommis airfield. The aircraft overran the field, jumped a stream, and was seriously damaged; both occupants were uninjured. The cause of the power loss could not be determined.

Accident Overview

On Thursday, 4 October 1962, at approximately 1515 MEZ, a Piper L-4 (registration HB-OGZ) departed from Lommis airfield in the canton of Thurgau, Switzerland, for a private flight. The pilot, born in 1941, held a private pilot license issued on 5 May 1960, valid until 23 December 1962, with about 70 total flying hours, of which 60 were on type. His passenger, born in 1903, was his father and had no aviation experience.

Flight and Accident

After a normal warm-up and preparation, the pilot took off from the dry grass runway, which was 525 meters long. The aircraft lifted off in the second half of the runway normally. The pilot intentionally kept the aircraft low to gain speed, but at that point engine power dropped significantly. Moving the throttle had no effect, forcing an immediate landing. The aircraft overran the airfield boundary, jumped a stream about eight meters wide and 2.5 meters deep located 150 meters west of the runway end, and came to rest on its belly in the takeoff direction. The landing gear was sheared off during the stream crossing.

Damage and Injuries

Both occupants were uninjured. The aircraft sustained serious damage. Before the investigator arrived, the wreckage was recovered and the engine was run on the ground by private parties; no discrepancies were found. The same engine subsequently flew about 20 hours without any issues.

Investigation

The investigation found no pre-existing condition to explain the power loss. The weather was fine with a temperature of 20°C and relative humidity of 60%. The runway was dry. The aircraft was a Piper Cub J-3/L-4 built in 1944, with a 65 hp Continental A-65 engine and a wooden propeller. It was owned by the Motorfluggruppe of the Thurgau section of the Aero-Club of Switzerland and had a valid permit to fly until 18 June 1963.

Discussion

The commission considered possible causes such as carburetor icing or insufficient fuel flow, but given the temperature and humidity, carburetor icing was unlikely. Other possibilities included a fuel shutoff valve not fully open or a temporary blockage of the carburetor jet by debris or water. However, no definitive evidence supported any specific cause.

Conclusion

The investigation commission concluded unanimously that the accident was caused by a sharp drop in engine power during takeoff, but the exact reason for the power loss could not be determined.

Probable cause

The accident is due to a sharp drop in engine power during takeoff; its cause could no longer be determined.

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/85.pdf. This page is a structured re-presentation; facts and quotes are in the Swiss Transportation Safety Investigation Board (STSB), Switzerland.