Casualties unknown

Piper J3C HB-ONB Accident near Staad SG on 19 May 1962

Staad, SG, CH

On May 18, 1962, a PIPER AIRCRAFT CORPORATION J3C-65/L-4. (registration HB-ONB) was involved in an aviation accident near Staad, SG, CH. Investigators recorded the probable cause as: Engine failure due to defects in the recently modified fuel system. 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

On 19 May 1962, during water conversion training, a Piper J3C HB-ONB suffered an engine failure on the 21st takeoff. The aircraft stalled and was heavily damaged; the two occupants were not injured. The engine failure was attributed to defects in the fuel system after an engine upgrade.

Background

The aircraft, a Piper J3C (registration HB-ONB), was originally equipped with a 65 hp Continental engine. In spring 1962, the owner commissioned Airbase GmbH in Zürich to replace the engine with a 90 hp Continental. The conversion required modifications, and the firm, lacking documentation, devised its own solution, including changes to the fuel system. The work was completed on 16 May 1962.

Pre-accident Events

On 15 May, Airbase notified the Swiss Air Office of the modification. The Air Office instructed the airfield chief at Altenrhein to conduct the inspection. The inspection on 16 May was interrupted and later concluded, allowing a test flight on 17 May. No anomalies were reported. After weighing, the aircraft was returned to Altenrhein. The outstanding inspection was deferred.

On 19 May, a flight instructor and his student arrived for water flying conversion training at Lake Constance. The instructor provided theoretical instruction before flights began.

Accident

During the 21st takeoff at 1924 MEZ, the engine unexpectedly stopped. The student, seeing a harbor wall ahead, initiated a turn, causing the aircraft to stall. It struck the water heavily and was severely damaged. Both occupants were uninjured.

Investigation

The investigation focused on the fuel system modifications. It was found that the fuel filter was no longer at the lowest point, and the fuel lines had upward bends above the connection points, which could trap air or affect fuel flow. The engine failure was attributed to these defects in the modified fuel system.

Probable cause

Engine failure due to defects in the recently modified fuel system.

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/83.pdf. This page is a structured re-presentation; facts and quotes are in the Swiss Transportation Safety Investigation Board (STSB), Switzerland.