Casualties unknown

Accident Involving Piper PA-18-150 HB-OZE During Glider Tow near Gaissau, Austria

Gaissau/AUT, CH

On April 30, 1978, a PIPER AIRCRAFT CORPORATION PA-18 "150" (registration HB-OZE) was involved in an aviation accident near Gaissau/AUT, CH. Investigators recorded the probable cause as: Glider flying higher than the towplane. Contributing factor: use of center-of-gravity tow hook combined with the glider pilot's low experience on the type. 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 30 April 1978, a Piper PA-18-150 towing a glider crashed near Gaissau, Austria, after the glider flew higher than the towplane, causing the towplane to pitch down. The pilot was killed; the glider landed safely.

General Information

The accident involved a Piper PA-18-150, registration HB-OZE, owned and operated by Segelfluggruppe Säntis of St. Gallen, Switzerland. The aircraft was powered by a Lycoming O-320-A2B engine. The pilot, a Swiss citizen born in 1953, was conducting a glider towing flight. The glider was an ASW 15, registration HB-1029, piloted by Pilot Y.

Accident Sequence

On 30 April 1978, at 16:26 GMT, the towplane departed from Altenrhein airfield on grass runway 10. The flight was the 32nd of the day for the pilot, who had accumulated 3 hours 54 minutes of flight time. The glider pilot was continuing his type familiarization on the ASW 15, which used a center-of-gravity tow hook for normal towing. The towrope, made of Perlon, was approximately 50 meters long and was equipped with weak links: 850 ± 50 kp at the towplane end and 600 ± 30 kp at the glider end. However, the weak link values exceeded those specified in the Swiss Federal Air Office directives and the flight manual.

The initial takeoff and climb were normal. During a left turn to crosswind or downwind leg at an altitude of about 150 meters, a significant height difference developed between the two aircraft. The glider, flying higher, raised the tail of the towplane, causing it to pitch into a dive. The towplane pilot was unable to recover. The glider pilot attempted to release the towrope, but the rope broke before he could do so, at the glider-side weak link. The towplane impacted the ground in a left-banked, nose-down attitude, with a longitudinal inclination between 30 and 50 degrees. The impact was partially cushioned by dense young forest, but a fire immediately broke out, resulting in the pilot's death. The glider pilot returned to Altenrhein and landed safely.

Investigation Findings

The investigation determined that the accident occurred because the glider flew higher than the towplane. A contributing factor was the use of the center-of-gravity tow hook, combined with the glider pilot's low experience on the ASW 15 type. The towrope's weak links were found to have breaking loads higher than recommended, which may have affected the sequence of events.

Probable cause

Glider flying higher than the towplane. Contributing factor: use of center-of-gravity tow hook combined with the glider pilot's low experience on the type.

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/1079.pdf. This page is a structured re-presentation; facts and quotes are in the Swiss Transportation Safety Investigation Board (STSB), Switzerland.