2 fatalities

Glider Accident in Laa-Graben, Löhningen on 1 October 1989 (HB-1516)

Löhningen, SH, CH

On October 1, 1989, a PZL-BIELSKO SZD-50-3 (registration HB-1516) was involved in an aviation accident near Löhningen, SH, CH. 2 people were killed. Investigators recorded the probable cause as: The accident was due to exceeding minimum speed near the ground, an intentional or unintentional spin initiated too late to recover, the instructor's low aerobatic experience, and a likely unlocked or misadjusted left trim control. This summary draws on records from the Swiss Transportation Safety Investigation Board (STSB / SUST).

Sourcesthe Swiss Transportation Safety Investigation Board (STSB / SUST)Primary reportUpdated 2026-10-18Data APIEditorial standards

On 1 October 1989, a SZD-50-3 Puchacz glider (HB-1516) crashed in Laa-Graben, Löhningen after a spin and subsequent stall. The instructor and student were fatally injured. The glider was destroyed.

Incident

On Sunday, 1 October 1989, at 1104 local time, an instructor and a student took off from Schaffhausen aerodrome in a SZD-50-3 "Puchacz" glider, registration HB-1516, for a training flight. After release at about 900 m above mean sea level east of Siblingen, the glider was observed by witnesses entering a spin. Seven to eight rotations were seen. The glider recovered near the ground, crossing a railway embankment at about 10 m above ground. It then stalled again and crashed from about 10 m onto its left wing. The accident occurred at 1124 hours at coordinates 683 000 / 282 800, elevation 430 m/M.

Aircraft and Crew

The glider, a two-seat shoulder-wing aircraft with a fixed main wheel, was manufactured in 1979 by PZL-Bielsko, Poland. It had accumulated 1812:23 hours on the airframe. The maximum takeoff mass was 570 kg; the mass at the time of the accident was about 558 kg, within limits. The aircraft was operated by Segelfluggruppe Schaffhausen.

The instructor, a Swiss citizen born in 1940, held a glider pilot license issued in 1963, with aerobatic endorsement from 1972. His total glider experience was 1338:19 hours, with 55:41 hours on the accident type. His aerobatic experience was low. The student, a Swiss citizen born in 1973, held a student pilot license issued in August 1989. He had 5:38 total glider hours, with 4:45 on the accident type.

Investigation

Examination of the wreckage revealed no pre-existing technical defects except the left trim control, which appeared to have been loose before the accident. Both pilots were wearing lap and shoulder belts, which remained intact. Autopsies showed both died from impact injuries; no pre-existing conditions or alcohol/drugs were found. Foot injuries indicated the right rudder pedal was depressed. The glider had minimal forward speed at impact; the nose section showed no sliding marks, indicating a near-vertical descent.

Causes

The investigation concluded that the accident was due to:

  • Exceeding the minimum speed near the ground.
  • An intentional or unintentional spin initiated too late to recover.
  • The instructor's low aerobatic experience.
  • A likely unlocked or misadjusted left trim control.

Probable cause

The accident was due to exceeding minimum speed near the ground, an intentional or unintentional spin initiated too late to recover, the instructor's low aerobatic experience, and a likely unlocked or misadjusted left trim control.

Frequently asked questions

What happened in the 1 Oct 1989 PZL-BIELSKO SZD-50-3 accident near Löhningen, SH, CH?

On 1 October 1989, a SZD-50-3 Puchacz glider (HB-1516) crashed in Laa-Graben, Löhningen after a spin and subsequent stall. The instructor and student were fatally injured. The glider was destroyed.

Were there any fatalities in the 1 Oct 1989 PZL-BIELSKO SZD-50-3 accident?

The accident was fatal, resulting in 2 fatalities.

What aircraft was involved and where did it happen?

The accident on 1 Oct 1989 involved a PZL-BIELSKO SZD-50-3, registration HB-1516, at Löhningen, SH, CH.

What was the probable cause of the accident?

The accident was due to exceeding minimum speed near the ground, an intentional or unintentional spin initiated too late to recover, the instructor's low aerobatic experience, and a likely unlocked or misadjusted left trim control.

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/1459.pdf. This page is a structured re-presentation; facts and quotes are in the Swiss Transportation Safety Investigation Board (STSB), Switzerland.