Glider Stall During Turnback After Winch Cable Break

Casualties unknown • Militärflugplatz, CH

A Rhönlerche II glider crashed on a military airfield after the instructor attempted a turning maneuver to return to the launch site following a cable failure.

What happened

On March 21, 1964, a Rhönlerche II glider, registration HB-702, was performing a dual training flight at a military airfield. The flight was conducted using an aero-winch launch method, with a student pilot in the front seat and an instructor in the rear.

During the initial climb, the winch cable began to rotate continuously due to an asymmetry in the cable shuttle. At an altitude of approximately 50 to 60 meters, the cable's weak link failed. Despite the cable break, the instructor allowed the student to maintain control of the aircraft.

Rather than continuing straight ahead to land on the remaining paved runway, the student proposed a left-hand turn to return to the takeoff position. The instructor agreed to this maneuver, despite the availability of roughly 800 meters of paved runway and an additional 1,000 meters of flat grass ahead. During the turn, the instructor took control to increase the bank angle but failed to maintain sufficient airspeed. Consequently, the aircraft lost speed and stalled at an altitude of about 15 to 20 meters, striking the paved surface with the left wingtip and the nose of the fuselage.

The investigation

The investigation examined the mechanical failure of the winch system and the flight maneuvers following the cable break. Investigators noted that the instructor had not flown since November 1963, having only resumed training with a brief solo flight on the day of the accident. The investigation also assessed the available landing area, which provided ample distance for a straight-ahead landing.

Findings

  • The primary cause of the accident was the decision to execute a turning maneuver to return to the launch site at an insufficient altitude.
  • The winch cable failure was caused by the continuous twisting of the cable, likely due to an asymmetric cable shuttle.
  • The instructor's decision to permit a turn, rather than proceeding with a straight landing, led to a loss of airspeed during the bank.
  • The instructor may have been motivated to avoid the long ground transport required to return the glider to the winch site.

Safety action

No specific safety recommendations were recorded in the final report.

Probable cause

The accident was caused by the instructor's decision to attempt a return to the launch site via a turning maneuver following a winch cable break, which resulted in a stall at low altitude due to insufficient airspeed.

Frequently asked questions

What happened in the 1964-03-21 ALEXANDER SCHLEICHER OHG SEGELFLUGZEUGBAU RHÖNLERCHE II accident near Militärflugplatz, CH?

A Rhönlerche II glider crashed on a military airfield after the instructor attempted a turning maneuver to return to the launch site following a cable failure.

What aircraft was involved and where did it happen?

The accident on 1964-03-21 involved a ALEXANDER SCHLEICHER OHG SEGELFLUGZEUGBAU RHÖNLERCHE II, registration HB-702, at Militärflugplatz, CH.

What was the probable cause of the accident?

The accident was caused by the instructor's decision to attempt a return to the launch site via a turning maneuver following a winch cable break, which resulted in a stall at low altitude due to insufficient airspeed.

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/164.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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