Casualties unknown

2006-05-03: APEX AIRCRAFT ROBIN DR 400/180 R (HB-KOC) — Bern Flughafen (LSZB), BE, CH

Bern Flughafen (LSZB), BE, CH

On May 3, 2006, an APEX AIRCRAFT ROBIN DR 400/180 R (registration HB-KOC) was involved in an aviation accident near Bern Flughafen (LSZB), BE, CH. Investigators recorded the probable cause as: The accident was due to the pilot not taking several emergency landing opportunities after an engine malfunction, resulting in uncontrolled ground contact with rollover and subsequent fire. This summary draws on records from the Swiss Transportation Safety Investigation Board (STSB / SUST).

Sourcesthe Swiss Transportation Safety Investigation Board (STSB / SUST)Primary reportUpdated 1785639345Data APIEditorial standards

On 3 May 2006, a Robin DR400-180R (HB-KOC) operated by Segelfluggruppe Bern crashed at Hühnerhubel, Belp, about 600 m southwest of Bern-Belp Airport after an engine problem. The pilot did not take several emergency landing opportunities, leading to uncontrolled ground contact, rollover, and fire. Lack of a cockpit tool to break the canopy made the otherwise survivable accident fatal.

Synopsis

On 3 May 2006 at 18:24 local time, a Robin DR400-180R aircraft, registration HB-KOC, operated by Segelfluggruppe Bern, departed from Bern-Belp Airport on a glider towing flight. During takeoff, an engine malfunction occurred. The pilot subsequently did not take several available opportunities for an emergency landing. The aircraft made uncontrolled ground contact at Hühnerhubel, in the municipality of Belp, approximately 600 meters southwest of the airport, resulting in a rollover and subsequent fire. The cockpit canopy's Plexiglass could not be broken from inside due to the absence of a suitable tool, which transformed an otherwise survivable accident into a fatal one.

Investigation

The investigation was conducted by the Swiss Aircraft Accident Investigation Bureau (AAIB). The aircraft was a Robin DR400-180R, a single-engine four-seat monoplane with a fixed-pitch propeller. The pilot held a valid license and had adequate flying experience for glider towing operations. The aircraft had been maintained in accordance with regulations. Weather conditions at the time were not a contributing factor. The engine and airframe were examined; no pre-existing technical defects were found that could have caused the engine malfunction.

Cause

The accident was caused by the pilot failing to take several available opportunities for an emergency landing after an engine malfunction, leading to uncontrolled ground contact, rollover, and fire. The lack of a cockpit tool to break the Plexiglass canopy resulted in the otherwise survivable accident having a fatal outcome.

Safety Recommendations

As a result of the investigation, Safety Recommendation No. 403 was issued to address the deficiency in cockpit emergency equipment. Additionally, the Segelfluggruppe Bern implemented measures regarding the use of radio frequencies during glider operations at Bern-Belp.

Probable cause

The accident was due to the pilot not taking several emergency landing opportunities after an engine malfunction, resulting in uncontrolled ground contact with rollover and subsequent fire. The lack of a cockpit tool to break the Plexiglass canopy made the otherwise survivable accident fatal.

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/2039_f.pdf. This page is a structured re-presentation; facts and quotes are in the Swiss Transportation Safety Investigation Board (STSB), Switzerland.