Casualties unknown

1992-12-17: LEARJET 35A (D-CCHB) — Bern Flughafen (LSZB), BE, CH

Bern Flughafen (LSZB), BE, CH

On December 17, 1992, a LEARJET 35A (registration D-CCHB) was involved in an aviation accident near Bern Flughafen (LSZB), BE, CH. Investigators recorded the probable cause as: Continuing an approach without sufficient visibility; landing with excessive sink rate. This summary draws on records from the Swiss Transportation Safety Investigation Board (STSB / SUST); 6 related events involving the same aircraft type or operator are linked below.

Sourcesthe Swiss Transportation Safety Investigation Board (STSB / SUST)Primary reportUpdated 1785034239Data APIEditorial standards
Aircraft registered D-CCHB
Aircraft registered D-CCHB. Photo: Rob Hodgkins / CC BY-SA 2.0, via Wikimedia Commons

On 17 December 1992, a Learjet 35A (D-CCHB) landed hard at Bern-Belp after continuing an ILS approach in low visibility, breaking the right main landing gear and buckling the wing skin.

Flight Details

On 17 December 1992, a Learjet 35A, registration D-CCHB, operated a private IFR flight from Stuttgart to Bern-Belp. The crew received ATIS information indicating visibility 3500 meters, temperature and dew point both 0°C, and QNH 1022. The pilot contacted the tower for additional weather information; the controller stated that landing minima were met and no significant deterioration was expected for the planned landing time.

Approach

The pilot requested a direct approach to the ILS for runway 14, bypassing the standard procedure. The controller cleared the aircraft for a direct line-up. At three miles from the runway, the controller asked if the crew had the runway lights in sight; the pilot replied "not yet." The controller then increased the intensity of the runway lights to 30% to avoid blinding the crew. No further communication was made, and landing clearance was not issued. The crew continued the approach, anticipating a warning from ATC if visibility decreased rapidly.

Landing and Damage

The pilot misjudged the distance to the ground due to diffuse visibility. The aircraft touched down with a high sink rate, resulting in a hard landing. The right main landing gear's cast component broke, and the upper wing skin was buckled. The aircraft rolled to the stop near the end of the runway. The controller only saw the aircraft after touchdown.

Aftermath

The crew did not report the incident. The airport authority was informed the next day and notified the Federal Office for Civil Aviation. After a provisional repair, the German Federal Aviation Office (LBA) issued a limited ferry permit to Nuremberg for permanent repairs.

Findings and Causes

The investigation found no pre-existing technical defects, valid crew licenses, and normal navigational aids. The accident was attributed to continuing an approach without sufficient visibility and landing with an excessive sink rate.

Probable cause

Continuing an approach without sufficient visibility; landing with excessive sink rate.

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/1490.pdf. This page is a structured re-presentation; facts and quotes are in the Swiss Transportation Safety Investigation Board (STSB), Switzerland.