Casualties unknown

2014-12-04: AVIONS DE TRANSPORT RéGIONAL 72-202 (D-ANFE) — Zürich Flughafen (LSZH), ZH, CH

Zürich Flughafen (LSZH), ZH, CH

On December 4, 2014, an AVIONS DE TRANSPORT RéGIONAL 72-202 (registration D-ANFE) was involved in an aviation accident near Zürich Flughafen (LSZH), ZH, CH. Investigators recorded the probable cause as: The accident is attributable to the fact that during landing the nose landing gear was not centered and thus the two nose wheels could not rotate freely. Consequently, control of the nose landing gear, which was considerably damaged, was no longer given. This summary draws on records from the Swiss Transportation Safety Investigation Board (STSB / SUST); 7 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

On 4 December 2014, an ATR 72-202 (D-ANFE) experienced a loss of nose landing gear control during landing at Zurich Airport. The nose landing gear was not centered, causing the wheels to lock and the gear to be damaged. The investigation identified a reversed valve input lever and poor maintenance as causes.

Accident

On 4 December 2014, an ATR 72-202 commercial aircraft, registration D-ANFE, was landing on runway 14 of Zurich Airport (LSZH). During the landing, the nose landing gear was not centered, preventing the two nose wheels from rotating freely. Consequently, control of the nose landing gear was lost, and the gear sustained significant damage.

Investigation

The Swiss Transportation Safety Investigation Board (STSB) conducted the investigation. Examination of the nose landing gear revealed that the valve input lever of the differential control selector valve (DCSV) had been connected rotated by 180°. This misalignment prevented proper steering function. Additionally, the investigation found that maintenance of the nose landing gear had been inadequate.

Probable Cause

The STSB determined that the accident was attributable to the nose landing gear not being centered during landing, which prevented free rotation of the nose wheels. The most likely cause was the interaction of two factors: a valve input lever of the differential control valve connected rotated by 180° on the nose landing gear, and inadequate maintenance of the nose landing gear. A contributing factor was the design that allowed the valve input lever to be installed incorrectly by 180°.

Other Findings

During runway inspections conducted a few hours after the accident, small aircraft parts were found on the runway. While these parts did not influence the occurrence or course of the accident, they were considered a safety risk.

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/2303_e.pdf. This page is a structured re-presentation; facts and quotes are in the Swiss Transportation Safety Investigation Board (STSB), Switzerland.