Nose gear failure causes taxiing accident in Robin DR 300

Casualties unknown • FR

A nose gear collapse during taxiing at Bordeaux-Léognan-Saucats led to an aircraft excursion and a small engine fire, involving undetected fatigue cracks.

What happened

On January 21, 1996, a Robin DR 300/140, registration F-BSLU, was performing a local VFR flight with one pilot and two passengers at the Bordeaux-Léognan-Saucats airfield. Following a normal landing on runway 04, the aircraft began taxiing. During this phase, the nose gear suddenly collapsed underneath the engine.

The aircraft slid approximately 100 meters along the runway before veering off to the left and coming to a halt. During the excursion, the nose of the aircraft made contact with the runway surface. Following the stop, the pilot evacuated the passengers and discovered the onset of a fire near the engine. The fire was quickly extinguished by a bystander using a portable fire extinguisher.

The investigation

The investigation focused on the structural failure of the nose gear, which was a S.A.B. T2 type. Physical and microscopic examinations revealed that the failure originated from two fatigue cracks located on either side of the upper attachment plate. These cracks were situated in a heat-affected zone created during the welding process that joins the plate to the gear strut.

Investigators also examined the maintenance history and existing airworthiness directives. While previous directives required inspections of the lower plate and certain weld areas, the upper attachment plate was located behind the engine and was not accessible without significant maintenance disassembly. Consequently, there was no requirement for regular inspections of this specific component.

Findings

  • The nose gear failure was caused by undetected fatigue cracks on the upper attachment plate.
  • The cracks developed in a thermally affected zone where the material structure had been altered by welding.
  • Current maintenance and inspection procedures did not include the upper attachment plate, making it impossible to detect the cracks during routine checks.
  • The aircraft was within weight and balance limits, and the pilot was properly licensed and qualified.
  • Similar failures had been observed in previous accidents involving other Robin aircraft, such as F-BRZE and F-BTBM.

Probable cause

The nose gear collapsed due to the presence of undetected fatigue cracks on the upper attachment plate, which weakened the connection between the gear strut and the attachment hardware. This structural vulnerability was not detectable through standard inspection protocols because the component was obscured by the engine.

Frequently asked questions

What happened in the 1996-01-21 MINISTERE DE L'EQUIPEMENT, DES TRANSPORTS, DU LOGEMENT, DU TOURISME ET DE LA MER - BUREAU D'ENQUETES ET D'ANALYSES POUR LA SECURITE DE L'AVIATION CIVILE Accident survenu le 21 janvier 1996 sur l’aérodrome de Bordeaux-Léognan-Saucats accident near FR?

A nose gear collapse during taxiing at Bordeaux-Léognan-Saucats led to an aircraft excursion and a small engine fire, involving undetected fatigue cracks.

What aircraft was involved and where did it happen?

The accident on 1996-01-21 involved a MINISTERE DE L'EQUIPEMENT, DES TRANSPORTS, DU LOGEMENT, DU TOURISME ET DE LA MER - BUREAU D'ENQUETES ET D'ANALYSES POUR LA SECURITE DE L'AVIATION CIVILE Accident survenu le 21 janvier 1996 sur l’aérodrome de Bordeaux-Léognan-Saucats, registration F-BSLU, at FR.

What was the probable cause of the accident?

The nose gear collapsed due to the presence of undetected fatigue cracks on the upper attachment plate, which weakened the connection between the gear strut and the attachment hardware. This structural vulnerability was not detectable through standard inspection protocols because the component was obscured by the…

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