Nose gear failure causes damage to Issoire Aviation APM20 during takeoff

Casualties unknown • Conséquences, FR

A nose gear strut failure during takeoff roll led to significant damage to an APM20 aircraft during a flight training session in France.

What happened

On October 16, 2011, an Issoire Aviation APM20 (registration F-GRRH) was performing a takeoff roll on the unpaved runway 27 at Salon Eyguières aerodrome during a flight training session. As the aircraft approached rotation speed, the instructor noted an unusual noise and elected to abort the takeoff. During the deceleration, the aircraft's nose pitched forward, causing the propeller to strike the ground. The aircraft came to a halt on the runway with significant damage to the airframe.

Upon inspection, the crew discovered that the nose gear strut had fractured at the attachment points for the shock absorber. This structural failure resulted in damage to both the fuselage and the horizontal stabilizer.

The investigation

The investigation focused on the structural integrity of the nose gear and the maintenance history of the aircraft. The club operating the aircraft utilized the APM20 primarily for instruction on unpaved surfaces, which subjects the landing gear to high stress. The specific nose gear on F-GRRH had been replaced in July 2011 following a previous hard landing and had accumulated approximately 150 hours and 700 cycles since installation.

Investigators noted that instructors had reported vibrations following takeoff for about a month prior to the accident. While maintenance personnel had checked the gear components for play, no significant anomalies were found, aside from slight ovalization of the tire. Fractographic examination of the broken strut revealed that the failure was caused by fatigue cracking originating from the four bores used to secure the shock absorber bolts. Although the edges of these bores had been smoothed, the cracks propagated through the material.

Findings

  • The nose gear strut failed due to a fatigue cracking process.
  • The fatigue cracks initiated at the bores of the shock absorber attachment points.
  • The existing inspection protocols and the edge-smoothing procedures mandated by a 2009 service bulletin were insufficient to prevent this failure.
  • The design of the nose gear was inadequate for the specific operational stresses encountered by the club, particularly when operating on unpaved runways.

Probable cause

The nose gear strut failed due to fatigue cracking originating at the shock absorber attachment bores, a failure mode exacerbated by the high-stress operating environment of unpaved runways and the inadequacy of previous design modifications and inspection requirements.

Frequently asked questions

What happened in the 2011-10-16 Issoire Aviation APM20 « Lionceau » accident near Conséquences, FR?

A nose gear strut failure during takeoff roll led to significant damage to an APM20 aircraft during a flight training session in France.

What aircraft was involved and where did it happen?

The accident on 2011-10-16 involved a Issoire Aviation APM20 « Lionceau », at Conséquences, FR.

What was the probable cause of the accident?

The nose gear strut failed due to fatigue cracking originating at the shock absorber attachment bores, a failure mode exacerbated by the high-stress operating environment of unpaved runways and the inadequacy of previous design modifications and inspection requirements.

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