No fatalities

Grumman AA-5 Traveler Front Gear Failure During Landing at Pons-Avy (G-BIWW)

revêtue 1 250 x 80 m, FR

On July 6, 2013, a Grumman American Aviation AA-5 Traveler (registration G-BIWW) was involved in an aviation accident near revêtue 1 250 x 80 m, FR. No fatalities were reported. Investigators recorded the probable cause as: Inappropriate control inputs after main gear touchdown, exacerbated by high approach speed and turbulence, caused excessive lateral loads that resulted in the static rupture of the front landing gear. This summary draws on records from the French Bureau d'Enquêtes et d'Analyses (BEA).

Sourcesthe French Bureau d'Enquêtes et d'Analyses (BEA)Primary reportUpdated 2026-10-18Data APIEditorial standards

On July 6, 2013, a Grumman AA-5 Traveler (G-BIWW) suffered front landing gear failure during a scenic flight landing at Pons-Avy. Turbulence and crosswinds contributed to the incident, resulting in minor damage.

Incident Overview

On July 6, 2013, at approximately 17:30 local time, a Grumman American Aviation AA-5 Traveler with registration G-BIWW experienced a mechanical failure during landing at Pons-Avy aerodrome in France. The aircraft was operated by a flying club for a general aviation scenic flight carrying one pilot and three passengers.

Flight Progression

The flight departed Pons-Avy around 15:00. While the initial portion of the half-hour flight proceeded normally, the pilot reported encountering turbulence during the final approach round-out phase. This instability forced the pilot to adjust power settings and alter the intended landing point, resulting in a touchdown approximately 200 meters down the unimproved runway (Runway 31). Upon contact with the main gear, the pilot released pressure on the control stick, causing the nose gear to collapse. The aircraft slid for roughly thirty meters before coming to rest on its fuselage.

Damage and Investigation Findings

Post-incident inspection revealed a static rupture of the front landing gear leg. Additionally, the tips of both propeller blades were folded backward, indicating the engine was operating at low power during the event. The pilot, who held a PPL/A license with 1,350 total flight hours but only 10 hours on type, noted that he had increased his approach speed to 75 knots due to crosswinds and turbulence. This exceeded the recommended range of 65–70 knots for maximum takeoff weight.

Contributing Factors

The investigation concluded that the combination of high approach speed, turbulence, and crosswind made the landing phase more challenging. It is probable that inappropriate control inputs after main gear touchdown generated significant lateral loads on the nose gear, leading to its failure. The pilot's limited experience on this specific aircraft type was also identified as a contributing factor.

Probable cause

Inappropriate control inputs after main gear touchdown, exacerbated by high approach speed and turbulence, caused excessive lateral loads that resulted in the static rupture of the front landing gear.

Frequently asked questions

What happened in the 6 Jul 2013 Grumman American Aviation AA-5 Traveler accident near revêtue 1 250 x 80 m, FR?

On July 6, 2013, a Grumman AA-5 Traveler (G-BIWW) suffered front landing gear failure during a scenic flight landing at Pons-Avy. Turbulence and crosswinds contributed to the incident, resulting in minor damage.

Were there any fatalities in the 6 Jul 2013 Grumman American Aviation AA-5 Traveler accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 6 Jul 2013 involved a Grumman American Aviation AA-5 Traveler, registration G-BIWW, at revêtue 1 250 x 80 m, FR.

What was the probable cause of the accident?

Inappropriate control inputs after main gear touchdown, exacerbated by high approach speed and turbulence, caused excessive lateral loads that resulted in the static rupture of the front landing gear.