No fatalities

2008-08-23: De Havilland DHC-8-300 (Dash-8) (HK-3952) — Aires Colombia - Aerovias de Integracion Regional — Barranquilla-Ernesto Cortissoz (ex Soledad), Colombia

Barranquilla-Ernesto Cortissoz (ex Soledad), ColombiaLanding (descent or approach)

On August 23, 2008, a De Havilland DHC-8-300 (Dash-8) (registration HK-3952) operated by Aires Colombia - Aerovias de Integracion Regional was involved in an aviation accident near Barranquilla-Ernesto Cortissoz (ex Soledad), Colombia during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: Fracture of the ring of the mechanical stop of the shock absorber on the right main gear, turning the whole gear into a solid structure incapable of absorbing the landing loads, due to the non-incorporation of the Airworthiness Directive AD-2006-14 in the… This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 5 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781197244Data APIEditorial standards

An aircraft landing at Barranquilla-Ernesto Cortissoz Airport experienced a right main gear collapse after touching down 770 meters past the runway threshold. All 31 occupants evacuated safely; the aircraft was damaged beyond repair.

Incident Overview

After an uneventful flight from Willemstad-Hato Airport, the crew initiated an approach to runway 23 at Barranquilla-Ernesto Cortissoz Airport. The aircraft landed 770 meters past the runway threshold. Following touchdown, the crew detected vibrations emanating from the right side of the aircraft. Soon after, the right main gear collapsed. The aircraft slid for a few dozen meters before coming to rest on the main runway.

Occupants and Damage

All 31 occupants evacuated the aircraft safely. The aircraft sustained damage that rendered it beyond repair.

Probable Cause

Official findings attributed the incident to a fracture of the ring of the mechanical stop of the shock absorber on the right main gear. This fracture turned the entire gear into a solid structure incapable of absorbing landing loads. The root cause was the non-incorporation of Airworthiness Directive AD-2006-14 during the general repair of the main gear.