No fatalities

2010-03-01: Airbus A300 (TC-ACB) — ACT Airlines — Bagram AFB, Afghanistan

Bagram AFB, AfghanistanLanding (descent or approach)

On March 1, 2010, an Airbus A300 (registration TC-ACB) operated by ACT Airlines was involved in an aviation accident near Bagram AFB, Afghanistan during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: Cracks as result of fatigue caused the fracture of the hinge arm of the left main gear strut. The cracking most likely occurred as result of corrosion that remained undetected during the last maintenance inspection. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 10 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781196243Data APIEditorial standards

During approach, crew observed a red indicator for the left main gear. After low passes confirmed gear down, the left main gear collapsed during braking, veering off the runway. All five crew were unhurt; the aircraft was damaged beyond repair.

Incident Details

While approaching Bagram Air Force Base, the crew lowered the landing gear but did not receive the standard three green lights. The indicator for the left main gear remained red.

Low Passes and Landing

The captain obtained authorization to perform two low passes over the airport. During these passes, air traffic control confirmed that all three landing gears appeared to be down. The crew then completed a final approach at low speed. After touchdown, while applying brakes, the left main gear collapsed.

Aftermath

The aircraft veered to the left off the runway and came to rest approximately 2 kilometers past the runway threshold. All five crew members were unhurt, but the aircraft sustained damage beyond repair.

Investigation Findings

According to official findings, the probable cause was cracks resulting from fatigue, which led to fracture of the hinge arm of the left main gear strut. The cracking likely occurred due to corrosion that remained undetected during the last maintenance inspection. The origin of pitting could not be identified, but the investigation identified deficiencies in the maintenance task conducted during the last overhaul of the gear strut. Incomplete maintenance documentation and tools available during the overhaul contributed to the accident.