Casualties unknown

2008-05-10: Cessna 310Q (N850KF) — Jersey Airport, GB

Jersey Airport, GB

On May 10, 2008, a Cessna 310Q (registration N850KF) was involved in an aviation accident near Jersey Airport, GB. Investigators recorded the probable cause as: The right main landing gear failed to lock down due to stiffness in operation caused by inadequate lubrication of the pivot bearings, preventing the leg from reaching the fully extended position. This summary draws on records from the UK Air Accidents Investigation Branch (AAIB).

Sourcesthe UK Air Accidents Investigation Branch (AAIB)Primary reportUpdated 1785053200Data APIEditorial standards

On 10 May 2008, a Cessna 310Q suffered a right main landing gear failure to lock down due to stiff operation from inadequate lubrication, leading to gear collapse during landing and damage to the right wingtip, flap, aileron, and propeller.

History of the Flight

On 10 May 2008, at approximately 1030 UTC, the pilot of a Cessna 310Q (registration N850KF) was conducting a private flight and approaching Jersey Airport. While on an ILS/DME approach about 3.5 miles out, the pilot selected the landing gear down. The green gear-down-and-locked light for the right main landing gear failed to illuminate.

The pilot initiated a go-around and, when safe, replaced the light bulb, but the light remained off. He then attempted to lower the gear using both the normal and emergency extension systems, and tried sideslipping the aircraft to lock the gear down. These efforts were unsuccessful, and the green light for the right main gear stayed off, leading the pilot to conclude the gear had not locked down.

The pilot made a visual approach to Runway 27 with full flap and reduced speed to the blue-line figure. On rounding out, he held off until the stall warning occurred to achieve a gentle touchdown. He kept the aircraft straight, allowing it to slow without braking, hoping the right main gear would continue to support the aircraft. As he moved the mixture controls toward fully closed, the right wing began to drop. He then turned off the fuel, electrics, and magnetos. After the aircraft came to a halt, he exited via the main door.

Examination and Findings

Post-accident examination revealed that a link securing the right leg in the extended position had suffered an overload failure. The damage was consistent with the component, designed to carry only retraction and extension loads, being subjected to ground loads due to the landing gear not reaching the locked position. During retraction and extension tests after repairs, considerable stiffness in the operation of the right leg was noted. This stiffness was attributed to inadequate lubrication of the pivot bearings.

The right wingtip, flap, aileron, and propeller contacted the runway and were damaged.

Probable Cause

The right main landing gear failed to lock down due to stiffness in operation caused by inadequate lubrication of the pivot bearings, preventing the leg from reaching the fully extended position.