Casualties unknown

2016-04-17: Mooney M20F Executive (G-CEJN) — Wellesbourne Mountford Airfield, Warwickshire, GB

Wellesbourne Mountford Airfield, Warwickshire, GB

On April 17, 2016, a Mooney M20F Executive (registration G-CEJN) was involved in an aviation accident near Wellesbourne Mountford Airfield, Warwickshire, GB. 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
Aircraft registered G-CEJN
Aircraft registered G-CEJN. Photo: James from Cheltenham, Gloucestershire / CC BY-SA 2.0, via Wikimedia Commons

A Mooney M20F suffered a right main landing gear collapse after touchdown during a private flight. The gear actuating rod was found bent, preventing overcentre locking. No injuries reported.

History of the Flight

On 17 April 2016, a Mooney M20F (registration G-CEJN) departed for a local flight to check system serviceability ahead of its annual inspection. The pilot, the sole occupant, returned to Wellesbourne Mountford Airfield and lined up for landing on Runway 18 with a light southerly wind. The approach was flown at 80 mph. The pilot verified the landing gear down indication via the single green light and a physical check through the cockpit floor window. The control tower also advised to "Check 3 greens."

Accident Sequence

The aircraft touched down gently on the threshold. As it slowed, the pilot sensed the right wing dropping. He applied left aileron and simultaneously pulled the mixture control to shut down the engine. The tailskid and right flap contacted the runway, and the aircraft veered right onto grass before stopping. Upon exiting, the pilot observed that the right main landing gear had collapsed.

Engineering Examination

Post-accident examination revealed that the actuating rod for the right main landing gear was bent. The maintenance engineer noted that this bend could indicate the gear had not been in its overcentre locked condition and had attempted to react to landing loads through the retraction rod. It was also possible that pre-existing distortion of the rod had prevented overcentering. The indicator light and the mechanical window check only confirm the actuating rods are in the correct position, not that the gears are locked down.