Casualties unknown

2006-07-19: Rockwell Commander 114 (G-DDIG) — Fearn Airstrip near Tain, Ross-shire, Scotland, GB

Fearn Airstrip near Tain, Ross-shire, Scotland, GB

On July 19, 2006, a Rockwell Commander 114 (registration G-DDIG) was involved in an aviation accident near Fearn Airstrip near Tain, Ross-shire, Scotland, GB. Investigators recorded the probable cause as: The accident resulted from the flaps retracting fully while the pilot was attempting to trim the aircraft during the go-around. 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

During a go-around after a bounced landing, the pilot fully retracted flaps instead of to Flaps 20, leading to loss of lift and nose landing gear collapse. No injuries.

Synopsis

After a bounce on landing, the pilot initiated a go-around by applying full power and retracting the flap. The flaps retracted fully rather than to the normal Flaps 20 for a go-around, and the pilot was unable to prevent the aircraft sinking onto the runway with a subsequent nose landing gear collapse.

History of the Flight

After a short local flight, the pilot returned to the airstrip for landing. The airstrip was an old military airfield with an asphalt surface oriented approximately east/west. The weather was good with a calm surface wind, and the pilot established his approach with Flap 35 for a landing on Runway 29. He considered that his approach was stable until, at an estimated 20 feet agl, he was aware of an increased descent rate. He applied some power but the aircraft bounced on landing. The pilot decided to go-around, applied full power, and selected the flap control to the ‘up’ position. He was then aware of a loss of lift and the aircraft tracking to the left of the runway but yawing to the right. The nose landing gear collapsed and G-DDIG came to rest at the edge of the runway. After switching off the battery, the pilot followed his passengers out of the aircraft.

The pilot later commented that the aircraft needs a lot of nose-up trim on approach and when he applied full power for his go-around, he then needed to apply forward trim.

Assessment

The flaps are electrically actuated and controlled by a three-position switch; these positions are up, neutral and down. The switch is spring-loaded in the down sense such that it must be held in the down position to extend the flaps and when released, it returns to the neutral position. However, when the switch is moved to the up position to raise the flaps, it will stay there until returned to the neutral position by the pilot. For a normal go-around, the flaps should only be retracted to Flaps 20. The pilot considered that the accident resulted from the flaps retracting fully while he was attempting to trim the aircraft during the go-around.

Probable cause

The accident resulted from the flaps retracting fully while the pilot was attempting to trim the aircraft during the go-around.