Casualties unknown

1998-07-15: Rand KR-2 (G-BVZJ) — Phoenix Farm, Hampshire, GB

Phoenix Farm, Hampshire, GB

On July 15, 1998, a Rand KR-2 (registration G-BVZJ) was involved in an aviation accident near Phoenix Farm, Hampshire, GB. Investigators recorded the probable cause as: The pilot assessed the cause of the accident as his lack of experience on the type of aircraft and the narrowness of the strip. 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-BVZJ
Aircraft registered G-BVZJ. Photo: Alec Wilson from Khon Kaen, Thailand / CC BY-SA 2.0, via Wikimedia Commons

A private Rand KR-2 suffered structural failure after a wingtip caught crops during a go-around at Upham. The pilot was unharmed and attributed the accident to his limited experience on type and the narrow strip.

Aircraft and Flight Details

The aircraft was a Rand KR-2, registration G-BVZJ, equipped with one Revmaster piston engine and built in 1996. It was operated on a private flight by a 64-year-old pilot holding a Private Pilot's Licence, who had accumulated 190 total flying hours, with only one hour on type. The flight was part of a test schedule for a Permit to Fly after the pilot had built the aircraft.

Accident Sequence

On 15 July 1998 at 1615 UTC, the aircraft was on a short local flight. An approach was made to Runway 25 at Upham, Hampshire, a 30-metre wide private grass strip bordered on one side by a hedge and on the other by a crop of oilseed rape. The wind was described by the pilot as 250°/10 kt and gusty. During the late stages of the approach, the aircraft drifted to the left, and the wingtip became caught in the crop before the pilot was able to carry out a go-around.

Damage and Injuries

The aircraft slewed around, causing the engine and tail to break off. The engine, complete with firewall and bulkhead, separated from the front fuselage. The fuselage rear separated at the tail leading edge. Damage occurred to the landing gear, engine, fuselage, and both wings. The wings and cockpit came to rest 20 metres further on in the crop in an upright position. There was no fire. The pilot, who was wearing a full shoulder harness, was not injured.

Pilot Assessment

The pilot assessed the cause of the accident as his lack of experience on the type of aircraft and the narrowness of the strip.

Probable cause

The pilot assessed the cause of the accident as his lack of experience on the type of aircraft and the narrowness of the strip.