Casualties unknown

2003-07-19: PIPER PA-38-112 (G-RECS) — Beverley Airfield, Humberside, GB

Beverley Airfield, Humberside, GB

On July 19, 2003, a PIPER PA-38-112 (registration G-RECS) was involved in an aviation accident near Beverley Airfield, Humberside, 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

On 19 July 2003, a Piper PA-38-112 Tomahawk (G-RECS) experienced a bounced landing and subsequent ground contact during a go-around at Beverley Airfield, Humberside. The pilot and passenger were uninjured, but the landing gear, propeller, and engine sustained damage.

Incident Overview

On 19 July 2003 at 1530 hours, a Piper PA-38-112 Tomahawk, registration G-RECS, was involved in an incident while landing at Beverley Airfield, Humberside. The aircraft was manufactured in 1981 and powered by a single Lycoming O-235-L2C piston engine. The flight was conducted under a Private Pilot's Licence, with the sole pilot and one passenger on board. No injuries were reported. Damage was limited to the landing gear, propeller, and engine.

Pilot Information

The commander, aged 40, held a Private Pilot's Licence and had accumulated 185 total flying hours, of which 181 were on the Piper PA-38-112 Tomahawk type. He had flown no hours in the previous 90 days or 28 days.

Sequence of Events

According to the pilot's report, the approach was to grass Runway 12. The surface wind was 220° at 11 knots. While crossing the displaced threshold at an altitude of 15 to 20 feet above ground level, the aircraft descended rapidly and contacted the ground on all three wheels. It then bounced back into the air in a nose-high attitude. The pilot initiated a go-around. During this maneuver, the right wing lifted, the aircraft veered to the left, and the left wing struck the ground, immediately followed by the nose.

Pilot Commentary

The pilot noted that he may have been too slow during the approach. He recalled hearing the stall warning after the initial ground contact.

Damage Assessment

Post-incident inspection revealed damage to the landing gear, propeller, and engine. No further details on the extent of damage were provided in the report.

Information Source

All details in this article are derived from the AAIB Bulletin No. 9/2003, reference EW/G2003/07/21, based on the Aircraft Accident Report Form submitted by the pilot.