Casualties unknown

2003-09-17: Jetstream 31, (G-EEST) — Wick Airport, Scotland, GB

Wick Airport, Scotland, GB

On September 17, 2003, a Jetstream 31, (registration G-EEST) was involved in an aviation accident near Wick Airport, Scotland, GB. Investigators recorded the probable cause as: The investigation determined that just before the first touchdown, one or both power levers were moved aft of the flight idle position, and both pilots were making control inputs from that moment until after the second heavy touchdown. 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 17 September 2003, a Jetstream 31, G-EEST, experienced a bounced landing at Wick Airport, resulting in a propeller strike and wing spar crack. All seven occupants were uninjured.

Incident Overview

A Jetstream 31, registration G-EEST, operated by Eastern Airways, was involved in a hard landing at Wick Airport, Scotland on 17 September 2003. The aircraft, manufactured in 1987, was conducting a scheduled passenger flight from Aberdeen with four passengers and three crew on board. No injuries were reported, but the aircraft sustained damage including a right propeller tip strike and a cracked wing spar.

Flight Details

The crew had already completed two sectors earlier that day in a different aircraft. After transferring to G-EEST, they departed Aberdeen for Wick at 1414 hrs. The co-pilot was the pilot flying. During the approach to Runway 31, the aircraft encountered turbulence and windshear, resulting in a higher-than-normal threshold speed of 130 kt, 21 kt above the correct speed. The VREF for the landing weight of 12,575 lb was 102 kt. The aircraft crossed the displaced threshold slightly high and fast.

Landing Sequence

As the aircraft flared, it floated approximately six feet above the runway. The co-pilot reduced power to flight idle, but just before the first touchdown, one or both power levers were moved aft of the flight idle position. The aircraft touched down nose-wheel first, bounced 10 to 15 feet, then touched down again more heavily. This second touchdown cracked the wing spar and flexed the fuselage, allowing the right propeller to contact the runway. The aircraft bounced a second time before landing for the third and final time. During the roll, the commander applied brakes and reverse thrust. The crew did not observe any abnormal indications until after shutdown, when the commander noticed the propeller damage.

Investigation Findings

The AAIB investigation found no technical faults with the aircraft. Weather conditions were within the aircraft's limitations. The investigation determined that both pilots were making control inputs from just before the first touchdown until after the second heavy touchdown. No safety recommendations were made.

Probable cause

The investigation determined that just before the first touchdown, one or both power levers were moved aft of the flight idle position, and both pilots were making control inputs from that moment until after the second heavy touchdown. No technical fault was found and weather was within limits.