No fatalities

2015-09-30: De Havilland DHC-8-400 (Dash-8) (LX-LGH) — Luxair — Saarbrücken, Germany

Saarbrücken, GermanyTakeoff (climb)

On September 30, 2015, a De Havilland DHC-8-400 (Dash-8) (registration LX-LGH) operated by Luxair was involved in an aviation accident near Saarbrücken, Germany during takeoff. No fatalities were reported. Investigators recorded the probable cause as: The accident was caused by the premature retraction of the landing gear during takeoff, which was permitted by both pilot action and the aircraft's control logic design. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 3 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781192778Data APIEditorial standards

A Bombardier DHC-8-402 experienced an unplanned landing gear retraction during takeoff from Saarbrucken, resulting in a tail strike and fuselage skid.

What happened

A scheduled flight operated by a crew of four was performing a multi-leg mission originating in Luxembourg, traveling via Saarbulence to Hamburg, and returning. On the day of the incident, the aircraft, a Bombardier DHC-8-402, was operating a leg from Luxembourg to Saarbrucken carrying 14 passengers, with an additional 16 passengers intended for the return leg to Luxembourg. The flight crew had completed pre-flight preparations early and were ahead of their planned schedule.

During the takeoff roll at Saarbrucken, the pilot in command elected to use a reduced engine thrust setting of 81%. As the aircraft accelerated through the rotation phase, reaching approximately 127 KIAS with a 5-degree nose-up attitude, the landing gear retracted unexpectedly. This premature retraction led to a tail strike at 10:16:44 hrs. Following the initial contact, the aircraft bounced three times and eventually came to a halt approximately 875 meters from the point of impact after skidding on its fuselage. Due to the presence of smoke and fumes within the cabin, an immediate evacuation was performed. There were zero fatalities and zero injuries among the passengers and crew.

Findings

The investigation determined that the primary cause of the accident was the early retraction of the landing gear during takeoff, a movement that was not intercepted by the landing gear selector lever or the aircraft's retracting control logic. Several contributing factors were identified, including:

  • A decrease in crew concentration levels.
  • A disruption in the established callout sequence and task management by the pilot non-flying.
  • The manual movement of the landing gear lever to the UP position prematurely.
  • A design flaw in the control logic that permitted the gear to retract while one wheel was still airborne.

Probable cause

The accident was caused by the premature retraction of the landing gear during takeoff, which was permitted by both pilot action and the aircraft's control logic design.