4 fatalities

1999-01-13: Boeing KC-135 Stratotanker (59-1452) — Air National Guard — Geilenkirchen NATO Air Base, Germany

Geilenkirchen NATO Air Base, GermanyLanding (descent or approach)

On January 13, 1999, a Boeing KC-135 Stratotanker (registration 59-1452) operated by Air National Guard was involved in an aviation accident near Geilenkirchen NATO Air Base, Germany during landing or approach. 4 people were killed. Investigators recorded the probable cause as: The crew lost control of the aircraft during a go-around because an undetected failure of the runway trim motor caused an uncommanded nose-up pitch. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 6 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781204607Data APIEditorial standards

A KC-135 Stratotanker crashed in a wooded area near Geilenkirchen NATO AFB during a night approach, resulting in the deaths of all four crew members.

What happened

During a nighttime arrival at Geilenlykirchen NATO Air Base, an aircraft operating for the 141st Air Refueling Wing from Fairchild, Washington, crashed into a forested region. The mission involved aerial refueling operations over German airspace prior to the return flight. While performing the final approach, the crew attempted a go-around maneuver. During this transition, the aircraft experienced a significant pitch-up motion, reaching an angle of 7.5 degrees before entering a stall and impacting the ground.

The accident resulted in the total destruction of the KC-135 Stratotanker and caused four fatalities, with no survivors among the crew.

Findings

Investigations into the accident suggest that the loss of control was triggered by a mechanical failure involving the runway trim motor. This component failed during the approach phase, an issue that went undetected by the flight crew. When engine power was increased during the go-around attempt, the malfunctioning motor caused the aircraft to pitch upward uncontrollably. The specific reason for the runaway trim motor has not been determined.

Probable cause

The crew lost control of the aircraft during a go-around because an undetected failure of the runway trim motor caused an uncommanded nose-up pitch.