28 fatalities

1954-09-05: Lockheed L-1049 Super Constellation (PH-LKY) — KLM Royal Dutch Airlines - Koninklijke Luchtvaart Maatschappij — Shannon, Ireland

Shannon, IrelandTakeoff (climb)

On September 5, 1954, a Lockheed L-1049 Super Constellation (registration PH-LKY) operated by KLM Royal Dutch Airlines - Koninklijke Luchtvaart Maatschappij was involved in an aviation accident near Shannon, Ireland during takeoff. 28 people were killed. Investigators recorded the probable cause as: The pilot failed to properly interpret instrument indications during flap retraction, a situation worsened by the unexpected re-extension of the landing gear which reduced aircraft performance. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781251848Data APIEditorial standards

A four-engine aircraft crashed into the Shannon Estuary shortly after departing Shannon Airport, resulting in 28 fatalities.

What happened

During a nighttime departure from runway 32 at Shannon Airport, the Triton four-engine aircraft began its ascent but reached a peak altitude of only 260 feet. While traveling at a speed of 155 knots, the aircraft entered a slight nose-down attitude. This maneuver led to a continuous descent that ended in a crash into the Shannon Estuary, located roughly 8,170 feet from the end of the departure runway. The impact occurred approximately 35 seconds after the aircraft had left the ground. The accident resulted in 28 fatalities and 28 survivors, with the aircraft being completely destroyed.

Findings

Investigations into the accident identified several critical factors. A primary contributor was the pilot's failure to correctly interpret instrument readings during the process of retracting the flaps, which prevented timely corrective actions. This difficulty in monitoring instruments was compounded by the unexpected and unintended re-extension of the landing gear. The subsequent loss of aircraft performance due to this gear movement, combined with the pilot's failure to maintain an adequate climb gradient, left no margin to recover from these unforeseen mechanical and operational issues.

Probable cause

The pilot failed to properly interpret instrument indications during flap retraction, a situation worsened by the unexpected re-extension of the landing gear which reduced aircraft performance.