Casualties unknown

Helicopter Ditching After Power Loss Off Gulf of Mexico Drill Rig (N514EH)

E Cameron Blk 2, US

On November 12, 1984, a Bell 206L-1 (registration N514EH) was involved in an aviation accident near E Cameron Blk 2. Investigators recorded the probable cause as: Total loss of power after takeoff from a high drill rig platform, compounded by the failure of the emergency flotation gear to inflate prior to rollover. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-06-23Data APIEditorial standards

A helicopter suffered total power loss shortly after takeoff from a high drill rig in the Gulf of Mexico. The pilot attempted an autorotation but crashed hard, causing the aircraft to roll over.

What happened

The incident occurred when the helicopter experienced a total loss of power shortly after lifting off from a drill rig platform situated approximately 130 feet above the water in the Gulf of Mexico. Following the sudden failure, the pilot initiated an autorotation to maintain control and attempt a safe landing on the water below. However, the subsequent touchdown during the ditching maneuver was hard, which caused the helicopter to roll over upon impact.

The investigation

Post-accident testing was conducted to determine the root cause of the power failure. These examinations did not reveal any evidence of mechanical failure or malfunction within the aircraft systems prior to the event. This finding suggests that the loss of power was likely due to an external factor or operational issue rather than a pre-existing defect in the helicopter's mechanics.

Findings

Several critical factors contributed to the outcome of this accident. The primary cause was the total loss of power immediately after takeoff, which left the pilot with limited options for recovery. Additionally, the emergency flotation gear did not fully inflate until after the helicopter had already rolled over, rendering it ineffective in preventing the rollover or ensuring buoyancy during the initial impact. The hard touchdown during the ditching phase resulted in significant structural stress, leading to the final position of the aircraft.

Probable cause

Total loss of power after takeoff from a high drill rig platform, compounded by the failure of the emergency flotation gear to inflate prior to rollover.

Frequently asked questions

What happened in the 12 Nov 1984 Bell 206L-1 accident near E Cameron Blk 2?

A helicopter suffered total power loss shortly after takeoff from a high drill rig in the Gulf of Mexico. The pilot attempted an autorotation but crashed hard, causing the aircraft to roll over.

What aircraft was involved and where did it happen?

The accident on 12 Nov 1984 involved a Bell 206L-1, registration N514EH, at E Cameron Blk 2.

What was the probable cause of the accident?

Total loss of power after takeoff from a high drill rig platform, compounded by the failure of the emergency flotation gear to inflate prior to rollover.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001214X41566. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.