Casualties unknown

Helicopter Accident on Gulf of Mexico Oil Platform after Landing Skid Failure (N5753B)

W.cameron 266, US

On December 9, 1990, a Bell 206L-1 (registration N5753B) operated by Industrial Helicopters, Inc. was involved in an aviation accident near W.cameron 266. Investigators recorded the probable cause as: The failure of the right rear landing skid due to high cycle low stress fatigue. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 1 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-07-04Data APIEditorial standards

A helicopter's right rear landing skid collapsed on touchdown at an oil platform helipad, leading to a tail rotor strike, main rotor blade separation, and the fuselage spinning onto a lower deck. Metallurgical examination found fatigue failure.

Incident Overview

An ATP-rated helicopter pilot was conducting a landing on a helipad located atop an oil platform in the Gulf of Mexico. Upon touchdown, the right rear landing skid collapsed, causing the tail rotor to strike the deck. As the pilot applied collective pitch in an attempt to level the aircraft, the helicopter began to spin. The main rotor blades subsequently struck the deck and separated as the fuselage spun off the helideck, eventually coming to rest on a lower deck.

Metallurgical Findings

A metallurgical examination of the failed landing skid revealed that the structural failure was due to high cycle low stress fatigue. This type of fatigue typically occurs from repeated loading below the material's yield strength over many cycles.

Probable cause

The failure of the right rear landing skid due to high cycle low stress fatigue.

Frequently asked questions

What happened in the 9 Dec 1990 Bell 206L-1 accident near W.cameron 266?

A helicopter's right rear landing skid collapsed on touchdown at an oil platform helipad, leading to a tail rotor strike, main rotor blade separation, and the fuselage spinning onto a lower deck. Metallurgical examination found fatigue failure.

What aircraft was involved and where did it happen?

The accident on 9 Dec 1990 involved a Bell 206L-1, registration N5753B, operated by Industrial Helicopters, Inc., at W.cameron 266.

What was the probable cause of the accident?

The failure of the right rear landing skid due to high cycle low stress fatigue.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X24761. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.