Casualties unknown

Helicopter Accident During Offshore Passenger Flight (N811CE)

Huntington Bch, CA, US

On May 28, 1999, a Mbb BO 105LS A-3 (registration N811CE) operated by Southern California Edison was involved in an aviation accident near Huntington Bch, CA. Investigators recorded the probable cause as: The pilot's in-flight loss of control due to spatial disorientation while maneuvering to reverse direction after an inadvertent encounter with instrument meteorological conditions. 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 2026-06-10Data APIEditorial standards

A helicopter transporting two company employees to an island 22 miles offshore crashed into the ocean. The pilot was not instrument rated. Weather included low clouds and reduced visibility at the accident site. Radar data showed a series of turns and altitude changes before the final descent. No mechanical malfunctions were found.

Flight Purpose and Weather

The flight was intended to transport two company employees to an island located 22 miles offshore. The pilot held no instrument rating. Weather conditions along the coast featured overcast skies with cloud bases between 700 and 1,100 feet and tops between 1,900 and 2,200 feet, with visibilities generally ranging from 4 to 5 miles. Ground and pilot witnesses reported localized lower cloud bases of 350 to 500 feet and reduced visibilities of about 1.5 miles in the area of the accident site.

Radar Track Analysis

Review of recorded radar data revealed that the helicopter descended from a cruise altitude of 900 feet and crossed the shoreline at 400 feet. Upon reaching the accident site location, it climbed to 600 feet over 19 seconds, then turned right to a northerly heading while ascending from 600 to 900 feet. The turn radius was calculated at 720 feet at an average ground speed of 69 knots. Subsequently, the helicopter descended to 700 feet as the radar track initiated a wide left turn, which then reversed into a tight right turn. The last four radar returns showed a right turn with a 120-foot radius and a consistent Mode C altitude report of 700 feet. The average computed ground speed during this turn was 67 knots. The final radar return was a secondary beacon without a Mode C altitude report, located approximately 200 feet from where the wreckage was found on the ocean floor.

Wreckage Examination

Examination of the wreckage revealed no preimpact mechanical malfunctions or failures.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X18798. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.