Accident Sikorsky S-76A C-GIMF, Friday 30 April 1982
ASN logo
 
This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. You can contribute by submitting additional or updated information.

Date:Friday 30 April 1982
Time:
Type:Silhouette image of generic S76 model; specific model in this crash may look slightly different    
Sikorsky S-76A
Owner/operator:Okanagan Helicopters
Registration: C-GIMF
MSN: 760038
Total airframe hrs:2255 hours
Fatalities:Fatalities: 13 / Occupants: 13
Other fatalities:0
Aircraft damage: Destroyed
Category:Accident
Location:105 km NNE off Songkhla, Gulf of Thailand -   Thailand
Phase: En route
Nature:Offshore
Departure airport:Songkhla
Destination airport:Erawan LQ
Confidence Rating: Information is only available from news, social media or unofficial sources
Narrative:
An Okanagan Helicopters Sikorsky S-76 crashed in the Gulf of Thailand, killing all 13 occupants.

The helicopter departed 07:13 for a gas field in the sea. The flight was heading 020 degrees at 5000 ft and cruising at 130 kt. The pilot reported check point A at 07:30 and estimated check point B at 07:44. At 0744 the pilot transmitted a mayday and reported partial loss of tail rotor control. He entered autorotation and slowed to 90 kt, but was unable to stop the aircraft from rotating. His last transmission was at 1000 ft. Debris and an oil slick were found at lat. 08 deg 06 min n long. 100 deg 57 min e.
The wreckage was retrieved from the sea 6 days after the accident. The left tail rotor control cable was fractured due to a combination of wear, rapid fatigue and tensile overload, probably caused by improper rigging.

Crashed into sea following loss of tail rotor control. A tail rotor control cable had been routed over a stainless steel grommet in the area of pulleys (2) under the Main Gear Box. The bracket holding these pulleys did not allow for visual confirmation of the routing. With a broken tail rotor control cable at that time, the tail rotor went immediately to full pitch, a condition from which a recovery was not possible.

A self centering device like that of the H-60 was later added which, under the same circumstances, would result in the T/R centering allowing a run-on landing to be performed. In September 1983 a US-registered S-76 (N521AC) ditched in Lake Michigan following loss of tail rotor control.


Sources:

World Airliner Crashes/Terry Denham
https://www.flightglobal.com/FlightPDFArchive/1982/1982%20-%201844.PDF


Similar issue https://assets.publishing.service.gov.uk/media/5422f213ed915d13740003d5/dft_avsafety_pdf_501789.pdf

Location

Revision history:

Date/timeContributorUpdates
27-Sep-2008 01:00 ASN archive Added
11-Jun-2010 12:20 TB Updated [Aircraft type, Other fatalities, Phase, Nature, Source, Narrative, ]
02-Jun-2012 01:51 Anon. Updated [Departure airport, Destination airport, ]
01-Nov-2016 13:30 Owenthai Updated [Narrative, ]
12-Jul-2019 21:31 Aerossurance Updated [Nature, Source, Narrative, ]
15-Feb-2025 09:48 ASN Updated [Location, Nature, Narrative, Category, ]
30-Apr-2025 08:09 Aerossurance Updated [Source, ]

Corrections or additions? ... Edit this accident description

The Aviation Safety Network is an exclusive service provided by:
Quick Links:

CONNECT WITH US: FSF on social media FSF Facebook FSF Twitter FSF Youtube FSF LinkedIn FSF Instagram

©2025 Flight Safety Foundation

1920 Ballenger Av, 4th Fl.
Alexandria, Virginia 22314
www.FlightSafety.org