Casualties unknown

Sikorsky S-76A Tail Rotor Failure During Training Flight at London International Airport

London, Ontario, CA

On September 17, 2002, a Sikorsky S-76A (Helicopter) C-GIMM operated by Canadian Helicopters Limited was involved in an aviation accident near London, Ontario, CA. Investigators recorded the probable cause as: The hard landing, caused by the pilot flying raising the collective for a two-engine landing while the number 2 engine was at flight idle, resulted in a high rate of descent that buckled the tail boom and severed the tail rotor drive shaft during subsequent… This summary draws on records from the Transportation Safety Board of Canada (TSB); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Transportation Safety Board of Canada (TSB)Primary reportUpdated 2026-09-13Data APIEditorial standards

A Sikorsky S-76A helicopter, C-GIMM, suffered a tail rotor failure during a training flight at London International Airport, Ontario, after a hard landing damaged the tail boom.

Incident Overview and Flight History On the day of the incident, two qualified pilots departed from London International Airport in Ontario at approximately 1530 EDT in a Sikorsky S-76A helicopter, registration C-GIMM, serial number 760044. The aircraft was operated by the Emergency Medical Services Division of Canadian Helicopters Limited. The flight was conducted for crew training purposes, specifically to prepare for a pilot proficiency check. The crew performed multi-engine exercises in the local area before returning to the airport to conduct simulated one-engine-inoperative exercises involving take-offs and landings across the button of Runway 27. During the second approach, the pilot flying raised the collective in the normal manner for both engines operative, unaware that an engine failure had been simulated on the number 2 engine. This resulted in a decay in rotor speed and a touchdown at a higher than normal rate of descent. The pilot not flying attempted to regain power from the simulated inoperative engine, but the number 2 engine did not respond quickly enough to avoid a hard landing. The tail boom of the helicopter buckled on impact, bringing the tail rotor drive shaft into contact with internal structure. The crew was unaware of the structural damage but felt a buzz in the anti-torque pedals, which might have indicated that a main rotor blade had hit the tail rotor. Consequently, they terminated the flight and began to ground taxi back to the company ramp. While taxiing, the tail rotor failed when the drive shaft was cut through. The accident occurred at approximately 1630 EDT.

Probable cause

The hard landing, caused by the pilot flying raising the collective for a two-engine landing while the number 2 engine was at flight idle, resulted in a high rate of descent that buckled the tail boom and severed the tail rotor drive shaft during subsequent ground taxi.