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Flight Safety Crest Epilogue
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Aircraft Accident Summary
Incident photo

Type: CH12404 SEA KING

Date: 19 July 1999

Location: Shearwater, NS

The crew of aircraft CH124A404 had just returned from a crew operational readiness exercise (COREX) and was in the process of shutting down on the Shearwater ramp. After rotor disengagement, three crewmembers deplaned, leaving the Co-pilot and the Navigator to conduct the remainder of the shutdown procedure. After attempting to cycle the rotor brake in accordance with the checklist procedure, smoke and flame developed in the forward part of the main gearbox. The ground crew advised the co-pilot of the fire and an emergency shutdown was performed. The co-pilot was unable to reselect the manual rotor brake. The ground crew commenced fighting the fire using four 50 lbs. dry chemical extinguishers retrieved from the surrounding area. The 12 Wing fire fighters arrived shortly thereafter with the foam truck and quickly extinguished the blaze. The aircraft suffered "B" category damage to the engine compartments and main gearbox area. There were no injuries in this occurrence.

The investigation concluded that improper installation of the rotor brake hydraulic line during MGB installation was responsible for the hydraulic line being in contact with the rotor brake accumulator housing. The automatic rotor brake pressure line chafed against the "rotor brake panel package accumulator housing" ultimately causing the line to rupture under pressure. Furthermore,the location of the hydraulic line and the lack of mandated opportunistic inspections made timely detection through routine inspection extremely unlikely.

Atomised hydraulic fluid from the damaged hydraulic line contacted the #2 engine exhaust cowling and ignited.

In response to recommendations made by the investigation team, maintenance personnel were briefed on their responsibilities during an aircraft ground fire and the Canadian Forces Fire Marshal is investigating a possible replacement of the portable fire extinguisher, with a more effective type of agent.

It was also recommended that

  1. 12 Wing staff evaluate the benefits of equipping the local aircraft recovery crew with fire extinguishing equipment;

  2. 1 CAD investigate the feasibility of replacing the 50 Lbs. Dry Chemical extinguisher with the compressed air foam type extinguisher;

  3. DGAEPM consider procedures and/or orders which would decrease the probability of improper routing and clamping and increase the probability of detecting errors in routing and clamping - with priority given to helicopters of the same vintage as the Sea King;

  4. 1 CAD Orders be reviewed to identify regulations that may have been rendered confusing or impractical by changes to Sea King Operating procedures.



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   Date modified: 2003-10-02
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