Casualties unknown

2009-03-03: Swearingen SA226-TC Metro II C-FSLZ — Perimeter Aviation Ltd. — Winnipeg, Manitoba, CA

Winnipeg, Manitoba, CA

On March 3, 2009, a Swearingen SA226-TC Metro II C-FSLZ operated by Perimeter Aviation Ltd. was involved in an aviation accident near Winnipeg, Manitoba, CA. Investigators recorded the probable cause as: The right main landing gear failed to extend because the number three tire caught on a ledge of the inboard gear door. This summary draws on records from the Transportation Safety Board of Canada (TSB); 1 related events involving the same aircraft type or operator are linked below.

Sourcesthe Transportation Safety Board of Canada (TSB)Primary reportUpdated 1785068748Data APIEditorial standards

A Swearingen SA226-TC Metro II experienced a landing gear failure during approach to Winnipeg, resulting in a belly landing with no injuries.

What happened

On a flight from St. Theresa Point, Manitoba, to Winnipeg, a Swearingle SA226-TC Metro II, registration C-FSLZ, was performing its final approach to Winnipeg/James Armstrong Richardson International Airport. The aircraft, operated by Perimeter Aviation Limited as PAG Flight 640, was carrying two crew members and eight passengers. During the approach, the crew attempted to extend the landing gear, but the right main gear failed to lock into position, remaining in-transit.

After a missed approach and an attempt to use emergency extension methods, the crew determined the gear could not be deployed. They declared an emergency and prepared for a gear-up landing on Runway 18. Prior to touchdown, the crew shut down both engines and feathered the propellers. The aircraft landed on its belly along the runway centerline. Despite substantial damage to the propellers, flaps, and the aft belly of the aircraft, there were no injuries among the ten people on board.

The investigation

Investigators examined the aircraft's landing gear mechanism and found that the right main gear was obstructed. Specifically, the number three tire was caught on a ledge on the inboard gear door skin, preventing full extension. The investigation focused on the maintenance history of the gear doors and the dimensions of the tires used.

It was determined that the right inboard landing gear door had been rigged too tightly following maintenance work performed in September 2008. There was no documented evidence that a required rigging check had been performed after that work. Furthermore, the investigation looked into the dimensions of the recently replaced re-capped tire, which had grown in diameter during its first 73 cycles of service to a size that exceeded the dimensions of the previous tire.

Probable cause

The right main landing gear failed to extend because the number three tire caught on a ledge of the inboard gear door. This was caused by the combined effects of incorrectly rigged gear doors, the installation of a larger-than-average re-capped tire, increased free play in the gear door bushings, and air loading on the doors.