No fatalities

2004-09-21: Swearingen SA227 Metro III (C-FIPW) — Norcanair - North Canada Air — La Ronge, Canada

La Ronge, CanadaLanding (descent or approach)

On September 21, 2004, a Swearingen SA227 Metro III (registration C-FIPW) operated by Norcanair - North Canada Air was involved in an aviation accident near La Ronge, Canada during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: Findings as to Causes and Contributing Factors: 1. An incorrect roller of a smaller diameter and type was installed on the left main landing gear outboard bellcrank assembly, contrary to company and industry practice. 2. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 3 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781200134Data APIEditorial standards

A Metro III operated by Northern Dene Airways suffered a landing gear collapse during a crosswind landing at La Ronge, Saskatchewan, causing minor injuries to three passengers.

Accident Details

On a day visual flight rules flight, a Metro III aircraft, registration C-FIPW and serial number AC524, operated by Northern Dene Airways Ltd. as Norcanair Flight KA1051, departed Stony Rapids, Saskatchewan, with two crew members and nine passengers. The flight was destined for La Ronge, Saskatchewan.

Sequence of Events

Upon arrival at La Ronge at approximately 1410 central standard time, the crew completed the approach and landing checklists and confirmed the gear-down indication. The aircraft was landed on Runway 18 in a crosswind, touching down firmly approximately 1000 feet from the threshold. During the landing, the left wing dropped, causing the propeller to contact the runway. The aircraft veered to the left despite full rudder and aileron deflection. The crew applied maximum right braking and shut down both engines. The aircraft departed the runway and traveled approximately 200 feet through the infield before the nose and right main gear were torn rearward; the left gear collapsed into the wheel well. The aircraft slid on its belly and came to rest approximately 300 feet off the side of the runway.

Injuries and Damage

Three passengers sustained minor injuries from the sudden stop associated with the final collapsing of the landing gear. The other passengers and the pilots were not injured.

Probable Cause

The investigation identified three findings as to causes and contributing factors: (1) An incorrect roller of a smaller diameter and type was installed on the left main landing gear outboard bellcrank assembly, contrary to company and industry practice. (2) The smaller diameter roller reduced the required rigging tolerances for the bellcrank-to-cam assembly in the down-and-locked position and allowed the roller to eventually move beyond the cam cutout position, resulting in the collapse of the left landing gear. (3) A rigging check was not carried out after the replacement of the bellcrank roller. Such a check should have revealed that neither the inboard nor outboard bellcrank assembly met the minimum rigging requirements for proper engagement with the positioning cam.