Casualties unknown

2001-12-03: Cessna 152 C-GJKE — Pacific Professional Visual Flight Training — Boundary Bay Airport, British Columbia, CA

Boundary Bay Airport, British Columbia, CA

On December 3, 2001, a Cessna 152 C-GJKE operated by Pacific Professional Visual Flight Training was involved in an aviation accident near Boundary Bay Airport, British Columbia, CA. Investigators recorded the probable cause as: The aircraft exhibited uncontrollable flight characteristics at lift-off due to restricted right rudder movement caused by an anomaly in the right-hand nosewheel steering tube assembly. This summary draws on records from the Transportation Safety Board of Canada (TSB).

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

A student pilot's solo flight ended in a runway excursion at Boundary Bay Airport after a Cessna 152 experienced a severe, uncommanded left yaw during takeoff.

What happened

During a solo training flight at Boundary Bay Airport, a Cessna 152, registration C-GJKE, experienced a sudden and severe left yaw immediately upon lifting off from Runway 12. The student pilot, who was performing circuits as part of a private pilot training program, found that while left rudder control remained functional, the right rudder could not be applied to counteract the deviation.

Despite attempting to use aileron inputs to stabilize the aircraft, the plane continued a left turn of approximately 180 degrees at an altitude of about 80 feet. The pilot declared an emergency and attempted to land on Runway 25. The aircraft touched down at an angle on the runway and veered into the grass. As the aircraft traveled through a swale, the nose gear collapsed, causing the plane to come to a stop on its nose. There were no injuries resulting from the incident.

The investigation

Investigators examined the aircraft's flight control systems, including the rudder, control cables, and pedals, finding no obvious anomalies in their general operation. The investigation also looked into whether items in the cockpit, such as the pilot's footwear or objects falling from the passenger seat, had jammed the pedals, but these possibilities were dismissed.

Technical focus shifted to the nosewheel steering tube assemblies. While the left-hand assembly functioned normally, the right-hand assembly was found to be operating differently. Specifically, a spring and a bent spring retainer washer were identified within the right-hand unit. Although testing showed the unit could still withstand design loads even in its damaged state, the investigation could not definitively determine if this internal damage occurred during the accident or if it was a pre-existing condition.

Probable cause

The aircraft exhibited uncontrollable flight characteristics at lift-off due to restricted right rudder movement caused by an anomaly in the right-hand nosewheel steering tube assembly.