WPR21LA318

Factual narrative

On August 12, 2021, about 1443 Pacific daylight time, a North American T-28B airplane, N392W, was substantially damaged when it was involved in an accident near Puyallup, Washington. The pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. The pilot reported that, after touchdown on runway 35 at Pierce County-Thun Field (PLU), the nose wheel started to shimmy, and he was not able to steer the airplane. The airplane veered to the left side of the runway as the pilot continued to try and steer away from the edge of the runway using the right brake. When the left main landing gear wheel went off the edge of the runway, he initiated the emergency procedures to retract the landing gear, shut down the engine and open the canopy. After the airplane came to a stop, a fire ignited the grass under the engine nacelle which was extinguished by emergency responders. The wings were substantially damaged. Examination of the wreckage revealed that the nose wheel steering components and the hydraulic shimmy damper appeared to remain intact and attached to their respective mounts. The shimmy damper piston rod was actuated by hand and found to compress and extend normally. No hydraulic fluid leaks were observed on the damper. No evidence of a pre-accident mechanical failure or malfunction was revealed that would have precluded normal operation. The pilot reported that, after touchdown the nose wheel started to shimmy, and he was not able to steer the airplane. The airplane veered to the left side of the runway as the pilot continued to try and steer away from the edge of the runway using the right brake. When the left main landing gear wheel went off the edge of the runway, he initiated the emergency procedures to retract the landing gear, shut down the engine and open the canopy. Examination of the wreckage revealed that the nose wheel steering components and the hydraulic shimmy damper appeared to remain intact and attached to their respective mounts. The shimmy damper piston rod was actuated by hand and found to compress and extend normally. No hydraulic fluid leaks were observed on the damper. No evidence of a pre-accident mechanical failure or malfunction was revealed that would have precluded normal operation. The reason for the nose wheel shimmy could not be determined from available evidence. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

FAA avdata. C = Cause, F = Factor.

• — Not determined-Not determined-(general)-(general)-Unknown/Not determined
• — Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Unknown/Not determined
• — Aircraft-Aircraft systems-Landing gear system-Shimmy damper-Unknown/Not determined