Piper PA-28 series aircraft experienced diverse mechanical failures, including critical in-flight issues such as a broken throttle cable and broken flap cable strands.
Significant structural degradation was reported across various models, encompassing corroded seat tracks, cracked wing channels, and a cracked ELT mounting bracket.
Landing gear components, particularly the nose gear, exhibited notable weaknesses with a bumper failing repeatedly and a broken downlock pin assembly leading to an emergency.
During flight, when the pilot attempted to reduce engine power, the throttle cable broke, leaving the engine stuck at cruise power. The mixture control was used overhead the airport to reduce power and land without incident.
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