Several Piper PA-28 series aircraft experienced critical mechanical failures, including a broken throttle cable during flight, and issues with flap cables and nose gear components.
Structural integrity concerns were identified, such as a severely corroded seat track, a cracked wing channel, and hidden cracks in an ELT mounting bracket.
Some defects, like the nose gear bumper, showed recurring failures, while others like the corroded seat track or cracked ELT bracket involved hidden damage, emphasizing the need for thorough inspections.
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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