Piper PA-28 series aircraft experienced various structural integrity issues, including cracked wing channels, ELT mounting brackets, and corroded seat tracks often linked to environmental exposure.
Control system malfunctions were reported, such as a broken throttle cable that left an engine stuck at cruise power, and fractured flap cable strands.
Several recurring landing gear component failures were identified, including a frequently breaking nose gear bumper and a broken nose gear downlock pin assembly.
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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