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Replacing the shimmy dampener currently installed in the affected model aircraft with new shimmy dampener, part number 13086-00, and instructions for continuing maintenance at regular intervals.
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Remove the tires and inspect the wheel flanges for fatigue cracks.
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Downloadable paint scheme sheet for Piper J-3.
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General specifications and performance data for the Piper Vagabond PA-15 and the Piper Vagabond Trainer PA-17.
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Steps to prevent the possible loss of elevator trim control.
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Required inspection of the rear seat back hinge areas for cracking and excessive elongation of the rear seat hinge bolt hole and replacement of the rear seat frame if necessary.
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Excerpt from FAA Order 8130.2F “Airworthiness Certification of Aircraft and Related Parts”
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The compliance time for inspection of lift strut assemblies is changed from every 5 years to every 12 months.
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Last Updated: 10/08/2021
in Technical Information Cessna
Control surface balance limits for early model Cessna airplanes.
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Excerpt of FAR Part 43 Maintenance, Preventive Maintenance, Rebuilding, and Alteration.