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Cleveland Wheel and Brake eligibility list per LPC Bulletin 1675 (Rev. A) for Piper aircraft models J-3 thru PA-22.
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Corrosion between the aluminum terminal and aluminum wire at the battery positive post, resulting in overheating of the wire due to high electrical resistance.
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Required operation limitations for 75HP model 415-C, per supplement No. 6 of FAA No. 43 dated August 15, 1942.
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Inspection of front and rear control stick socket castings for cracks at the ears to which the push-pull tube attaches.
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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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Prevent flight controls malfunction including possible loss of control due to cable failure.
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Provides inspection and fatigue life requirements applicable to the wing lift strut forks.
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Required inspections of the ailerons, aileron balance assembly, and aileron rigging for looseness or wear, and required repair or replacement of parts as necessary.
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Last Updated: 09/23/2021
in Safety Alerts For OperatorsPowder coating of aircraft wing struts.
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Possibility of the fuel valve detent pins in a few valves were improperly centered, thus preventing positive indication of valve position.