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Prevent flight controls malfunction including possible loss of control due to cable failure.
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Required inspection for incorrect swaging width of the cable Nicopress sleeves on the elevator, rudder, aileron, and flap control cables, and make a temporary POH limitation entry.
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Cross reference chart of original Piper part numbers mapped to current part numbers.
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Corrosion and pitting on control cable attachment fittings could lead to loss of some flight controls.
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Remove the tires and inspect the wheel flanges for fatigue cracks.
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Excerpt from FAA Order 8130.2F “Airworthiness Certification of Aircraft and Related Parts”
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How to detect cracks in the muffler assembly in Cessna model airplanes incorporating Piper Muffler Assembly P/N 10308-00 with the installation of a Lycoming engine.
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Last Updated: 10/08/2021
in Technical Information Ercoupe
Information regarding converting an Ercoupe 415-D to a 415-C.
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Steps to detect permanent deformation and/or cracks in the lower frame side tubes on the adjustable front seat.
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Method of effecting engine change for increased horsepower.