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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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Requires inspecting the front and rear wood spars for damage, including installing any as-needed inspection holes; and repairing or replacing any damaged wood spar.
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Wing separation from the airplane after the wing strut attach fitting failed due to corrosion.
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Powder coating of aircraft wing struts.
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Created On: 09/02/2021
in PMA Supplement List
Download the PDF spreadsheet of all FAA Parts Manufacturing Approval eligible parts available from Univair. You will need the free Adobe Acrobat Reader to view this file. Once you have opened the file, you can search for a particular part number by ...
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Information regarding piston pin plug replacement during engine overhaul.
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The use of standard inspection methods to determine any presence of unauthorized holes or cracks in the main spar assembly or any components thereof.
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