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Improper maintenance of the wing fabric causing wing panel failures, resulting in serious Ercoupe accidents.
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Modification of the cabin heat box plate to prevent interference with the movement of the safety belt attaching link.
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The following installations have been FAA approved in the field. The party securing the approval is also listed.
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Revises compliance time, purpose, and instructions for inspection and/or replacement of wing lift strut assembly. Also announces the availability of new sealed lift struts.
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Approximate material required to recover Piper J-3, PA-11, PA-15, PA-17 and PA-18 aircraft using raw fabric and cellulose acetate butyrate dope.
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Subject: Typical and maximum number of exposed strut threads as permitted for rigging on Piper aircraft. Applicability: Piper J-3, J-4, J-5, and PA-11 through PA-22 Download PDF: Lift-Strut-Fork-Extension.pdf Piper Strut Thread (Typical ...
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Installing an additional standard fuse (15A Bussman #AGC-15) in the wire between the cigar lighter and the ammeter at the next 100 hour inspection to protect against a short circuit condition.
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Possibility of loss of fuel and hydraulic oil and fire in flight caused by chafing of these lines between the firewall and muffler.
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Reinforcement of the stabilizer adjustment yokes due to cracks in the tubular stubs.
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Parts list for Stinson 108-3042450 Bungee Kit.