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Article from the August 2019 issue of Coupe Capers, by author Bob Kachergius "The Stromberg Specialist".
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Compromised structural integrity of the fuselage due to excessive rust and corrosion between steel tubing and preformed sheet steel material.
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Instructions to provide an alternate source of fuel tank venting in case of fuel tank vent obstruction by foreign material and/or sticking of the fuel vent valve.
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Checking fuel selector valve for ease of rotation and instructions for lubricating.
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Replacement of front lift strut wing attachment fittings to prevent failure of lift strut wing fitting due to tie-down loads.
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Instructions for installing shock cords on Piper PA-12 and PA-14 aircraft.
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The following is cited from LPC Bulletin 1033, the installation instructions for the PA-22 taildragger conversion.
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Spar repair information for Piper aircraft with aluminum spars.
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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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Cleveland Wheel and Brake eligibility list per LPC Bulletin 1675 (Rev. A) for Piper aircraft models J-3 thru PA-22.