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Directions to prevent failure of the upper wing front spar strut fittings, P/N 2-1976, that could result
in an in-flight separation of the wing.
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Due to recurring failures of the control cables, all cables should be carefully inspected at each section which passes either over a pulley or through a fairlead.
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Steps to prevent weakening of the fuselage steel tubing cluster in the area of the rear wing spar attachment due to corrosion of the fuselage tubing.
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Correction to the PA-12 Weight and Balance Form regarding the propeller installation arm.
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Last Updated: 10/08/2021
in Technical Information Cessna
Control surface balance limits for early model Cessna airplanes.
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Required inspection of the rear seat back hinge areas for cracking and excessive elongation of the rear seat hinge bolt hole and replacement of the rear seat frame if necessary.
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Drawing for the Piper PA-18 150hp Primer System.
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Rigging and leveling procedures for Piper J-3 Cub Special and PA-11 aircraft.
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Cross reference chart of old Van Sickle part numbers to modern Cleveland mechanical brake and wheel part numbers.
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Modification for installing Silflex jack strut.