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Instructions for compliance with Marvel-Schebler Division Bulletin No. A1-69.
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Pertains to the inspection of the Single Belt Driven Ring Gear Support Assembly as installed on the affected aircraft above.
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A recent design change to the fuel tank caps has created a possible hazard to the venting system and it is therefore requested that the caps be reworked in the following manner.
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Reports of the vacuum pump splined coupling on Airborne Mechanisms Vacuum Pumps Models 113A5 and 113A8 may fail prematurely as a result of over-curing.
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Instructions for an inspection of the vacuum pump adapter drive assembly.
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Tightening engine mounting bolts to obtain a torque of (40) inch pounds.
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Servicing instructions for the carburetor air filter with paper cartridge.
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Misalignment of the oil radiator lines on the Lycoming 0-290-D2 135 horsepower engines at the point where they pass through the rear engine baffle.
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Correction to the fuel grade specification in flight manuals and fuel tank placards for the Lycoming O-290-D2 engines.
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Inspecting for weld separation where the rudder pedal cable attachment fitting is welded to the rudder pedal.