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Procedure for Installation of 180hp Franklin 6A335-B1 engine in lieu of original Franklin 6A4-165-B3.
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Inspection to determine if fatigue cracks have developed in the fitting that attaches the horizontal stabilizer to the fin.
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The following repair procedure is recommended for those aircraft on which the hole in the elevator tab control horn has elongated.
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Inspection of rudder skins at points immediately adjacent to the upper and lower ends of the rudder tab hinge for cracks.
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Inspection procedure for determining if rudder cables have frayed due to misalignment of the pulley brackets located on the fuselage structure.
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Parts list for Stinson 108-3901001 Float Fitting Kit.
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How to determine whether or not the core strands of the rudder cables are broken.
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Relocating the battery vent tube to prevent the acid vapors from attacking the paint on the landing gear fairing.
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Covers modifications on the Aeromatic F200/00-76B propeller to reduce exposure to a condition that causes fatigue stress.
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It has come to our attention that 108 series aircraft certified in the "Utility" and "Aerobatic" category do not conform to the pertinent C.A.R. Regulations due to lack of exits which will permit all occupants to bail out quickly with a parachute.