Stinson 108 Series

Blade retaining flanges, P/N 3277 must be replaced with P/N 3277-1.

Reports of fuel seepage into the space between the inner cabin trim and the outer fabric covering of the fuselage.

Reports of broken core strands in the rudder cables where they pass over the pulley at fuselage Station 18.75.

Steps to prevent wing fabric loosening along the upper surface of the front and rear spars in the area of the fuel tank causing a spoiler action.

Inspection of the stabilizer leading edge attachment to the fuselage should be made for fatigue cracks.

The front ash trays shall be modified to the self-contained type or a "No Smoking" placard installed.