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Inspect engine mount bolts, spacer, hose, bushings, cup washers, nut, pin, and engine mount seats for damage.
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Provisions for expelling water and gasoline from the forward belly regions of the aircraft for all normal parking attitudes.
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Recommended inspection of the sealing of firewall holes.
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Reports have been received indicating that movement of the nose gear can be restricted due to binding of the upper nose gear oleo bearing due to lack of lubrication.
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Partial or almost complete loss of rudder control of one or both rudders due to partial failure of the rudder horn attachments.
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The re-routing of the oil breather line will empty oil vapors almost directly to the outside of the airplane, helping to eliminate an excessively dirty engine compartment.
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Instructions for moving the Scott Brake cylinders from a position directly aft of the rear rudder pedals to a new position as shown in the attached sketches.
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Instructions to inspect the fuel tank filler caps for presence of a vent hole in the cap dome.
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Reports of malfunctioning steerable tail wheels caused by the tail wheel arm striking the end of the tail wheel installation bolt.
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Solution for fuel line installation that is too close to the valve.