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Inspecting tail brace rod clevises attached to the fin for cracks and replacing wherever necessary.
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Failure of the fuel shut-off control attachment at the swivel fitting.
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Failure of the stabilizer rear bearing bracket as a result of improper or insufficient lubrication.
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Replacing fuselage tubes beneath the seats and floorboards due to damage.
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Inspection of the stabilizer aluminum yoke casting, and if any cracks are apparent, the part should be replaced before further operation of the airplane.
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Approved changes to make the heat control on the instrument panel more readily accessible for a pilot flying solo in the rear seat.
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Reworking of bottom cowl for replacing air scoop EQ5259 with EQ5370 (Continental part numbers).
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Inspect the lift strut clevis bolts for evidence of abuse. If such evidence is noted, the bolts shall be replaced.
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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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Installation of a new gasket with more cushioning properties to eliminate breakage of the glass fuel strainer bowl.