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Directions to prevent failure of the upper wing front spar strut fittings, P/N 2-1976, that could result
in an in-flight separation of the wing.
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Verify that the propeller is properly indexed to the crankshaft flange.
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Inspect and, if necessary, modify the pilot/co-pilot upper shoulder harness adjusters that have certain Cessna accessory kits incorporated.
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How to prevent an inflight electrical system failure, smoke in the cockpit, and/or fire in the wire bundle behind the instrument panel.
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Steps to correct an unsafe condition in the main gear (Met-Co-Aire Tricycle Landing Gear).
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Inspect wing drag wire system for loose or broken drag wires and inspect ribs for damage.
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Inspect the two bolts attaching the horizontal stabilizer to the fin post for tightness and proper length.
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Refers to the various Airplane Flight Manuals which are required equipment for landplane, skiplane, and seaplane, and must be carried in the aircraft at all times.
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Inspect for fatigue cracks in the elevator spar web at the hinges.
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Replacing U.S. Rubber Co. flexible ducts installed in the carburetor hot air system with P-208-S duct or P-208 duct coated with neoprene.