-
Due to the possibility of a defective fitting on the upper end of the control column shaft in the aileron control system, the system should be tested to a load of 94 pounds.
-
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.
-
Verify that the propeller is properly indexed to the crankshaft flange.
-
Inspect and, if necessary, modify the pilot/co-pilot upper shoulder harness adjusters that have certain Cessna accessory kits incorporated.
-
Prevention of a degradation of the induction system icing protection or partial engine power loss.
-
Replacing the original muffler on the serial numbers listed above with a new muffler.
-
How to prevent an inflight electrical system failure, smoke in the cockpit, and/or fire in the wire bundle behind the instrument panel.
-
Extreme surface corrosion has been found to exist inside the fuselage spar carry through structures of Luscombe Series 8 aircraft, particularly in those airplanes located near coastal areas.
-
Steps to correct an unsafe condition in the main gear (Met-Co-Aire Tricycle Landing Gear).
-
Failures of the exhaust stacks have occurred in the area of the cabin heat muffs, causing hazardous carbon monoxide contamination of the cabin when cabin heat is used.