New Articles

  1. AD 46-23-03 Aileron Control Column Fitting

    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.
  2. AD 90-15-15 R1 Front Spar Strut Fittings

    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.
  3. AD 74-15-07 Propeller Mounting

    Verify that the propeller is properly indexed to the crankshaft flange.
  4. AD 2004-19-01 Upper Shoulder Harness Adjusters

    Inspect and, if necessary, modify the pilot/co-pilot upper shoulder harness adjusters that have certain Cessna accessory kits incorporated.
  5. AD 80-21-06 Muffler Core and Body Assembly

    Prevention of a degradation of the induction system icing protection or partial engine power loss.
  6. AD 46-23-01 Muffler Replacement

    Replacing the original muffler on the serial numbers listed above with a new muffler.
  7. AD 79-08-03 Electrical System Failure

    How to prevent an inflight electrical system failure, smoke in the cockpit, and/or fire in the wire bundle behind the instrument panel.
  8. AD 55-24-01 Corrosion Inspection

    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.
  9. AD 61-25-01 Unsafe Condition in Main Gear

    Steps to correct an unsafe condition in the main gear (Met-Co-Aire Tricycle Landing Gear).
  10. AD 62-24-03 Cabin Heat System

    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.