New Articles

  1. AD 73-15-05 Hopper Bay Longerons Cracks

    Inspection of the left and right upper longerons for cracks using the dye penetrant technique.
  2. AD 65-15-05 Elevator Control System

    Steps to prevent loss of the elevator control system as a result of worn clevis bolts.
  3. AD 50-34-01 Retaining Flanges

    Blade retaining flanges, P/N 3277 must be replaced with P/N 3277-1.
  4. AD 49-16-02 Wing Fabric Inspection

    Steps to prevent wing fabric loosening along the upper surface of the front and rear spars in the area of the fuel tank causing a spoiler action.
  5. AD 2008-09-18 Wing Strut Attach Fittings

    Wing separation from the airplane after the wing strut attach fitting failed due to corrosion.
  6. AD 75-18-05 Engine Mount Bolts

    Inspect engine mount bolts, spacer, hose, bushings, cup washers, nut, pin, and engine mount seats for damage.
  7. AD 47-50-12 Stabilizer Attachment Fitting

    Inspection of the stabilizer leading edge attachment to the fuselage should be made for fatigue cracks.
  8. AD 47-13-02 Fuel Hose

    Examine the two flexible fuel lines to determine whether the hose inner liner has collapsed or failed thus causing a restriction to the flow of fuel.
  9. SAFO 10018 Powder Coating of Sealed Lift Struts

    Powder coating of aircraft wing struts.
  10. AD 67-24-02 Engine Fuel Starvation

    To forestall the possibility of engine fuel starvation during takeoff operations, install a placard on the right fuel quantity gauge.