Popular Articles

  1. AD 49-14-01 Elevator Connector Tube Fitting

    Inspect the fittings at each end of the elevator connector tube to determine if the end fittings are riveted to the tube with two rivets 90 degrees apart.
  2. AD 78-20-11 Aileron Control Malfunction

    Inspect the two aileron stop pins (Taylorcraft P/N A-235) of the aileron control assembly.
  3. AD 63-17-05 Landing Gear Shock Struts

    Steps to preclude weld separations on the end of the landing gear shock strut assembly.
  4. SM-29 Ercoupe Provision for Locking Cabin Windows

    Provisions for locking the sliding windows with or without the green sunshade.
  5. SB-40 Piper J-3 Outlet Reinforcement on 12 Gallon Fuel Tanks

    Installation of a reinforcing patch around the fuel outlet fitting of the fuel tank.
  6. SM-73 Piper PA-22 Nose Wheel Oleo Boot Assembly

    Installation of this boot will reduce the possibility of moisture accumulating between the oleo assembly and the oleo housing.
  7. FAR 8110.42 Parts Manufacturer Approval Procedures (Excerpts)

    Excerpts of FAR 8110.42 Parts Manufacturer Approval Procedures.
  8. SB-20 Alon/Forney/Mooney Cylinder Head Temperature Indicator

    Reports have been received indicating overheating of cylinder heads. To provide continuous indication of engine operating temperatures accomplish the following.
  9. SM-49A Ercoupe Detailed Inspection of Control Column Cable Assembly

    This memorandum is a supplement to Memorandum #49, covering the inspection of control column cables.
  10. SB 4-46 Luscombe Rudder Pedal Horn Inspection

    Checking the attachment of the rudder control arm on the torque tubes.