Popular Articles

  1. AD 60-01-07 Tail Brace Wires

    Steps to prevent the possibility of a catastrophic accident in the event of tail brace wire failure.
  2. 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.
  3. AD 96-24-17 R1 Wing Inspection Holes

    Installing new inspection holes, modifying the wing tip fairings, and inspecting the wing spars for intergranular corrosion.
  4. AD 2005-24-10 Pilot's Operating Handbook Limitation

    Required inspection for incorrect swaging width of the cable Nicopress sleeves on the elevator, rudder, aileron, and flap control cables, and make a temporary POH limitation entry.
  5. SM-08 Piper PA-12 Rigging Procedure

    Rigging and leveling procedures for Piper PA-12.
  6. SL-1135 Piper Control Cable and Pulley Inspection

    Over time, a chafing condition resulting from the control cable sliding against the stationary pulley groove can cause the control cable to wear completely through, possibly resulting in loss of aileron control during flight.
  7. SM-49 Piper PA-15/PA-17 Specifications and Performance

    General specifications and performance data for the Piper Vagabond PA-15 and the Piper Vagabond Trainer PA-17.
  8. Piper J-3 Paint Scheme

    Downloadable paint scheme sheet for Piper J-3.
  9. SL-233 Piper Fuel Selector Valve

    The new Fuel Selector Valve, part number 11383-04, should be used for all service replacements and all new installations on Piper PA-18, PA-20 and PA-22 airplanes equipped with two wing fuel tanks.
  10. 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.