Popular Articles

  1. AD 72-20-06 Aerobatic Flight Placard

    Prevent flight controls malfunction including possible loss of control due to cable failure.
  2. 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.
  3. Piper Generic Numbers Sorted by Current Part Number

    Cross reference chart of original Piper part numbers mapped to current part numbers.
  4. SL-1069 Piper Flight Control Cable Terminal Corrosion Inspection

    Corrosion and pitting on control cable attachment fittings could lead to loss of some flight controls.
  5. AD 48-08-02 Cleveland Wheels

    Remove the tires and inspect the wheel flanges for fatigue cracks.
  6. FAR 8130.2F Data Plate Replacement

    Excerpt from FAA Order 8130.2F “Airworthiness Certification of Aircraft and Related Parts”
  7. AD 69-15-03 Cracks in Muffler Assembly

    How to detect cracks in the muffler assembly in Cessna model airplanes incorporating Piper Muffler Assembly P/N 10308-00 with the installation of a Lycoming engine.
  8. Conversion of Ercoupe 415-D to 415-C Designation

    Information regarding converting an Ercoupe 415-D to a 415-C.
  9. AD 76-22-01 Adjustable Front Seat

    Steps to detect permanent deformation and/or cracks in the lower frame side tubes on the adjustable front seat.
  10. SB Luscombe Engine Change to More Horsepower

    Method of effecting engine change for increased horsepower.