New Articles

  1. SL-406 Piper PA-20/PA-22 Revision to Owner's Handbook

    Correction to Owner's Handbooks for the listed models.
  2. SM-25 Piper PA-20/PA-22 Approximate Materials to Recover

    Approximate amount of materials required to recover PA-20 and PA-22 models using raw fabric and cellulose acetate butyrate dope.
  3. SM-60 Piper PA-22 Specifications and Performance

    Specifications and performance data for Piper PA-22 "125" and "135" airplanes.
  4. 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.
  5. SB P-2 Univair Inspection of Landing Gear Hydrasorb Shock Struts

    Procedure for examining both left and right Univair hydrasorb (U486-604-1) for any possible cracks or irregularities.
  6. SB P-1 Univair Throttle Inspection in Piper Airplanes

    Steps to preclude failure of the U12694 series throttle cables, which could cause loss of full travel of the throttle control.
  7. AD 72-20-06 Aerobatic Flight Placard

    Prevent flight controls malfunction including possible loss of control due to cable failure.
  8. SB-01 Alon Engine Breather Fitting

    To reduce the amount of oil passing through the breather tube and exhausting on the under-side of the aircraft, Continental Motors Corporation has a newly designed engine fitting which extends further into the engine case.
  9. SB-02 Alon Alternate Air Source

    In order to supply an alternate source of breather air to eliminate the possibility of pressurizing the engine case in the event that icing occurs at the breather tube end, a slot has been added to the lower portion of the breather tube.
  10. SB-03 Alon Wire Change

    A correction in the wiring on current models has been incorporated to completely eliminate the possibility of overheating the generator if the master switch is turned off in flight for a prolonged period of time.