Piper PA-22

Approximate amount of materials required to recover PA-20 and PA-22 models using raw fabric and cellulose acetate butyrate dope.

The following installations have been FAA approved in the field. The party securing the approval is also listed.

Increase in gross weight 1800 to 1950 pounds (Lycoming 0-290-d engine) (125 hp only).

Specifications and performance data for Piper PA-22 "125" and "135" airplanes.

An approval has been obtained for operating the PA-22 Tri-Pacer with the rear door removed (parachute jumping, photography, etc.).

Installation of this boot will reduce the possibility of moisture accumulating between the oleo assembly and the oleo housing.

Addresses a potential for impulse coupling failure, which can result in total loss of engine power.

Information on replacing an existing diaphragm suspected to be defective in master brake cylinders installed in listed Piper aircraft models.