Piper PA-18

Actual labor breakdown, in hours, of factory time required to cover and finish 100 each of the Piper PA-18, PA-18A and PA-22 models.

Rigging procedure for Piper PA-18 and PA-19.

Approximate list of materials required to cover and finish the various component assemblies of the listed piper planes.

Approximate material required to recover Piper J-3, PA-11, PA-15, PA-17 and PA-18 aircraft 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.

Specifications and performance data for Piper PA-18 with Continental 90hp and Lycoming 108hp engines.

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

Pertains to the inspection of the Single Belt Driven Ring Gear Support Assembly as installed on the affected aircraft above.

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