Rework to eliminate the possibility of the windshield coming out of its top retaining channel.
These inspection notes are issued as a recommended check list to assist owners, operators, and maintenance personnel in keeping their Piper airplanes in an airworthy condition.
Replacing aluminum aileron hinge reinforcing bracket with one made of steel, part number 10931-02.
How to fix difficulties with the fabric where it attaches to the fuselage under the windshield top and/or directly over the rear edge of the windshield top attachment channel.
Revises compliance time, purpose, and instructions for inspection and/or replacement of wing lift strut assembly. Also announces the availability of new sealed lift struts.
Compromised structural integrity of the fuselage due to excessive rust and corrosion between steel tubing and preformed sheet steel material.
Outlines the repair of Univair STC'd Stamped Ribs in accordance with the original STC and FAA Advisory Circular AC 43.13-1B.
Inspection of upper and lower shock strut end fitting attachment bolts for excessive tightness.
Recommendation that two hinge plates, Part Number 11876-00, be installed on the fuselage door hinge as an added safety feature to prevent the rivets from working loose.
Information concerning the use of safety belts which do not have TSO approval.
This letter is to advise all concerned that as of September 1st, 1962, the Piper Aircraft Corporation considers the following aircraft models obsolete inasmuch as they have been out of production for at least seven years.
Material list and instructions to reinforce the area where the fabric attaches to the fuselage under the windshield top and/or directly over the rear edge of the windshield top attachment channel.
Table showing the type of brake fluid used in airplanes manufactured by the Piper Aircraft Corporation.
Shock cord application chart for listed Piper models.
Rigging and leveling procedures for Piper PA-15 and PA-17.
General information regarding the installation of dual controls in a Piper PA-15 airplane.
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.
General specifications and performance data for the Piper Vagabond PA-15 and the Piper Vagabond Trainer PA-17.