-
Requires installing inspection openings in the outer wing panels, inspecting the wing outer panel structural components for corrosion, and repairing any corroded component.
-
Over time, a chafing condition resulting from the control cable sliding against the stationary pulley groove can cause the control cable to wear completely through, possibly resulting in loss of aileron control during flight.
-
Last Updated: 10/08/2021
in Technical Information ErcoupeThis 101 page document contains the production history of Ercoupe 415-C thru 415-G airplanes, listed by serial number.
-
Rigging and leveling procedures for Piper PA-12.
-
Directions to prevent failure of the upper wing front spar strut fittings, P/N 2-1976, that could result
in an in-flight separation of the wing.
-
Due to recurring failures of the control cables, all cables should be carefully inspected at each section which passes either over a pulley or through a fairlead.
-
General specifications of the Piper PA-11 Cub Special.
-
Instructions to prevent possible leakage of carbon monoxide into the cabin heater system in airplanes utilizing Avcon Industries, Inc., kits with defective mufflers.
-
Procedure for inspection of the wing center section to establish the condition of the center section structure.
-
Excerpt of FAR Part 43 Maintenance, Preventive Maintenance, Rebuilding, and Alteration.