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"Identifying a Cub's Gross Weight" by Joel Gehring excerpted from Cub Clues #135 July/August 2006.
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The compliance time for inspection of lift strut assemblies is changed from every 5 years to every 12 months.
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List of STC'd parts from F. Atlee Dodge Aircraft Services, LLC.
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How to prevent sudden failure of the fabric at the top of the windshield where the fabric attaches to the channel.
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Installing new inspection holes, modifying the wing tip fairings, and inspecting the wing spars for intergranular corrosion.
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Requires installing inspection openings in the outer wing panels, inspecting the wing outer panel structural components for corrosion, and repairing any corroded component.
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Determining the maximum and minimum lengths the tail brace wire should protrude through brass nipple U41051-000.
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Information and instructions for maintaining and rebuilding the Ercoupe nose landing gear assembly.
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Procedure for inspection of the wing center section to establish the condition of the center section structure.
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An improperly maintained three-position fuel selector valve could become difficult to rotate; this could result in damage to the selector lever mechanism and/or inability to switch tanks.