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To prevent excessive wear of the primer line, resulting in fuel leakage and possible cabin fire, it is recommended that primer lines be clamped and/or re-routed per the sketch included with this letter.
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Using a sealing compound to prevent water from entering the cabin through the sliding window channels.
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Last Updated: 10/11/2021
in Technical Information Stinson
FAA approved Appendix A to CAA approved Operating Limitations for Stinson 108 Landplane, Stinson 108-1 Landplane and Stinson 108 and 108-1 Seaplane
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Remove the forward part of the tunnel fairing on the cockpit floor and inspect the control cable horns on the rudder bar for signs of bending.
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Installation of insulators inside the battery box cover over the battery terminals to positively prevent a metallic contact between the wing nuts or terminals and cover.
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It has been found necessary to provide a positive lock on the zipper at the bottom of the baggage compartment to eliminate the possibility of it opening while in flight, and having articles fall into the controls.
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The following installations have been FAA approved in the field. The party securing the approval is also listed.
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Reports of the vacuum pump splined coupling on Airborne Mechanisms Vacuum Pumps Models 113A5 and 113A8 may fail prematurely as a result of over-curing.
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Subject: This comprehensive inspection report provides recommendations for an inspection program per requirements of FAR Part 43 and Advisory Circular 91-60 (The Continued Airworthiness of Older Airplanes). Applicability: J-2 Series Cub...
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Revising the present front and rear wing lift struts.