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As a result of several cases of engine power loss due to the carburetor alternate air door being sucked into the engine, make the spring loaded alternate air door inoperative by one of the following methods.
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To prevent accidental operation of the fuel shutoff valve during flight, a safety device must be installed on this control.
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Preventing elevator flutter in the event the elevator trim tab control wire fails by installing elevator trim tab stop and spring.
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Eliminating the possibilities of a rudder bellcrank seizure caused by the bakelite bushing that has expanded due to moisture within the bushing.
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List of approved batteries for installation on the Stinson 108 Series aircraft.
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Last Updated: 10/08/2021
in Technical Information GoodrichInstallation of and turning of Goodrich brake drum B13-4.
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Correction to Owner's Handbooks for the listed models.
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Remove the fairing at the wing root of each wing and inspect the wing root area for interference between the forward fuel line and the aileron cable and/or aileron pulley.
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To reduce the amount of oil passing through the breather tube and exhausting on the under-side of the aircraft, Continental Motors Corporation has a newly designed engine fitting which extends further into the engine case.
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Instructions on the installation of the 5.00 x 5 and 6.00 x 6 nose wheels on Ercoupes, especially those subject to unusually rough landings or operating from unusually rough fields.