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A correction in the wiring on current models has been incorporated to completely eliminate the possibility of overheating the generator if the master switch is turned off in flight for a prolonged period of time.
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In order to supply an alternate source of breather air to eliminate the possibility of pressurizing the engine case in the event that icing occurs at the breather tube end, a slot has been added to the lower portion of the breather tube.
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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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If the window catch does not properly engage its mating part, which is riveted to the door frame, it is suggested that the door frame catch be relocated to insure proper fit.
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Correction to Service Letter Number 126 regarding Metal Spar Splice Kits.
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List of approved batteries for installation on the Stinson 108 Series aircraft.
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A new design aluminum valve is now available that provides more positive detents for each position and does not require the repeated lubrication procedures.
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The wording on the Operating Limitations Placard used on Stinson Model 108 does not agree with the placard description in the Type Certificate Data Sheet A-767. A revised placard is now available.
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An unsafe condition may be created if the vent tube of the fuel cap assembly is not pointed directly into the oncoming air.
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When replacing Stinson fuel selector valves, if the valves are not indexed properly in relation to the panel mounted selector knob an unsafe condition could be created.