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To preclude the possibility of failure at the upper shock strut-drag tube area of the LPC 1012 series landing gear vees used in the STC-SA45RM taildragger modification, a second gusset has been added to the upper end of the streamline brace tube.
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Instructions and materials list for the installation of elevator trim tab stops and springs on early Ercoupes.
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Provisions for expelling water and gasoline from the forward belly regions of the aircraft for all normal parking attitudes.
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Specifications and performance data for Piper PA-22 "125" and "135" airplanes.
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Covers the tightening of the propeller hub bolts on the Continental hub used with the Continental C-75 and C-85 engines.
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Inspect the lift strut clevis bolts for evidence of abuse. If such evidence is noted, the bolts shall be replaced.
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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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Reference: 45.11 (b) Removal of data plate.
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How to prevent the control stick inadvertently pulling out of the socket.
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Removing the R003-201 propeller blades and visually inspecting the propeller blade retainer ferrule for cracks.