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Reports that a certain batch of Resistoflex was used in fuel systems which caused trouble. This batch, manufactured during third quarter of 1945, can be identified by marking LP-3-45.
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Proper adjusting of starter control clearances will reduce the possibility of the starter being accidentally engaged while the motor is running.
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Refinishing procedure for airplanes with enamel type finish and airplanes finished with acrylic lacquer.
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Procedure to reduce the possibility of breakage through incorrect removal of the dome light lens.
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Outlines the repair of Univair STC'd Stamped Ribs in accordance with the original STC and FAA Advisory Circular AC 43.13-1B.
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Approximate list of materials required to cover and finish the various component assemblies of the listed piper planes.
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Compromised structural integrity of the fuselage due to excessive rust and corrosion between steel tubing and preformed sheet steel material.
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Information concerning the use of safety belts which do not have TSO approval.
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The round upper and lower tail brace tie rod assemblies, part numbers 10555-02 and 10556-02, respectively, have been approved to replace the upper and lower streamline tail brace tie rod assemblies in the listed aircraft.
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Reworking of bottom cowl for replacing air scoop EQ5259 with EQ5370 (Continental part numbers).