What was found
UPON REMOVAL OF CYLINDERS (PN LW-1663) FOR ACCOMPLISHMENT OF STC SE792NW (INCREASE IN HORSEPOWER FROM 112 HP TO 125 UP), ALL FOUR CYLINDER WALLS SHOWED CONSIDERABLE PITTING. CAMSHAFT (PN 75706) LOBES AND LIFTERS (PN 71105) SHOWED FLAT SPOTTING, PITS, AND EXCESSIVE WEAR. SUSPECT CONDITIONS WERE CAUSED BY RUSTING WHICH OCCURRED WHEN AIRCRAFT WAS INACTIVE.