What was found
INSPECTION FOUND A 2 CRACK IN FORMED ANGLE AT FUSELAGE SKIN, STA 1421, LONGERON 31L TO 32L, AT LT WING INBOARD TOP FILLET AREA. THE ANGLE WAS REMOVED. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-53-01, VOL II, 51-31-01, VOL II, AND 51-33-01, VOL 11.