As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE SUPPORT ANGLE LOCATED ABOVE STRINGER 26R AT BS 558 HAS SURFACE CORROSION. REMOVED CORRODED SUPPORT ANGLE AND FABRICATED SUPPORT ANGLE FROM 7075 O -.040 INCH (9 INCHES X 4.5 INCHES) HEAT TREATED TO T6. INSTALLED SUPPORT ANGLE. IAW SRM 53-10-2, 51-30-2. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.