What was found
DURING D CHECK INSPECTION, FOUND RIGHT WING I/B MID FLAP I/B FITTING CARRIAGE CAVITY CORRODED AT ACCESS PLATE 8508. REMOVED CORROSION. MATERIAL LOSS .050. OUT OF LIMITS PER SRM 57-30-1. INSTALLED 2 X 7 INCH REINFORCED ANGLE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING D CHECK INSPECTION, FOUND RIGHT WING I/B MID FLAP I/B FITTING CARRIAGE CAVITY CORRODED AT ACCESS PLATE 8508. REMOVED CORROSION. MATERIAL LOSS .050. OUT OF LIMITS PER SRM 57-30-1. INSTALLED 2 X 7 INCH REINFORCED ANGLE.