What was found
DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 90-18-03; SB 57-98 REV 8, FOUND T-CAP CORRODED INSIDE BARREL NUT HOLES AT STRINGERS 12, 18, 19, 20, 21, 22 AND 23 ON THE RIGHT WING. REPAIRED IAW DC-9 SRM 51-10-3 AND DC-9 SB 57-98.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 90-18-03; SB 57-98 REV 8, FOUND T-CAP CORRODED INSIDE BARREL NUT HOLES AT STRINGERS 12, 18, 19, 20, 21, 22 AND 23 ON THE RIGHT WING. REPAIRED IAW DC-9 SRM 51-10-3 AND DC-9 SB 57-98.