What was found
DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 90-18-03; SB 57-98 REV 8, FOUND STRINGER 23L CORRODED AND GOUGED INSIDE TENSION BOLT HOLE AT T-CAP. REPAIRED IAW DC-9 SRM 51-10 AND 57-03.
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 STRINGER 23L CORRODED AND GOUGED INSIDE TENSION BOLT HOLE AT T-CAP. REPAIRED IAW DC-9 SRM 51-10 AND 57-03.