As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFT FUSELAGE AFTER SKIN FOUND CORROSION IN THE LONGERON 19L STA 1309 TO 1322. REMOVED CORROSION ON L19L STA 1309 TO STA 1322 AFT FUSE IAW DC9/MD80 SRM 53-01 FIG 1 SH 2 PG 8. FOUND OUT OF LIMITS IAW SRM 53-14-3 FIG 4 SH 2 PG 30-31 ITEM 21 AND SRM 51-10-1 FIG 15 PG 69. REMOVED L19L STA 1212 TO 1388 IAW SRM 51-30-05 PG 1. INSTALLED L19L FROM STA 1202 TO 1338 IAW SRM 51-30-05 PG 12.