As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND FUSELAGE DAMAGE AFT OF L1 BETWEEN F.S. 229-F.S. 256 AT STRS 16L-18L. DAMAGE IS .550 DEEP AT DEEPEST POINT. 11 1/2 IN LONG X 7 IN WIDE AT THE DEEPEST POINT AND 5 IN WIDE AT F.S. 237. REMOVED DAMAGED OUTER SKIN REPAIR AND AFT INTERNAL DOUBLER AND FINGER DOUBLER. REPAIRED SKIN DAMAGE FS 229-FS256 AT STRS 16L-18L PER B717 SRM 53-00-01 REPAIR 6. (LP #2173002)