What was found
WHILE IN C-CHECK, MAINTENANCE FOUND FUSELAGE SKIN GOUGED 1.5 WIDE AND .065 DEEP AT BS 1097, RBL 70, WL 200. INSTALLED FABRICATED PARTS IAW SRM 51-20-1, 53-30-3, M/M 51-20-151.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
WHILE IN C-CHECK, MAINTENANCE FOUND FUSELAGE SKIN GOUGED 1.5 WIDE AND .065 DEEP AT BS 1097, RBL 70, WL 200. INSTALLED FABRICATED PARTS IAW SRM 51-20-1, 53-30-3, M/M 51-20-151.