What was found
DURING D-CHECK, FWD FUSELAGE LOWER RT SKIN HAD SEVERAL CREASES IN CORNER BETWEEN STA 218 TO 256 AND LONG 24R TO 26R. INSTALLED A REPAIR IAW SRM 53-04, FIG 38 VIEW P.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING D-CHECK, FWD FUSELAGE LOWER RT SKIN HAD SEVERAL CREASES IN CORNER BETWEEN STA 218 TO 256 AND LONG 24R TO 26R. INSTALLED A REPAIR IAW SRM 53-04, FIG 38 VIEW P.