What was found
DURING SCHEDULED C4 CHECK, FOUND A 2.5 INCH LONG CRACK AT FUSELAGE SKIN, BS 885, STR 24R, (CONFIRMED WITH EDDY CURRENT INSPECTION). REPAIRED PER SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED C4 CHECK, FOUND A 2.5 INCH LONG CRACK AT FUSELAGE SKIN, BS 885, STR 24R, (CONFIRMED WITH EDDY CURRENT INSPECTION). REPAIRED PER SRM.