What was found
FUSELAGE SKIN CRACK APPROXIMATELY 2.5 INCHES LONG AT BS 787 AND STR 18L. VERIFIED CRACK USING HIGH FREQUENCY EDDY CURRENT. REPAIRED PER SRM 53-30-3 FIG 1. AIRCRAFT RETURNED TO SERIVCE. TAT: 29,087.1 HRS. TAC: 34,722. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN CRACK APPROXIMATELY 2.5 INCHES LONG AT BS 787 AND STR 18L. VERIFIED CRACK USING HIGH FREQUENCY EDDY CURRENT. REPAIRED PER SRM 53-30-3 FIG 1. AIRCRAFT RETURNED TO SERIVCE. TAT: 29,087.1 HRS. TAC: 34,722. (X)