What was found
DURING SCHEDULED MAINTENANCE, FOUND FUSELAGE SKIN CRACKED AT BS 941 S24L. HFEC CONFIRMED CRACK LENGTH 2.9375 INCH (CRACK PARALLEL WITH STRINGER). REPAIRED PER SRM 53-30-3. ACFT RETURNED TO SERVICE. (W)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED MAINTENANCE, FOUND FUSELAGE SKIN CRACKED AT BS 941 S24L. HFEC CONFIRMED CRACK LENGTH 2.9375 INCH (CRACK PARALLEL WITH STRINGER). REPAIRED PER SRM 53-30-3. ACFT RETURNED TO SERVICE. (W)