What was found
DURING HEAVY CHECK, FOUND UPPER FUSELAGE SKIN CRACK AT BS 1155, 10 INCHES LEFT OF BL 0. CRACK APPROXIMATELY 2 INCHES LONG. VERIFIED PER HFEC. REPAIRED PER SRM 53-30-3. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING HEAVY CHECK, FOUND UPPER FUSELAGE SKIN CRACK AT BS 1155, 10 INCHES LEFT OF BL 0. CRACK APPROXIMATELY 2 INCHES LONG. VERIFIED PER HFEC. REPAIRED PER SRM 53-30-3. (M)