What was found
AFT ROW SECOND FROM THE TOP OF FUSELAGE, SKIN CRACKED AT BS 540, LOWER BULKHEAD CHORD LT SIDE. REPAIRED SKIN IAW SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFT ROW SECOND FROM THE TOP OF FUSELAGE, SKIN CRACKED AT BS 540, LOWER BULKHEAD CHORD LT SIDE. REPAIRED SKIN IAW SRM.