What was found
AFT FUSELAGE COMPT: AFT PRESSURE BULKHEAD VERTICAL STIFFENER AT STA 2007, X=-10 UPPER END FOUND CRACKED. REPAIR CARRIED OUT AS PER EA 1-5310-117418, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFT FUSELAGE COMPT: AFT PRESSURE BULKHEAD VERTICAL STIFFENER AT STA 2007, X=-10 UPPER END FOUND CRACKED. REPAIR CARRIED OUT AS PER EA 1-5310-117418, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.