What was found
INSPECTION FOUND AFT PRESSURE BULKHEAD SIDE, TWO EACH CENTER CHANNEL STIFFENERS CORRODED ON BOTH SIDES AT STA 1016. A STIFFENER REPAIR WAS INSTALLED IAW DRAWING 65C28106-1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND AFT PRESSURE BULKHEAD SIDE, TWO EACH CENTER CHANNEL STIFFENERS CORRODED ON BOTH SIDES AT STA 1016. A STIFFENER REPAIR WAS INSTALLED IAW DRAWING 65C28106-1.