As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FWD PIT; RH Z-ANGLE HAS CORROSION AT STA 500E+6.5 / FWD PIT RH Z ANGLE HAS CORROSION AT STA 500E + 6.5 - 500A BLENDED CORROSION AND FOUND ORIGINAL THICKNESS TO BE .040' REMAINING THICKNESS .032' REMOVED .008' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 REMOVED AND REPLACED WITH NEW 'Z' ANGLE IAW SRM 53-00-53-2R-5 REPAIR 5.