What was found
DURING INSPECTION, FOUND RADIAL STIFFENER CRACKED AT 9 O'CLOCK POSITION ON AFT PRESSSURE BULKHEAD. INSTALLED DOUBLE ANGLE REPAIR IAW SRM 53-01 FIG 2 SHT 4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, FOUND RADIAL STIFFENER CRACKED AT 9 O'CLOCK POSITION ON AFT PRESSSURE BULKHEAD. INSTALLED DOUBLE ANGLE REPAIR IAW SRM 53-01 FIG 2 SHT 4.