What was found
DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND LEVEL II CORROSION ON STIFFENER ON AFT FACE OF CANTED BULKHEAD 1089 AT LONGERON 6 LEFT. REPLACED STIFFENER IAW DC-9 SRM CHAPTER 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND LEVEL II CORROSION ON STIFFENER ON AFT FACE OF CANTED BULKHEAD 1089 AT LONGERON 6 LEFT. REPLACED STIFFENER IAW DC-9 SRM CHAPTER 51-30-2.