What was found
DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 94-03-01, FOUND THE RIGHT FUSELAGE FRAME FITTING AT FS 984 HAD LEVEL II CORROSION. REPLACED RIGHT TEE FITTING IAW DC-9 SRM 51-30-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 94-03-01, FOUND THE RIGHT FUSELAGE FRAME FITTING AT FS 984 HAD LEVEL II CORROSION. REPLACED RIGHT TEE FITTING IAW DC-9 SRM 51-30-5.