What was found
DURING D-CHECK ACCEPTANCE INSPECTION, FOUND FUSELAGE FRAME FITTING CRACKED AT FS 1121. REPLACED FITTING IAW DC-9 SRM CHAPTERS 51-30-2, 51-30-5 AND 51-30-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING D-CHECK ACCEPTANCE INSPECTION, FOUND FUSELAGE FRAME FITTING CRACKED AT FS 1121. REPLACED FITTING IAW DC-9 SRM CHAPTERS 51-30-2, 51-30-5 AND 51-30-3.