What was found
DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND FUSELAGE FRAME AT FS 1152 CRACKED AT LONGERON 14R. REPLACED FRAME IAW DC-9 SRM 51-30-2 AND 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, FOUND FUSELAGE FRAME AT FS 1152 CRACKED AT LONGERON 14R. REPLACED FRAME IAW DC-9 SRM 51-30-2 AND 51-30-5.