What was found
WHILE COMPLYING WITH C INSPECTION, FOUND FUSELAGE FRAME 544 RIGHT CRACKED AT TRANSVERSE FLOORBEAM. REPLACED FUSELAGE FRAME IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
WHILE COMPLYING WITH C INSPECTION, FOUND FUSELAGE FRAME 544 RIGHT CRACKED AT TRANSVERSE FLOORBEAM. REPLACED FUSELAGE FRAME IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.