As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C-CHECK WHILE COMPLYING WITH AD 78-07-05/EO 12-531-29-B1044 IR, FUSELAGE FRAME FITTING INSPECTION FOUND RIGHT AFT MAIN FRAME CRACKED BEYOND FIG 4 LIMITS. REMOVED AND REPLACED FITTING IAW OPTION 2 OF EO 12-5311-29-B1044 REV IR. (M)