What was found
MAIN FRAME WING TO FUSELAGE FITTING CRACKED AT 661, LONG 22R. REMOVED AND REPLACED FITTING IAW SRM & DWG.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
MAIN FRAME WING TO FUSELAGE FITTING CRACKED AT 661, LONG 22R. REMOVED AND REPLACED FITTING IAW SRM & DWG.