What was found
LEFT WING MAIN FRAME WING TO FUSELAGE FITTING CRACKED AT BS 661, LONGERON 22L. R & R FITTING IAW SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING MAIN FRAME WING TO FUSELAGE FITTING CRACKED AT BS 661, LONGERON 22L. R & R FITTING IAW SRM.