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