What was found
CRACK ON ANGLE OF WING TO BODY FITTING, LONGERON 22L, BS 661. THE ANGLE WAS REMOVED, FABRICATED, TREATED, PAINTED, AND INSTALLED IAW ER/A 560866-14, AND ETI-17-17-134, REV 3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON ANGLE OF WING TO BODY FITTING, LONGERON 22L, BS 661. THE ANGLE WAS REMOVED, FABRICATED, TREATED, PAINTED, AND INSTALLED IAW ER/A 560866-14, AND ETI-17-17-134, REV 3.