What was found
CRACK ON MAIN FRAME WING TO FUSELAGE FITTING BS 661, LONGERON 22L. REPAIRED IAW ETI-17-17-155, REV ORIGINAL, AND ER/A 560940-14, REV ORIGINAL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON MAIN FRAME WING TO FUSELAGE FITTING BS 661, LONGERON 22L. REPAIRED IAW ETI-17-17-155, REV ORIGINAL, AND ER/A 560940-14, REV ORIGINAL.