As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C2 U/D BS 380 STR 6L AND 7L FRAME INNER CHORD CRACKED. REPAIRED FRAME INNER CHORDS & WEB AS PER SRM 53-10-04 FIG 98 (NDT C/OUT PER NDT MANUAL PT.6, 51-00-00 FIG04 CONFIRMED; RESULT: NO CRACK REVEALED AT TRIM OFF AREA NO CRACK BEYOND STOP HOLE ).