What was found
CRACK ON ANGLE OF WING BOX INTERNAL STRUCTURE AT BS 962, X=42 AND Z=-8. REMOVED AND INSTALLED NEW ANGLE IAW DWG 9923417, REV B AND SRM 51-30-05.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON ANGLE OF WING BOX INTERNAL STRUCTURE AT BS 962, X=42 AND Z=-8. REMOVED AND INSTALLED NEW ANGLE IAW DWG 9923417, REV B AND SRM 51-30-05.