What was found
CRACKED SUPPORT ANGLE ON OTBD AUXILIARY TRACK SLAT 8, RT WING. REPLACED THE SUPPORT ANGLE IAW CMM 57-43-03, REV 41. ASSEMBLY PROCEDURES STEP 2.C(9) PAGE 702.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED SUPPORT ANGLE ON OTBD AUXILIARY TRACK SLAT 8, RT WING. REPLACED THE SUPPORT ANGLE IAW CMM 57-43-03, REV 41. ASSEMBLY PROCEDURES STEP 2.C(9) PAGE 702.