What was found
AT C CHECK, LEFT WING FIXED LEADING EDGE CAVITY UPPER OUTBD SUPPORT ANGLE AT SLAT STA 0 IS CRACKED AT AFT ATTACH FASTENERS. REMOVED ANGLE, FABRICATED NEW SUPPORT ANGLE, PER SRM 51-40-3, 16 BY 1.625, N/R 1390.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C CHECK, LEFT WING FIXED LEADING EDGE CAVITY UPPER OUTBD SUPPORT ANGLE AT SLAT STA 0 IS CRACKED AT AFT ATTACH FASTENERS. REMOVED ANGLE, FABRICATED NEW SUPPORT ANGLE, PER SRM 51-40-3, 16 BY 1.625, N/R 1390.