What was found
AT C-CHECK, RIGHT WING T/E INBOARD LOWER STA 5.00 AT I/B FLAP I/B HINGE SUPPORT FWD AREA FOUND CRACK ON ANGLE REINFORCEMENT. REMOVED CRACKED ANGLE, FABRICATED NEW ANGLE 12 X 2.5 PER SRM 51-1-21.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, RIGHT WING T/E INBOARD LOWER STA 5.00 AT I/B FLAP I/B HINGE SUPPORT FWD AREA FOUND CRACK ON ANGLE REINFORCEMENT. REMOVED CRACKED ANGLE, FABRICATED NEW ANGLE 12 X 2.5 PER SRM 51-1-21.