What was found
AT C-CHECK, FUSELAGE LEFT WING T/E AREA, UPPER FIXED PANEL TOP OF I/B FLAP O/B JACKSCREW HAS SUPPORT ANGLE CRACKED ALONG RIVET.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, FUSELAGE LEFT WING T/E AREA, UPPER FIXED PANEL TOP OF I/B FLAP O/B JACKSCREW HAS SUPPORT ANGLE CRACKED ALONG RIVET.