What was found
AT C-CHECK, LEFT WING T/E COVE PANEL SUPPORT ANGLE IS CRACKED JUST I/B OF NR 3 SPOILER ACTUATOR STA 497. REMOVED AND INSTALLED SUPPORT ANGLE PER SRM 57-50-1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, LEFT WING T/E COVE PANEL SUPPORT ANGLE IS CRACKED JUST I/B OF NR 3 SPOILER ACTUATOR STA 497. REMOVED AND INSTALLED SUPPORT ANGLE PER SRM 57-50-1.