What was found
AT C-CHECK, LEFT WING T/E COVE PANEL SUPPORT ANGLE IS CRACKED JUST BELOW NR 4 SPOILER I/B HINGE. REMOVED AND REPLACED COVE PANEL SUPPORT ANGLE PER SRM 51-30-2.
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 BELOW NR 4 SPOILER I/B HINGE. REMOVED AND REPLACED COVE PANEL SUPPORT ANGLE PER SRM 51-30-2.