What was found
AT C-CHECK, LEADING EDGE COVE PANEL SUPPORT ANGLE IS CRACKED JUST BELOW NR 3 SPOILER O/B HINGE. REMOVED AND INSTALLED 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, LEADING EDGE COVE PANEL SUPPORT ANGLE IS CRACKED JUST BELOW NR 3 SPOILER O/B HINGE. REMOVED AND INSTALLED ANGLE PER SRM 57-50-1.