What was found
AT C-CHECK, LEFT WING COVE PANEL SUPPORT ANGLES ARE CRACKED AT STA 573. REMOVED SUPPORT ANGLES AND REPLACED 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 COVE PANEL SUPPORT ANGLES ARE CRACKED AT STA 573. REMOVED SUPPORT ANGLES AND REPLACED PER SRM 51-30-2.