What was found
RIGHT OVERWING TO FUSELAGE CLOSEOUT PANEL ATTACHMENT STRUCTURE, FS 461.00 IS CRACKED. REPLACED PANEL SUPPORT ATTACHMENT IAW SRM 51-24-21, 51-40-11, 51-42-06 & 53-82-83.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT OVERWING TO FUSELAGE CLOSEOUT PANEL ATTACHMENT STRUCTURE, FS 461.00 IS CRACKED. REPLACED PANEL SUPPORT ATTACHMENT IAW SRM 51-24-21, 51-40-11, 51-42-06 & 53-82-83.