What was found
RT OVERWING TO FUSELAGE PANEL ATTACH STRUCTURE FS 470.00 IS CRACKED. R & R SUPPORT ANGLE AND RESTORED FINISH IAW SRM 51-42-06 AND SRM 51-25-16.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RT OVERWING TO FUSELAGE PANEL ATTACH STRUCTURE FS 470.00 IS CRACKED. R & R SUPPORT ANGLE AND RESTORED FINISH IAW SRM 51-42-06 AND SRM 51-25-16.