What was found
RIGHT OVERWING TO FUSELAGE PANEL ATTACH STRUCTURE FS 470.00 IS CRACKED. R & R ATTACH STRUCTURE AT IAW SRM-51-42-21.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT OVERWING TO FUSELAGE PANEL ATTACH STRUCTURE FS 470.00 IS CRACKED. R & R ATTACH STRUCTURE AT IAW SRM-51-42-21.