What was found
AFT WING TO BODY FAIRINGS INTERNAL SUPPORT WEB HAS CORRODED SPLICE ANGLE. R & R ANGLE IAW SRM 51-42-06, WO 80289 & WC 1115.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFT WING TO BODY FAIRINGS INTERNAL SUPPORT WEB HAS CORRODED SPLICE ANGLE. R & R ANGLE IAW SRM 51-42-06, WO 80289 & WC 1115.