What was found
AFT WING TO BODY SUPPORT ATTACHMENT ANGLE IS CORRODED AT F/S. 953 FROM B/L 24L-24R. CORRECTIVE ACTION: REMOVED AND REPLACED ANGLE (P/N: SH670-39189-1) IAW CRJ 700 SRM 51-40-00.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFT WING TO BODY SUPPORT ATTACHMENT ANGLE IS CORRODED AT F/S. 953 FROM B/L 24L-24R. CORRECTIVE ACTION: REMOVED AND REPLACED ANGLE (P/N: SH670-39189-1) IAW CRJ 700 SRM 51-40-00.