What was found
WHILE REMOVING RT O/B FLAP HINGE ARM ASSEMBLIES AT WS 178.00 AND WS 264.00 FOUND HARDWARE TO BE CORRODED. (C-CHECK) RO 2/17/2021. RECEIVED SERVICEABLE HARDWARE. REFERENCE CAMP 21819157-1 FOR INSTALL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
WHILE REMOVING RT O/B FLAP HINGE ARM ASSEMBLIES AT WS 178.00 AND WS 264.00 FOUND HARDWARE TO BE CORRODED. (C-CHECK) RO 2/17/2021. RECEIVED SERVICEABLE HARDWARE. REFERENCE CAMP 21819157-1 FOR INSTALL.