What was found
LEFT AFT O/B FLAP, I/B HINGE INNER AND OUTER SURFACE OF I/B ACTUATOR HOLE FOUND WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOL II & REPAIRED AS PER FEDEX EA 1-5750-76011, BRACKET CORROSION REMOVAL & REPAIR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT AFT O/B FLAP, I/B HINGE INNER AND OUTER SURFACE OF I/B ACTUATOR HOLE FOUND WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOL II & REPAIRED AS PER FEDEX EA 1-5750-76011, BRACKET CORROSION REMOVAL & REPAIR.