What was found
AFTER REMOVAL, CORROSION WAS FOUND ON THE FRAME ANGLE, S28R, BS 500G. THE FRAME ANGLE WAS REPLACE IAW SRM 51-40-02-0G-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFTER REMOVAL, CORROSION WAS FOUND ON THE FRAME ANGLE, S28R, BS 500G. THE FRAME ANGLE WAS REPLACE IAW SRM 51-40-02-0G-0.