What was found
DURING INPSECTION, CORROSION WAS FOUND AT THE R2 THRESHOLD AROUND THE RIVET HEADS AT THE GRIT BAR FITTING. MAINTENANCE R & R THE THRESHOLD IAW SRM 51-40-02, 51-41-01, 51-41-02, 51-43-03, 51-43-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INPSECTION, CORROSION WAS FOUND AT THE R2 THRESHOLD AROUND THE RIVET HEADS AT THE GRIT BAR FITTING. MAINTENANCE R & R THE THRESHOLD IAW SRM 51-40-02, 51-41-01, 51-41-02, 51-43-03, 51-43-02.