What was found
C2 OKC - FLAP LEADING EDGE PANEL 684LB IS CHAFED ON LEADING EDGE. REPAIRED IAW SRM 57-52-01, 51-21-11.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
C2 OKC - FLAP LEADING EDGE PANEL 684LB IS CHAFED ON LEADING EDGE. REPAIRED IAW SRM 57-52-01, 51-21-11.