What was found
DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND ATTACH ANGLE CORROSION AND FASTENER HOLE ELONGATED FS 477, LBL 24-60, WL 280. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583 CH 51-60 & 51-70.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND ATTACH ANGLE CORROSION AND FASTENER HOLE ELONGATED FS 477, LBL 24-60, WL 280. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583 CH 51-60 & 51-70.