What was found
DURING ROUTINE C-CHECK INSPECTION FOUND ANGLE CRACKED IN LEFT WING LEADING EDGE OF NR 3 KRUEGER FLAP. REMOVED ANGLE, FABRICATED AND INSTALLED REPAIR ANGLE, ALODINED AND PRIMED IAW SRM 51-40-3 FIG 1, 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ROUTINE C-CHECK INSPECTION FOUND ANGLE CRACKED IN LEFT WING LEADING EDGE OF NR 3 KRUEGER FLAP. REMOVED ANGLE, FABRICATED AND INSTALLED REPAIR ANGLE, ALODINED AND PRIMED IAW SRM 51-40-3 FIG 1, 51-30-2.