What was found
DURING INSPECTION, THE PYLON LEADING EDGE WAS FOUND CHAFED INTO THE FUSELAGE SKIN. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM'S 51-10-3, 51-30-2, 53-04, FIG. 3A, SHEET 1, PG 6A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, THE PYLON LEADING EDGE WAS FOUND CHAFED INTO THE FUSELAGE SKIN. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM'S 51-10-3, 51-30-2, 53-04, FIG. 3A, SHEET 1, PG 6A.