What was found
DURING C-CHECK, FOUND NR 2 PYLON TO FUSELAGE ATTACH ANGLE CRACKED BENEATH THE PYLON LEADING EDGE. REPLACED ANGLE IAW DC9 SRM 54-04.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK, FOUND NR 2 PYLON TO FUSELAGE ATTACH ANGLE CRACKED BENEATH THE PYLON LEADING EDGE. REPLACED ANGLE IAW DC9 SRM 54-04.