What was found
DURING C-CHECK, THE LOWER PYLON TO FUSELAGE ATTACH ANGLE WAS FOUND CRACKED. THE ANGLE WAS REPAIRED IAW DC9 SRM 54-04, FIGURE 10.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK, THE LOWER PYLON TO FUSELAGE ATTACH ANGLE WAS FOUND CRACKED. THE ANGLE WAS REPAIRED IAW DC9 SRM 54-04, FIGURE 10.