What was found
DURING C-INSPECTION, FOUND THE PYLON UPPER FUSELAGE ATTACH ANGLE CRACKED AT FS 980. REPAIRED ATTACH ANGLE IAW DC9 SRM CHAPTERS 54-04 FIGURE 10 AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-INSPECTION, FOUND THE PYLON UPPER FUSELAGE ATTACH ANGLE CRACKED AT FS 980. REPAIRED ATTACH ANGLE IAW DC9 SRM CHAPTERS 54-04 FIGURE 10 AND 51-30-2.