What was found
DURING ROUTINE INSPECTION, THE LEFT PYLON UPPER SURFACE TO FUSELAGE ATTACH ANGLE WAS FOUND CRACKED APPROX .25 INCH IN LENGTH. REPAIRED ATTACH ANGLE IAW SRM 54-05 FIG 10. RETURNED A/C TO SERVICE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ROUTINE INSPECTION, THE LEFT PYLON UPPER SURFACE TO FUSELAGE ATTACH ANGLE WAS FOUND CRACKED APPROX .25 INCH IN LENGTH. REPAIRED ATTACH ANGLE IAW SRM 54-05 FIG 10. RETURNED A/C TO SERVICE.