What was found
NR 1 PYLON UPPER AFT END HAS FIBERGLASS PANEL DAMAGE. REPAIRED PER SRM 51-40-09, 52-24-11.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 1 PYLON UPPER AFT END HAS FIBERGLASS PANEL DAMAGE. REPAIRED PER SRM 51-40-09, 52-24-11.