What was found
DURING L/O, NR 2 ENG WAS REMOVED FOR SCHEDULED MAINTENANCE, FOUND A 1.5 INCH CRACK IN THE INBOARD WEB OF PYLON STRUCTURE AT THE FWD INSPECTION HOLE. REPAIRED PER SRM 54-51-01 FIG 203.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING L/O, NR 2 ENG WAS REMOVED FOR SCHEDULED MAINTENANCE, FOUND A 1.5 INCH CRACK IN THE INBOARD WEB OF PYLON STRUCTURE AT THE FWD INSPECTION HOLE. REPAIRED PER SRM 54-51-01 FIG 203.