What was found
INSPECTION NOTED NR 2 ENGINE UPPER PYLON RIB 06 FORWARD INBOARD STRINGER WAS CRACKED AT CORNER HOLE. MAINTENANCE PERFORMED REPAIR BY FABRICATING SUPPORT ANGLE AND INSTALLING PER SRM 51-42-11 AND 54-52-12.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION NOTED NR 2 ENGINE UPPER PYLON RIB 06 FORWARD INBOARD STRINGER WAS CRACKED AT CORNER HOLE. MAINTENANCE PERFORMED REPAIR BY FABRICATING SUPPORT ANGLE AND INSTALLING PER SRM 51-42-11 AND 54-52-12.