As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(RIGHT WING) TRANSVERSE WEB IS CRACKED AT O/B END UPPER LEG JUST I/B OF PROGRAM ROLLER SUPPORT ARM ATTACH POINT / REMOVED AND REPLACED TRANSVERSE WEB FITTING OF O/B END AND I/B OF PROGRAM ROLLER ARM SUPPORT IAW SOPM 20-50-01 84036 22JUN17