What was found
RIGHT WING TRANSVERSE WEB ATTACH ANGLE CRACKED AT PROGRAM ROLLER SUPPORT ARM ATTACH POINT. R & R ANGLE IAW SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT WING TRANSVERSE WEB ATTACH ANGLE CRACKED AT PROGRAM ROLLER SUPPORT ARM ATTACH POINT. R & R ANGLE IAW SRM.