What was found
LT WING TRANSVERSE WEB TO MAIN FLAP PROGRAM ROLLER SUPPORT ARM ATTACH ANGLE CRACKED. R & R THE ATTACH ANGLE IAW SRM AND DWG.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT WING TRANSVERSE WEB TO MAIN FLAP PROGRAM ROLLER SUPPORT ARM ATTACH ANGLE CRACKED. R & R THE ATTACH ANGLE IAW SRM AND DWG.