What was found
LEFT WING TRANSVERSE WEB CRACKED AT MAIN FLAP PROGRAM ROLLER SUPPORT ARM ATTACH POINT, INBD FASTENER, UPPER FLANGE. R & R WEB IAW SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING TRANSVERSE WEB CRACKED AT MAIN FLAP PROGRAM ROLLER SUPPORT ARM ATTACH POINT, INBD FASTENER, UPPER FLANGE. R & R WEB IAW SRM.