What was found
SUPPLEMENTAL INFORMATION: LT WING L/E; AFT STIFFENER CRACKED AT WS 228 / REPLACED L/H WING L/E AFT STIFFNERAT WS 228 PER SRM 51-40-02-0G-0; AND BOEING DWG # 116A4008 ID: 0001 REV.A. 92385U 02/20/2018
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
SUPPLEMENTAL INFORMATION: LT WING L/E; AFT STIFFENER CRACKED AT WS 228 / REPLACED L/H WING L/E AFT STIFFNERAT WS 228 PER SRM 51-40-02-0G-0; AND BOEING DWG # 116A4008 ID: 0001 REV.A. 92385U 02/20/2018