What was found
DURING POST FLIGHT WALKAROUND, CREW REPORTED FINDING A FUSELAGE SKIN CRACK ON THE LT DV WINDOW UPPER FRAME AREA. MX PERFORMED REPAIR ON UPPER BEAM ATTACHED TO DV WINDOW AND WINDSHIELD POST ON LT SIDE IAW SRM 51-40-02. SHV MX ALSO PERFORMED REPAIR ON LT DV WINDOW LOWER STRUT AT FASTENER HOLES IAW SRM 51-40-02 AND SRM 51-20-03. LT LOWER STRUT PN 120-35690-509 AND BEAM PN 123-07751-005. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.