What was found
DURING C-CHECK, FOUND A 1.50 INCH CRACK ON L/E OF WING SKIN PANEL UNDERSIDE WS 135 AND WS 140. INSTALLED REPAIR PLATE AND ANGLE. ACFT TT: 56,458. ACFT TC: 23,698.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK, FOUND A 1.50 INCH CRACK ON L/E OF WING SKIN PANEL UNDERSIDE WS 135 AND WS 140. INSTALLED REPAIR PLATE AND ANGLE. ACFT TT: 56,458. ACFT TC: 23,698.