What was found
WHILE INVESTIGATING POSSIBLE SURFACE CORROSION ON THE LEFT WING TO FORWARD SPAR HINGE CAP DURING THE 12-MONTH SPAR CAP INSPECTION PER CHAPTER 5 OF THE MM, AN APPROXIMATE 2.6 INCH CRACK WAS FOUND AT APPROXIMATELY WS 153.735.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
WHILE INVESTIGATING POSSIBLE SURFACE CORROSION ON THE LEFT WING TO FORWARD SPAR HINGE CAP DURING THE 12-MONTH SPAR CAP INSPECTION PER CHAPTER 5 OF THE MM, AN APPROXIMATE 2.6 INCH CRACK WAS FOUND AT APPROXIMATELY WS 153.735.