What was found
INSPECTION FOUND A .5 INCH CRACK AT FASTENER HOLE IN LT WING FIRST UPPER STRINGER FROM REAR SPAR, ABOVE RIB AT WS 656.50. THE FASTENERS AND CLAMPS WERE REMOVED. THE CRACK WAS STOP DRILLED AND THE AREA WAS REPAIRED IAW EA 5762-01050.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK AT FASTENER HOLE IN LT WING FIRST UPPER STRINGER FROM REAR SPAR, ABOVE RIB AT WS 656.50. THE FASTENERS AND CLAMPS WERE REMOVED. THE CRACK WAS STOP DRILLED AND THE AREA WAS REPAIRED IAW EA 5762-01050.