What was found
INSPECTION FOUND A .5 INCH CRACK IN LT WING SECOND UPPER STRINGER FROM AFT SPAR AT WS 686.50. AN ANGLE REPAIR WAS WAS INSTALLED 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 IN LT WING SECOND UPPER STRINGER FROM AFT SPAR AT WS 686.50. AN ANGLE REPAIR WAS WAS INSTALLED IAW EA 5762-01050.