What was found
INSPECTION FOUND A .25 INCH CRACK IN LT WING STRINGER ON TOP OF RIB (SECOND UPPER STRINGER FROM AFT SPAR) WS 686.5. THE CRACK WAS STOP DRILLED AND A REPAIR 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 .25 INCH CRACK IN LT WING STRINGER ON TOP OF RIB (SECOND UPPER STRINGER FROM AFT SPAR) WS 686.5. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW EA 5762-01050.