What was found
INSPECTION FOUND A 1 INCH CRACK IN UPPER AREA OF RT WING STRINGER, SECOND FROM AFT AT STA 686.5. THE CRACK WAS STOP DRILLED, A REPAIR WAS FABRICATED AND INSTALLED IAW EA 5762-01050 AND SRM 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN UPPER AREA OF RT WING STRINGER, SECOND FROM AFT AT STA 686.5. THE CRACK WAS STOP DRILLED, A REPAIR WAS FABRICATED AND INSTALLED IAW EA 5762-01050 AND SRM 51-30-2.