What was found
INSPECTION FOUND A .25 INCH CRACK IN SECOND FROM AFT VERTICAL WEB AT RT WING FRONT SPAR CHORD INBOARD AREA JUST FORWARD OF BOTTLE PIN. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-10-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .25 INCH CRACK IN SECOND FROM AFT VERTICAL WEB AT RT WING FRONT SPAR CHORD INBOARD AREA JUST FORWARD OF BOTTLE PIN. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-10-2.