What was found
INSPECTION FOUND A .25 INCH CRACK JUST FORWARD OF RT FAN COWL HINGE AREA IN VERTICAL STABILIZER SKIN PANEL. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-33-01, 55-00-01 AND 51-31-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .25 INCH CRACK JUST FORWARD OF RT FAN COWL HINGE AREA IN VERTICAL STABILIZER SKIN PANEL. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-33-01, 55-00-01 AND 51-31-01.