What was found
INSPECTION FOUND A .75 INCH CRACK IN VERTICAL STABILIZER, 24 INCHES FROM LEADING EDGE. THE CRACK WAS ROUTED OUT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-30-6. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .75 INCH CRACK IN VERTICAL STABILIZER, 24 INCHES FROM LEADING EDGE. THE CRACK WAS ROUTED OUT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-30-6. (M)