What was found
INSPECTION FOUND A 1 INCH CRACK IN LT FUSELAGE SUPPORT ANGLE AT STA 540, STRINGER 22. A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW SRM 51-70-11.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN LT FUSELAGE SUPPORT ANGLE AT STA 540, STRINGER 22. A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW SRM 51-70-11.