What was found
INSPECTION FOUND A 2 INCH CRACK IN FRAME AT FS 880 BETWEEN STRINGER 18R AND 17R. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR ANGLE WAS INSTALLED IAW SRM 51-30-2 AND 51-40-3, FIGURE 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 INCH CRACK IN FRAME AT FS 880 BETWEEN STRINGER 18R AND 17R. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR ANGLE WAS INSTALLED IAW SRM 51-30-2 AND 51-40-3, FIGURE 1.