What was found
INSPECTION FOUND A 1 INCH CRACK IN STRINGER 16L AT BS 500C. A STRINGER SPLICE REPAIR WAS INSTALLED IAW SRM 53-00-03, FIGURE 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN STRINGER 16L AT BS 500C. A STRINGER SPLICE REPAIR WAS INSTALLED IAW SRM 53-00-03, FIGURE 201.