What was found
INSPECTION FOUND A .25 INCH CRACK IN TAIL COMPARTMENT STRINGER 21R BETWEEN STA 1040 AND 1064. A REPAIR ANGLE AND SHIM WERE INSTALLED IAW SRM 53-00-00.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .25 INCH CRACK IN TAIL COMPARTMENT STRINGER 21R BETWEEN STA 1040 AND 1064. A REPAIR ANGLE AND SHIM WERE INSTALLED IAW SRM 53-00-00.