What was found
CRACK ON ANGLE AFT FACE BS 500H, STRINGER 26R. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7505, SHEET 139, REV-. MEASUREMENT OF CRACK: L: 0.480 INCH.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON ANGLE AFT FACE BS 500H, STRINGER 26R. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7505, SHEET 139, REV-. MEASUREMENT OF CRACK: L: 0.480 INCH.