What was found
CRACKED ANGLE, BS 500C, S26L. REPLACED THE ANGLE IAW SRM 51-40-02; SRM 51-10-02, ITEM 9, AND DWG 143A7505, SHEET 118, REV-. MEASUREMENT OF CRACK: L: 0.350.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED ANGLE, BS 500C, S26L. REPLACED THE ANGLE IAW SRM 51-40-02; SRM 51-10-02, ITEM 9, AND DWG 143A7505, SHEET 118, REV-. MEASUREMENT OF CRACK: L: 0.350.