What was found
CRACKED SUPPORT ANGLE, BS 867, LBL 10. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, DWG 149A8102, SHEET 19, REV A. MEASUREMENT OF CRACK IS L= 0.602.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED SUPPORT ANGLE, BS 867, LBL 10. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, DWG 149A8102, SHEET 19, REV A. MEASUREMENT OF CRACK IS L= 0.602.