What was found
CRACKED SUPPORT ANGLE AT THE FIXED TRAILING EDGE PANEL, ORSS 261, LT WING. REPLACED THE SUPPORT ANGLE IAW RM 51-10-02, PARAGRAPH 9, SRM 51-40-02, DWG 115A2512, SHEET 16, REV-.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED SUPPORT ANGLE AT THE FIXED TRAILING EDGE PANEL, ORSS 261, LT WING. REPLACED THE SUPPORT ANGLE IAW RM 51-10-02, PARAGRAPH 9, SRM 51-40-02, DWG 115A2512, SHEET 16, REV-.