As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AIRCRAFT IN BASE MAINTENANCE: PANEL SUPPORT ANGLE (115A2156-8), INBOARD OF FLAP MID SPAN DEFLECTION RIB, HAS 3 INCH CRACK IN O/B UPPER RADIUS. REMOVED AND REPLACED SECONDARY SUPPORT ANGLE FROM T/E MIDSPAN PANEL IAW SRM 51-10-02-0G AND SRM 51-40-02-0G.