As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(DOT 67-20) LEFT WING T/E AT DEFLECTION CONTROL RIB; SUPPORT BRACKET FOR FIXED T/E IS CRACKED. / [01] REMOVED AND REPLACED CRACKED SUPPORT BRACKET; P/N 115A6260-1; L/H WING T/E DEFLECTION CONTROL RIB IAW SRM 51-40-02-0G-0 AND BOEING DWG 115A6200 ID 0024 REV A<BR>ATAG A113710;[02] VERIFIED STEP 1 IS COMPLETE;[03] VERIFIED STEPS 1 AND 2; AUDIT C/W