What was found
DOT 20-A-22; RIGHT HORIZONTAL STAB RIB STA 92.70; RIB STIFFENER #2 CRACKED 1' ABOVE LOWER FLANGE ; / C.I.CED RIBI.A.W MM51-21-91-620-802; REINED RIB AT R/H HORZ STAB STA92.70 TO REPAIR #2 RIB STIFFENER I.A.W SRM51-40-02-0G-0.<BR>REMOVED DAMGE AT #2 RIB STIFFENER I.A.W SRM 55-10-09-2R-4<BR>FABRICTED REPAIR PARTS I.A.W SRM55-10-09-2R-4.<BR>INSTALLED REPAIR PARTS I.A.W SRM55-10-09-2R-4.<BR>REINSTALLED RIB I.A.W SRM51-40-02-0G-0 AND BOEING DWG 002A0001 REV:C; CIC AND SUMMARY OK AUDIT OK