What was found
DOT 21-A-22; RIGHT HORIZONTAL STAB RIB STA 129.50; RIB STIFFENER #3 CRACKED 1' ABOVE LOWER FLANGE ; / C.I.CED AREA I.A.W MM51-21-91-620-802; REMOVED RIB TO REPAIR CRICKET # 3 STIFFENER AT R /H HORZ STAB STA129.5 I.A.W ARM 51-40-02-0G-0<BR>REMOVED DAMAGED AREA FROM #3 STIFFENER I.A.W SRM55-10-09-2R-4.<BR>FABRICATED 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 182A1500 SHT11 REV :A; CIC AND SUMMARY OK AUDIT OK