What was found
R/H HORIZONTAL STABILIZER FRONT SPAR L/E INTERNAL RIB # 1 HAS STIFFENER # 2 CRACKED @ LOWER RADIUS MKD DOT<[01] REMOVED CRACK AT R/H HORIZONTAL STAB FRONT SPAR L/E #1RIB STIFFENER#2 AS PER REF B/737-700 SRM 55-10-09-2R-4 REPAIR 4.;[02] VERIFIED STEP 1;[03] PERFORMED HFEC INSP ON CUT OUT AREA STIFFENER#2 IAW B737 NDT P6 51-00-00 PROC.23; CRACK REMAINS ON WEB.(MARKED)<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 03/23;[04] PERFORMED ROTO INSP ON 8EA EXISTING HOLES AT STIFFENER#2 LOWER CHORD IAW B737 NDT P6 51-00-00 PROC.16; NO CRACKS NOTED<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 03/23;[05] REMOVED CRACK ON WED AT R/H HORIZONTAL STAB FROM SPAR L/E #1 RIB STIFFENERS # 2 AS PER REF B/737-700 SRM 55-10-09-2R-4 REPAIR 4.;[06] VALIDATED STEP 5;[07] PERFORMED HFEC INSP ON CUT OUT AREA STIFFENER#2 IAW B737 NDT P6 51-00-00 PROC.23;NO CRACKS NOTED<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 03/23;[08] RII: VERIFIED STEP 1;[09] LOCATED AND DRILLED NEW PARTS OF REPAIR AT R/H HORIZONTAL STAB FROM SPAR L/E RIB # 1 STIFFENERS #2 AS PER REF B/737-700 SRM 55-10-09-2R-4 REPAIR 4.;[10] VALIDATED STEP 9;[11] TREATED AND PRIMED AREA AND PARTS AT R/H H STAB L/E RIB #1 STIFFENERS #2 REPAIR AS B/737 -700 AMM51-21-41-370-803 AND AMM 51-21-72-370-803.;[14] INSTALLED REPAIR AND APPLIED SEALANT AROUND EDGE AT R/H HORIZONTAL STAB L/E RIB#1 STIFFENERS #2 LOWER RADIOS AS B737 -700 SRM 55-10-09-2R-4 REPAIR 4 AND SOPM 20-50-19.;