What was found
SUPPLEMENTAL INFORMATION: R/H STAB INSPAR RIB ASSY NO. 5 AT STAB STA 129.50 STIFFENER NO.4 CRACKED ; / [01] TRIMMED OUT DAMAGED AREA ON RH STAB INSPAR RIB ASSY NO. 5 AT STAB STA 129.5 STIFFENER 4 AS PER B737-700 SRM 55-10-09-2R-4; [06] FABRICATED REPAIR PARTS (SHIM; FILLER AND ANGLE (BAC1490-2793)) AS PER B737-700 SRM 55-10-09-2R-5. FIG 204.; [15] INSTALLED REPAIR PARTS (SHIM; FILLERS; ANGLE (BAC1490-2793) AND REPAIR STIFFENER) AS PER B737-700 SRM 51-40-02-0G-0 AND 55-10-09-2R-5. FIG 204.; [16] VERIFIED STEP 15; [17] APPLIED FILLET SEALANT ON REPAIR EDGES AS PER SOPM 20-50-19; [18] TRIMMED OUT DAMAGED AREA ON RH STAB INSPAR RIB ASSY NO. 5 AT STAB STA 129.5 STIFFENER 4 AS PER B737-700 SRM 55-10-09-2R-5. PERFORMED HFEC INSP; NO CRACKS. PERFORMED A FASTENER HOLE INSPECTION (ROTARY SCANNER); NO CRACKS. ACCOMPLISHED A GVI OF ALL AREAS WITHIN THE REPAIR AREA. NO OTHER DEFECTS NOTE. FABRICATED REPAIR PARTS (SHIM; FILLERS; ANGLE (BAC1490-2793) AND REPAIR STIFFENER) AS PER B737-700 SRM 55-10-09-2R-5. FIG 204. TREATED AND PRIMED REWORKED AREAS AND REPAIR PARTS AS PER B737-700 AMM 51-21-41-370-803 AND 51-21-72-370-804. INSTALLED REPAIR PARTS (SHIM; FILLERS; ANGLE (BAC1490-2793) AND REPAIR STIFFENER) AS PER B737-700 SRM 51-40-02-0G-0 AND 55-10-09-2R-5. FIG 204.;