What was found
CRACK INDICATION FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 16 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 0.600 INCH. APPROX. 2024-420742<[01] STEPS 5 AND 6 TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 500D; S/N: 00X12101V022235; CAL DUE DATE: 07-SEP-24;[02] REPAIRED LT HORIZONTAL STABILIZER LOWER SKIN PANEL LOCATED BETWEEN STAB STA 187.5 TO STAB STA 203.5 AND BETWEEN 12 INCHES TO 22 INCHES FROM FRONT SPAR IAW B737-700 SRM 55-10-01-2R-11 REPAIR 11. SEE INDIVIDUAL SIGN OFF BELOW;[03] CORRECTED STEP 2: REPAIRED LT HORIZONTAL STABILIZER LOWER SKIN PANEL LOCATED BETWEEN STAB STA 187.5 TO STAB STA 203.5 AND BETWEEN 12 INCHES TO 22 INCHES FROM FRONT SPAR IAW B737-700 SRM 55-10-01-2R-11 REPAIR 11. ELEVATOR POWER OFF FLIGHT TEST IS NOT NECESSARY DUE TO NOT EXCEED AERODYNAMIC LIMITS ELEVATOR IAW B737-700 SRM 55-10-01-2R-11 PARAGRAPH 4.S. SEE INDIVIDUAL SIGN OFF BELOW;[04] CORRECTED STEP 3: REPAIRED LT HORIZONTAL STABILIZER LOWER SKIN PANEL LOCATED BETWEEN STAB STA 187.5 TO STAB STA 203.5 AND BETWEEN 12 INCHES TO 22 INCHES FROM FRONT SPAR IAW B737-700 SRM 55-10-01-2R-11 REPAIR 11. ELEVATOR POWER OFF FLIGHT TEST IS NOT NECESSARY DUE TO NOT EXCEED AERODYNAMIC LIMITS IAW B737-700 SRM 55-10-01-2R-11 PARAGRAPH 4.S. SEE INDIVIDUAL SIGN OFF BELOW;[05] CERTIFIED WORK PERFORMED AS RII