What was found
CORROSION EXTERNAL SKIN LOCATED BETWEEN BS 1016 AND BS 1040 BETWEEN S-3R AND S-3L WL308.5 AT UPPER FUSELAGE 2022-283998 / [01] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC600D; S/N: 60007161486; CAL DUE DATE: 06-DEC-22;[02] TOOL USED: ULTRASONIC THICKNESS GAGE; P/N: 45MG; S/N: 130066401; CAL DUE DATE: 17-JUN-22;[03] REMOVED CORROSION ON EXTERNAL SKIN LOCATED BETWEEN BS 1016 AND BS 1040 BETWEEN S-3R AND S-3L WL308.5 AT UPPER FUSELAGE IAW B737-700 SRM 51-10-02-0G-0; AND EVALUATED REWORKED AREA POINT 1; POINT 2; POINT 4 AND POINT 5 FOUND WITHIN LIMITS IAW B737-700 SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 PARAGRAPH 4.C.(2)(A) FIGURE 103 DETAIL D EXCEPT POINT 3 THAT IS OUT LIMITS MUST BE REPAIRED; REPAIR DOCUMENTED ON TTG8Q00CNEGC.<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[04] CORRECTED STEP 3<BR>REMOVED CORROSION ON EXTERNAL SKIN LOCATED BETWEEN BS 1016 AND BS 1040 BETWEEN S-3R AND S-3L WL308.5 AT UPPER FUSELAGE IAW B737-700 SRM 51-10-02-0G-0; AND EVALUATED REWORKED AREA POINT 1; POINT 2; POINT 4 AND POINT 5 FOUND WITHIN LIMITS IAW B737-700 SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 PARAGRAPH 4.C.(2)(A) FIGURE 103 DETAIL D; NO FURTHER ACTION OR INSPECTION REQUIRED. EXCEPT POINT 3 THAT IS OUT LIMITS MUST BE REPAIRED; REPAIR DOCUMENTED ON TTG8Q00CNEGC.<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[05] CERTIFIED STEP 4 COMPLETED