What was found
(SUPPORT TASK) FUSELAGE SKIN BETWEEN STA 360 TO 380 STR 25 L/H FASTENERS ARE PULLING THROUGH THE SKIN. PERFORMED REPAIR AT FUSELAGE SKIN BETWEEN STA 360 TO STA 380 STR EDGE IAW B737 SRM 53-00-03-2R-1 FIG 205, SRM 51-40-02, SRM 25L AND REMOVED AND REINSTALLED SUB STRUCTURAL PARTS FOR REPAIR 51-20-01, AMM 24-21-71, 737 NDT MANUAL PT6 51-00-00. FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR PARTS AT S25L BS360 TO 380. PERFORMED NDT HFEC OF THE STRINGER CUT.