What was found
(LOG 0387578) CRACK STIFFENER STA 540 RBL=6 THROUGH ACCESS PANEL 192E AT LOWER FUSELAGE. STIFFENER STA 540 RBL=6 THROUGH ACCESS PANEL 192E AT LOWER FUSELAGE WAS REPLACED PER B737-800 SRM 51-40-02-0G.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(LOG 0387578) CRACK STIFFENER STA 540 RBL=6 THROUGH ACCESS PANEL 192E AT LOWER FUSELAGE. STIFFENER STA 540 RBL=6 THROUGH ACCESS PANEL 192E AT LOWER FUSELAGE WAS REPLACED PER B737-800 SRM 51-40-02-0G.