What was found
DURING SERVICE CHECK FOUND A 2.5" CRACK ON THE RT SIDE FUSELAGE AT BS 360+4, BELOW STRINGER 14R. THE CRACK WAS REPAIRED IAW ENGINEERING CHANGE ORDER 3824, SB 737-53A1177 REV 6 & SRM 53-30-03, FIGURE 48.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SERVICE CHECK FOUND A 2.5" CRACK ON THE RT SIDE FUSELAGE AT BS 360+4, BELOW STRINGER 14R. THE CRACK WAS REPAIRED IAW ENGINEERING CHANGE ORDER 3824, SB 737-53A1177 REV 6 & SRM 53-30-03, FIGURE 48.