What was found
SKIN PANEL - .25 INCH CRACK INDICATION BOTTOM RIVET ROW SECOND LAYER SKIN LAP JOINT AT BS 817, S4R. REPAIRED FUSELAGE SKIN AT BS 817, S4R IAW B737 SRM 53-00-01, REPAIR 31.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
SKIN PANEL - .25 INCH CRACK INDICATION BOTTOM RIVET ROW SECOND LAYER SKIN LAP JOINT AT BS 817, S4R. REPAIRED FUSELAGE SKIN AT BS 817, S4R IAW B737 SRM 53-00-01, REPAIR 31.