What was found
DURING WALKAROUND CHECK, FOUND A 2.25 INCH FUSELAGE SKIN CRACK AT BS 814, AT S16L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING WALKAROUND CHECK, FOUND A 2.25 INCH FUSELAGE SKIN CRACK AT BS 814, AT S16L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.