What was found
DURING WALKAROUND CHECK, FOUND A FUSELAGE SKIN CRACK AT BS 831, 2 INCHES ABOVE S25R. 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 FUSELAGE SKIN CRACK AT BS 831, 2 INCHES ABOVE S25R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.