What was found
DURING SCHEDULED SC CHECK, FOUND A 4 INCH CRACK IN FUSELAGE SKIN 27 INCHES FWD OF OUTFLOW VALVE, BETWEEN STRINGERS 27 AND 26R. REPAIRED PER BOEING SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED SC CHECK, FOUND A 4 INCH CRACK IN FUSELAGE SKIN 27 INCHES FWD OF OUTFLOW VALVE, BETWEEN STRINGERS 27 AND 26R. REPAIRED PER BOEING SRM.