What was found
(CAN) LOWER FUSELAGE SKIN CRACKED APPROXIMATELY 5 INCHES LONG AT R/H SIDE STRINGER 31 FUSELAGE STATION 1368, PRESSURIZED AREA. OPPOSITE SIDE ALSO CRACKED. SKIN CORROSION DUE TO WASTE WATER TRAPPED IS PROBABLE CAUSE. REPAIRED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) LOWER FUSELAGE SKIN CRACKED APPROXIMATELY 5 INCHES LONG AT R/H SIDE STRINGER 31 FUSELAGE STATION 1368, PRESSURIZED AREA. OPPOSITE SIDE ALSO CRACKED. SKIN CORROSION DUE TO WASTE WATER TRAPPED IS PROBABLE CAUSE. REPAIRED.