What was found
(AUS) FUSELAGE LAP SPLICE CRACKED ON THE LEFT SIDE BETWEEN BS 340 AND BS400 ADJACENT TO STRINGER 6L. CRA CK LENGTH 0.508 MM (0.020 INCHES). FOUND DURING HIGH FREQUENCY EDDY CURRENT INSPECTION.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(AUS) FUSELAGE LAP SPLICE CRACKED ON THE LEFT SIDE BETWEEN BS 340 AND BS400 ADJACENT TO STRINGER 6L. CRA CK LENGTH 0.508 MM (0.020 INCHES). FOUND DURING HIGH FREQUENCY EDDY CURRENT INSPECTION.