What was found
(CAN) DURING MANUFACTURING AND INSTALLATION OF THE DORSAL FIN, A RIVET AT THE REAR PRESSURE BULKHEAD (STN 345.0) WAS DRILLED THROUGH THE SKIN, DOUBLER AND FLANGE ANGLE ADJACENT TO A BULKHEAD ATTACHMENT RIVET. AIRCRAFT TT: 2,277 HOURS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) DURING MANUFACTURING AND INSTALLATION OF THE DORSAL FIN, A RIVET AT THE REAR PRESSURE BULKHEAD (STN 345.0) WAS DRILLED THROUGH THE SKIN, DOUBLER AND FLANGE ANGLE ADJACENT TO A BULKHEAD ATTACHMENT RIVET. AIRCRAFT TT: 2,277 HOURS.