What was found
THE EXTERNAL SKIN OF THE FUSELAGE IS CRACKED AT THE RIVET, AT FRAME 75 & 4 INCHES BELOW THE RT AFT CORNER OF THE DORSAL FIN. ACCOMPLISHED REPAIR TO RT UPPER FUSELAGE SKIN CRACKS IAW ERS-EM-53MR-1748.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
THE EXTERNAL SKIN OF THE FUSELAGE IS CRACKED AT THE RIVET, AT FRAME 75 & 4 INCHES BELOW THE RT AFT CORNER OF THE DORSAL FIN. ACCOMPLISHED REPAIR TO RT UPPER FUSELAGE SKIN CRACKS IAW ERS-EM-53MR-1748.