What was found
CLT - Q6 - MAJOR REPAIR - CRACK ON FUSELAGE FRAME AT BS 616, 8 INCHES BELOW S17R. REPAIRED FUSELAGE FRAME AT BS 616, 8 INCHES BELOW S17R IAW TYPICAL REPAIR 53-62-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - Q6 - MAJOR REPAIR - CRACK ON FUSELAGE FRAME AT BS 616, 8 INCHES BELOW S17R. REPAIRED FUSELAGE FRAME AT BS 616, 8 INCHES BELOW S17R IAW TYPICAL REPAIR 53-62-01.