What was found
CLT - Q5 - MAJOR REPAIR - FUSELAGE FRAME HAS A .125 INCH CRACK AT BS 440, BETWEEN S8R & S9R. ALSO BETWEEN S8L & S9L. REPAIRED FUSELAGE FRAME AT BS 440, BETWEEN S8R & S9R, ALSO BETWEEN S8L & S9L IAW US AIRWAYS TYPICAL REPAIR 53-10-20E.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - Q5 - MAJOR REPAIR - FUSELAGE FRAME HAS A .125 INCH CRACK AT BS 440, BETWEEN S8R & S9R. ALSO BETWEEN S8L & S9L. REPAIRED FUSELAGE FRAME AT BS 440, BETWEEN S8R & S9R, ALSO BETWEEN S8L & S9L IAW US AIRWAYS TYPICAL REPAIR 53-10-20E.