What was found
CLT - Q5 - MAJOR REPAIR - FUSELAGE FRAME HAS A .250 INCH CRACK AT BS 747, BETWEEN S8L & S9L, ALSO A .062 INCH CRACK AT BS 747, BETWEEN S8R & S9R. REPAIRED FUSELAGE FRAME AT BS 727 BETWEEN S8L & S9L, ALSO BETWEEN S8R & S9R IAW US AIRWAYS TYPICAL REPAIR 53-10-20E.