What was found
CLT - Q6 - RIB, (1.5 AND .3750 INCH) CRACK; H WING, ROB AT WS 505 UPPER FLANGE RADIUS 20 INCH FROM L/E OF RIB. INSTALLED REPAIR DOUBLER IAW EA. (K)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - Q6 - RIB, (1.5 AND .3750 INCH) CRACK; H WING, ROB AT WS 505 UPPER FLANGE RADIUS 20 INCH FROM L/E OF RIB. INSTALLED REPAIR DOUBLER IAW EA. (K)