What was found
CLT Q5 MAJOR REPAIR NR 03C10753038/006 FUSELAGE FRAME CRACKED ON INNER CHORD AT BS 601, S17R, WL 202, RBL 66. REPAIRED FUSELAGE FRAME INNER CHORD AT BS 601, S17R, WL 202, RBL 66 IAW EA NR 100688.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT Q5 MAJOR REPAIR NR 03C10753038/006 FUSELAGE FRAME CRACKED ON INNER CHORD AT BS 601, S17R, WL 202, RBL 66. REPAIRED FUSELAGE FRAME INNER CHORD AT BS 601, S17R, WL 202, RBL 66 IAW EA NR 100688.