What was found
CDFI CHECK - 3 INCH CRACK IN FUSELAGE FRAME INNER CHORD AT BS 616, WL 208, RBL 70.85. REPAIRED FUSELAGE FRAME INNER CHORD AT BS 616, WL 208, RBL 70.85 IAW B737 51-40-02 & BOEING DRAWING 65-40539.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CDFI CHECK - 3 INCH CRACK IN FUSELAGE FRAME INNER CHORD AT BS 616, WL 208, RBL 70.85. REPAIRED FUSELAGE FRAME INNER CHORD AT BS 616, WL 208, RBL 70.85 IAW B737 51-40-02 & BOEING DRAWING 65-40539.