What was found
FUSELAGE FRAME CRACKED ON INNER CHORD AT BS601, S17R. REPAIRED FUSELAGE FRAME INNER CHORD AT BS 601, S17R IAW TYPICAL REPAIR 53-62-01. (K)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FRAME CRACKED ON INNER CHORD AT BS601, S17R. REPAIRED FUSELAGE FRAME INNER CHORD AT BS 601, S17R IAW TYPICAL REPAIR 53-62-01. (K)