What was found
FUSELAGE FRAME CRACKED ON INNER CHORD STRAP AT LOWER END BS 616, S17L. REPAIRED FUSELAGE FRAME ON INNER CHORD STRAP AT LOWER END BS616, S17L IAW AMM 2015-05 AND 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 STRAP AT LOWER END BS 616, S17L. REPAIRED FUSELAGE FRAME ON INNER CHORD STRAP AT LOWER END BS616, S17L IAW AMM 2015-05 AND REPAIR 53-62-01. (K)