What was found
FUSELAGE FRAME OUTER CHORD WEB CRACKED AT BS 348.2, STRINGER 16L. REPAIRED WEB IAW ER & EA.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FRAME OUTER CHORD WEB CRACKED AT BS 348.2, STRINGER 16L. REPAIRED WEB IAW ER & EA.