What was found
CLT - Q2 - CRACK ON FUSELAGE FRAME AT BS 380 BETWEEN S20L TO S21L. REPAIRED FUSELAGE FRAME AT BS 380 BETWEEN S20L TO S21L IAW EA 102696.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - Q2 - CRACK ON FUSELAGE FRAME AT BS 380 BETWEEN S20L TO S21L. REPAIRED FUSELAGE FRAME AT BS 380 BETWEEN S20L TO S21L IAW EA 102696.