What was found
CLT - C1 - CRACK ON SKIN PANEL AT AFT END OF E & E EXHAUST PORT CUTOUT AT BS 380 BETWEEN S26R TO S26L. REPAIRED FUSELAGE SKIN AT AFT END OF E & E EXHAUST PORT CUTOUT AT BS 380 BETWEEN S26R TO S26L IAW EA 103113.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - C1 - CRACK ON SKIN PANEL AT AFT END OF E & E EXHAUST PORT CUTOUT AT BS 380 BETWEEN S26R TO S26L. REPAIRED FUSELAGE SKIN AT AFT END OF E & E EXHAUST PORT CUTOUT AT BS 380 BETWEEN S26R TO S26L IAW EA 103113.