What was found
CLT - Q1 - MAJOR REPAIR - CRACK ON FUSELAGE SKIN AT BS 727D + 3 INCHES BELOW S23L. REPAIRED FUSELAGE SKIN AT BS 727D + 3 INCHES BELOW S23L IAW EA 102030 DRAFT NR 8.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - Q1 - MAJOR REPAIR - CRACK ON FUSELAGE SKIN AT BS 727D + 3 INCHES BELOW S23L. REPAIRED FUSELAGE SKIN AT BS 727D + 3 INCHES BELOW S23L IAW EA 102030 DRAFT NR 8.