What was found
FUSELAGE SKIN CHAFED BETWEEN BS 1825 AND 1878 AND ABOVE S17L. REMOVED AND REPLACED WITH SKIN FABRICATED AS PER DWG 148N7303, SHT.1, REV. AND INSTALLED IAW DWG 148N7301, SHT 1, REV A. REPAIR IS MAJOR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN CHAFED BETWEEN BS 1825 AND 1878 AND ABOVE S17L. REMOVED AND REPLACED WITH SKIN FABRICATED AS PER DWG 148N7303, SHT.1, REV. AND INSTALLED IAW DWG 148N7301, SHT 1, REV A. REPAIR IS MAJOR.