What was found
2S CHECK - CORROSION ON EXTERNAL FUSELAGE SKIN PANEL AT FR 63+8 INCHES BETWEEN S40L TO S43L. REPAIRED EXTERNAL FUSELAGE SKIN PANEL AT FR 63+8 INCHES BETWEEN S40L TO S43L IAW EA 133741.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
2S CHECK - CORROSION ON EXTERNAL FUSELAGE SKIN PANEL AT FR 63+8 INCHES BETWEEN S40L TO S43L. REPAIRED EXTERNAL FUSELAGE SKIN PANEL AT FR 63+8 INCHES BETWEEN S40L TO S43L IAW EA 133741.