What was found
2S CHECK - CORROSION ON FUSELAGE SKIN PANEL AT FR63 + 8 INCHES & BETWEEN S41L TO S42L. REPAIRED FUSELAGE SKIN PANEL AT FR63 + 8 INCHES & BETWEEN S41L TO S42L IAW EA 133806.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
2S CHECK - CORROSION ON FUSELAGE SKIN PANEL AT FR63 + 8 INCHES & BETWEEN S41L TO S42L. REPAIRED FUSELAGE SKIN PANEL AT FR63 + 8 INCHES & BETWEEN S41L TO S42L IAW EA 133806.