What was found
FUSELAGE SKIN IS CORRODED ON EXTERIOR SURFACE AT AFT BOTTOM EDGE OF SERVICE DOOR CUTOUT. CORROSION IS APPROX .002" D. REMOVED LIGHT CORROSION IAW SRM 51-21-06, RESTORED FINISH IAW SRM 51-25-06 & 51-25-26.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN IS CORRODED ON EXTERIOR SURFACE AT AFT BOTTOM EDGE OF SERVICE DOOR CUTOUT. CORROSION IS APPROX .002" D. REMOVED LIGHT CORROSION IAW SRM 51-21-06, RESTORED FINISH IAW SRM 51-25-06 & 51-25-26.