What was found
LEVEL 1 CORROSION FOUND ON FUSELAGE WINDOW FORGING. CORROSION BLENDED AND TREATED. REMAINING THICKNESS .081 INCHES DEEP PER SRM 51-10-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEVEL 1 CORROSION FOUND ON FUSELAGE WINDOW FORGING. CORROSION BLENDED AND TREATED. REMAINING THICKNESS .081 INCHES DEEP PER SRM 51-10-01.