What was found
DURING INSPECTION, CORROSION WAS FOUND IN THE AFT EDGE AT THE TOP OF THE UPPER LEFT BEARING HALF OF THE MAIN LANDING GEAR FITTING. THE CORROSION WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-010402 REVISION A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, CORROSION WAS FOUND IN THE AFT EDGE AT THE TOP OF THE UPPER LEFT BEARING HALF OF THE MAIN LANDING GEAR FITTING. THE CORROSION WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-010402 REVISION A.