What was found
(CAN) DURING A PHASE 1-5 INSPECTION OF THE MAIN LANDING GEAR THE AXLE EXPANSION PLUG PN 5514350 WAS FOUND CORRODED. UPON REMOVAL OF THE PLUG CORROSION WAS FOUND ON THE AXLE BORE APPROXIMATELY 1.5 INCHES FROM THE END.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) DURING A PHASE 1-5 INSPECTION OF THE MAIN LANDING GEAR THE AXLE EXPANSION PLUG PN 5514350 WAS FOUND CORRODED. UPON REMOVAL OF THE PLUG CORROSION WAS FOUND ON THE AXLE BORE APPROXIMATELY 1.5 INCHES FROM THE END.