What was found
HYD LEAK FOUND IN NR 2 ENGINE STRUT AREA DURING ENGINE SERVICE AND VISUAL CHECK. REPLACED THRUST REVERSER BI-DIRECTIONAL RESTRICTOR VALVE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
HYD LEAK FOUND IN NR 2 ENGINE STRUT AREA DURING ENGINE SERVICE AND VISUAL CHECK. REPLACED THRUST REVERSER BI-DIRECTIONAL RESTRICTOR VALVE.