I recently simulated an engine fire (eng #2) during climb. The fire came up at FL300 and was successfully extinguished. I followed the PMDG QRH procedures.
Once the engine 2 was stopped, I checked my hydraulics and both systems were fine.
As I approached the airport for landing, the Hydraulic System B failed (no more pressure / "overhead" indicated for system B. I was able to land using the alternate flaps.
My question; was the Hydraulic failure Syst B a result of the Eng 2 fire or was it a result of my (mis)management of the engine fire ?
I have completed this "simulation" a few times in the past and I am pretty sure I had the hydraulic problem each time.
Thanks