Going through some simulated failure scenarios today.
Houston - we have a problem.
Electrical bus MN A seems to have issues, the MDUs powered by it blank, the CWS matrix comes on like a Christmas tree.
Okay, first keep calm, take a deep breath, then look at SM SPEC 67 to find out what the trouble actually is.
Seems something is drawing a LOT of amps here, that's why the voltage is collapsing - seems like a circuit shorted out.
Okay, we can't have that - so first MN A gets disconnected from the fuel cell.
Checking back on SPEC 67, yes, voltage at the cell is back to normal and amps are fine, but of course AC 1 is now unpowered. Can't be helped, but that means we have to take care of some equipment now.
First order of business - avionics bay cooling (they'll overheat within 5-10 minutes if not properly cooled). All fans and water loop pumps need to be switched to either AC 2 or AC 3:
Next are hydraulic circulation pumps - hydraulic system 1 needs to be powered by MN B now.
Payload bay door and payload mechanical power get switched to sys 2.
Now we can take down the fuel cell as it isn't connected to anything, so the shutdown command gets issued and the reactant valves closed next.
Also, since the load is now a bit unevenly distributed, we can tie the remaining buses to drain both surviving cells equally.
Again a look at SPEC 67 - yes, everything properly taken down, the fuel cell shows no voltage any more, voltages on MN B and MN C are equal, power consumption is normal.
Short look at the radiator loops - loop 1 has been affected, loop 2 has been running on fine, so we just switch loop 1 freon pump and controllers away from AC 1.
Whew - all critical systems (cooling mostly...) are back to nominal, quick check of the antenna shows the status okay, so... we're good to continue and discuss options with mission control.