Knowing the GTX 335 was going in, I went thru the power consumption few months ago. Just swapping out the GE 4509 landing light for LED saved almost 10 amps. Position lights went LED, the little position light, then changed the Grimes rotary tail beacon to the Whelen LED. Overall, almost 20 amps.Great looking panel! I am in the process of having the 2nd G5 installed in my PA32-301. I have a Century 41 AP that relies on the vacuum AI so I had to retain the original AI for that purpose. I moved it to the T/C hole and installed the G5 AI in the primary AI hole. Since that install the G5 HSI became certified... I was planning to drag my feet on that addition but recently my NSD-360 HSI began giving me some issues so it was time to make the move.
As this 2nd G5 is being added to my plane it has really made me start thinking about partial panel / alternator failure / vacuum failure / etc. A little over a year ago I was flying a plane where a vacuum failure was a pretty significant event. Standard 6 pack. No electric or backup AI (other than my Ipad and Foreflight) which I really don't trust. Since that time my panel has slowly evolved to be more dependent on the electrical system. I'm studying hard to understand the exact method(s) of failure and have yet to come to any firm conclusions. I thought this thread might be a good place to chime in on that topic.
Here's my panel:
Dual G5's (HSI has GMU-11 and GAD29b)
vacuum AI in T/C hole - to drive AP and even provide a backup AI in the event of a complete electrical failure.
Nav/Com #1 - Avidyne IFD 550- has true SV
Nav/Com #2 - KX155 w/out glideslope / has it's own CDI.
JPI 830
GMA 340
Avidyne remote ADSB transponder (in and out)
So here are the two primary modes of failure:
1- vacuum- almost a non-event as it does kill my autopilot, but I honestly haven't been relying on the vacuum AI for the primary scan anyway. I'll just have to hand fly and that should be pretty simple given my panel.
2- electrical failure - obviously an "event"! Let's look for the weak link shall we. One thing I love about the G5's is their huge independent battery. That's great. Should easily have a solid AI for the remainder of the flight. But wait... How about the HSI??? It's got power but will it work? Well, this where my head scratching starts. Assuming main-ship battery has depleted the GMU-11 magnetometer and the GAD29b will fail. Now my HSI is gone. Will it show track? Not if the IFD550, GMU-11, and GAD29B are all dead. So I'll essentially be left with an AI (OK 3 if you count the dual G5's and the vacuum AI) but zero NAV info. In this case declare an emergency and get vectored to the nearest airport.
I think the next step I need to take is to find out the power (amp) draw for each piece of equipment. Figure out which pieces are essential to get down and land and have a known time frame for that to happen. One thing I love about the JPI 830 is that I set a low voltage alarm, so I am instantly notified of an alternator failure.
I don't mean to hijack the thread. I just think as we transition more and more to electric panels it's super important to know the results of that failure and the steps to take to turn an emergency into a non-event. Power management will be critical with the last resort being what to do if/when it's all gone.
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