I thought i would share the FMEA i have been working on for my RV-14. It will be an electrically dependent aircraft.
This was a pretty useful process - it highlighted some operational checks i realised i needed to add (some at each flight, some monthly (occasionally) and some at the 100 hourly). It also showed me i think i need to go with 2 seperate firewall ground blocks for redundancy - otherwise everything is coming back to one bolt!
I still have to decide if i want to dual feed my essential bus with diodes (i have a couple there so it wouldn't be hard). But it is only guarding against a single failure (the shorting of the essential bus feed wire), so may not be worth it.
If anyone is bored and wants to take a look the whole docuement is here:
docs.google.com
Otherwise, the printouts are attached.
Welcome any feedback!
This was a pretty useful process - it highlighted some operational checks i realised i needed to add (some at each flight, some monthly (occasionally) and some at the 100 hourly). It also showed me i think i need to go with 2 seperate firewall ground blocks for redundancy - otherwise everything is coming back to one bolt!
I still have to decide if i want to dual feed my essential bus with diodes (i have a couple there so it wouldn't be hard). But it is only guarding against a single failure (the shorting of the essential bus feed wire), so may not be worth it.
If anyone is bored and wants to take a look the whole docuement is here:
FMEA VH-TBA SDS-EFI.xlsx
Otherwise, the printouts are attached.
Welcome any feedback!
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