Hello Bearhawkers,
I'm still a while away from worrying about the engine side of things, but I've been thinking ahead about my ignition options anyway.
I have an O-360-A1G6D Lycoming overhauled for experimental use, and modified with an updraft MA-4 updraft carburetor.
It came off a twin engine aircraft, and so has only the one drive pad for a Bendix D2000-type dual mag.
Obviously these dual mags aren't really supported going forward, and have a single point of failure, so I'm looking at new options.
I'm thinking of a single IC mag modified to go in this drive pad, and a separate EI system run off crank timing.
The reason I'm going with the traditional mag rather than just blanking off the drive pad and going fully EI is because I just can't bring myself to fully trust anything that has a computer inside it.
Plus I want to do away with the need for a second battery as backup.
As Svyolo says (thread 38792), one EI system will get me about 80% of the benefits of dual. And I might be able to save some money on spark plugs :-)
Ok, so looking around the net, I've discovered:
Light Speed Plasma II
Electroair + EA-003 crank timer.
EFII System 32
seem to be the only companies that offer EI based on crankshaft timing.
All the other systems require putting the timing mechanism into an existing magneto drive pad.
Can anyone suggest any other systems I should start researching?
Or is there a smarter way to look at this whole ignition question? I have zero experience with piston engines, and even less operating fixed wing aircraft, so it's all new to me :-)
BAnton and Rob Caldwall have both installed the Light Speeds - any thoughts on a capacitor discharge type EI in terms of performance and reliability?
Ok, thanks in advance for sharing the wisdom guys :-)
James
I'm still a while away from worrying about the engine side of things, but I've been thinking ahead about my ignition options anyway.
I have an O-360-A1G6D Lycoming overhauled for experimental use, and modified with an updraft MA-4 updraft carburetor.
It came off a twin engine aircraft, and so has only the one drive pad for a Bendix D2000-type dual mag.
Obviously these dual mags aren't really supported going forward, and have a single point of failure, so I'm looking at new options.
I'm thinking of a single IC mag modified to go in this drive pad, and a separate EI system run off crank timing.
The reason I'm going with the traditional mag rather than just blanking off the drive pad and going fully EI is because I just can't bring myself to fully trust anything that has a computer inside it.
Plus I want to do away with the need for a second battery as backup.
As Svyolo says (thread 38792), one EI system will get me about 80% of the benefits of dual. And I might be able to save some money on spark plugs :-)
Ok, so looking around the net, I've discovered:
Light Speed Plasma II
Electroair + EA-003 crank timer.
EFII System 32
seem to be the only companies that offer EI based on crankshaft timing.
All the other systems require putting the timing mechanism into an existing magneto drive pad.
Can anyone suggest any other systems I should start researching?
Or is there a smarter way to look at this whole ignition question? I have zero experience with piston engines, and even less operating fixed wing aircraft, so it's all new to me :-)
BAnton and Rob Caldwall have both installed the Light Speeds - any thoughts on a capacitor discharge type EI in terms of performance and reliability?
Ok, thanks in advance for sharing the wisdom guys :-)
James
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