I'm having an Aerospace logic fuel flow instrument installed on my 79' 8KCAB AEIO360HIA. The instructions say to install transducer in the fuel line between the throttle body and flow divider and in a horizontal plane. That being the case, the only place it seems to fit on this aircraft is on top of the engine, after the baffling and before where the fuel line enters the flow divider.
Does anyone have any experience or advice on this setup? Any pictures of completed set up? I am fairly certain JPI and others use same transducer.
Thanks.
Does anyone have any experience or advice on this setup? Any pictures of completed set up? I am fairly certain JPI and others use same transducer.
Thanks.