Superior IO-360 (Airflow Performance Pump for the boost pump)
I can't seem to find the specs on fuel pressures from the engine driven fuel pump to set my Dynon EMS.
Thanks in advance for any help.
Minimum fuel pressure at the servo is 14 psi and maximum is 45 psi, for a fuel injected Lycoming 180 HP engine. Normally should run 21-26 psi depending on the power setting. Weather it is a Superior or Lycoming engine shouldn?t make any difference with the spec.Superior IO-360 (Airflow Performance Pump for the boost pump)
I can't seem to find the specs on fuel pressures from the engine driven fuel pump to set my Dynon EMS.
Thanks in advance for any help.
Mark,
The 9 psi is with the mechanical pump only. I'll have to look tomorrow and see how that changes with the boost pump on.
greg
My Superior runs around 30 psi with only the engine driven, mechanical fuel pump operating, but that's pushing fuel into their standard FI setup. I am mystified that the same pump would produce only 9 psi. Are we looking at issues with instrument calibration? I don't see a big change with the boost pump on, either.
Mark,
The 9 psi is with the mechanical pump only. I'll have to look tomorrow and see how that changes with the boost pump on.
greg
OK, just back from 2.4 more hours toward my required 40. Flying at altitudes from 5000 (Reno) to 1800 (Sac Valley) to 11000 (over Sierras). Fuel pressure ran about 9 psi with or without the boost pump on. Dropped to maybe 8.5 when I shoved the throttle forward but rapidly recovered to 9-9.3 (I have all this logged on the Dynon but haven't looked at the detailed log yet).
My suspicion is that there are different takeoff points. I am taking my pressure readings from a split just past the mechanical pump. Perhaps it would/should be higher (25-30) at the spider? I am far from a FI expert, this being my first experience with FI.
This is an interesting discussion...
greg