In a message dated 1/9/2004 10:29:53 AM Central Standard Time,
gary21sn@hotmail.com writes:
It would seem the line from the fuel pump to the header tank will have
fuel in it because of header tank slosh back from taxi, turns, climb and
turbulence, etc. unless a check valve is in the line.
Rob, et al,
Hmmmm...
Let me describe my setup and experience.
1. Automatic "header full" system keeps the header tank between 8.25 and 9
gallons at all times. Lower level sensor must remain at the lower level
for about 15 seconds before the pumps are started (avoiding start/stop cycles in
turbulence). This assures me of about 1 hour flight time in case of
complete power failure, etc. Indicators show the header full and another
for "timer running."
2. Both pumps (located in the stub wings) are simultaneously
engergized. There are check valves at each header entry point for a
variety of safety reasons - siphoning, negative pressure, etc. The wings
are emptied evenly meaning that lateral trim does not change thru the flight
unless I throw the passenger out.
3. Each pump has its' own pullable breaker and manual on/off
switch. This allows for non-automatic operation. There is no fuel
selector for KISS.
4. VM EPI 800 fuel probes are in all three tanks. They are very
accurate. All tanks produce a warning (I have annunciator lights) when
they are below 4 gallons. I would be gasping for air if the header falls
below 4 gallons (ask the Don about this). The Gallons indicator shows zero
(by design) when below 2 gallons. There is a fuel totalizer running
off the fuel flow sensor, generally 2-3% high, that is another low fuel warning
source.
5. The automatic system is manually turned off when the header does
not refill after dropping to 8 gallons and the wings have been zero for a while.
This probably means the pumps are running "dry" for no more than 15-20
minutes. Slosh, etc. probably means the pumps are not really dry for that
length of time. I have flown in this condition about ten times
(including the Kitty Hawk to Dayton race leg, 10 minutes before
crossing the finish line) and the pumps are still working. The wings have
been emptied in level flight with not much more than a cup of fuel remaining in
each wing as later measured on the ground.
6. The panel is placarded "Do Not Take Off With Less Than 8
Gallons In The Header." There is no experience maneuvering when the
header contained less than 4 gallons, although the header is throughly
baffled.
In flight I cannot hear the pitch of the pumps change when thay run dry
because of their stub wing location - perhaps you can hear them as they are
under the seat. Maybe you could hook up an aural sensor switched into the
audio panel or use a stethoscope, checking heart rate and pump pitch, when
you think the wings are dry.
Scott Krueger
AKA Grayhawk
Sky2high@aol.com
II-P N92EX IO320 Aurora, IL
(KARR)
"...as we know, there are known knowns; there are things we know
we know. We also know there are known unknowns; that is to say we know there are
some things we do not know. But there are also unknown unknowns - the ones we
don't know we don't know." D. Rumsfeld