Hi Finn
Thanks for the reminder of my pump issue.
Yes, you chose more wisely the pump capacity.
Mine were way overkill.
So I’m thinking options are:
1. Fuel Pressure transducer fault - No - as
this was confirmed by the mixture monitor and tune going
out.
2. Power supply to pump via fault in
termination or switch current path - Unlikely, given the
slow reduction - I would imagine a faulty connection would
create a less uniform symptom.
3. Alternator Battery voltage/current
reduction over time - No - You would see this in the log.
4. Significant Fuel leak - No - Would think
this would have become obvious on inspection and not
intermittent.
5. Fuel Regulator - They are pretty simple but
unsure if they can fail with this symptom?
6. Fuel filter blockage - Certainly this would
have to be an obvious, but I take it you swapped this out.
7. Pump internal failure -
Electrical
- ?
Mechanical
breakage - ?
Flow
Path - blockage - unlikely if filtered effectively
Where is your pressure transducer in relation
to Reg/Any post pump filtering/Flow Transducer/Rail?
If fuel regulator and filters can be
discounted, I’m struggling to trust the pump. But your
test had it sounding in good shape and to spec.
So frustrating.
Cheers
Steve
Thanks Steve.
>From your March/April 2017 posts it was a
GSL392 that failed (high current draw/low
pressure, even after you removed the insect you
found in the inlet).
So this afternoon I ran the pump for about an
hour. Amp draw from 3.04 to 286 depending on
voltage. Pressure between 43 and 40 psi (also
depending on voltage). No noticeable
degradation. Of course the difference with this
test is that no fuel went to engine -- all
recirculated through pressure regulator and back
to tank. But no signs of a failing pump in terms
of higher current draw and less pressure.
I guess I should put a temp probe on the pump
and see what it reads during flight to see if
that could be a factor.
Finn
On 5/21/2022 9:01 PM, Stephen Izett
stephen.izett@gmail.com wrote:
Hi
Finn
I had from memory a 393 fail.
Can’t recall the symptoms sorry.
I test before takeoff and then run
both pumps below 2ooo ft incase of failure.
I plan to instal a comparator
relay board in fuel pressure circuit to
automatically bring on backup pump and failure
indicator.
So testing before flight becomes -
switch off and back on main engine pump. This
will save amps and wear of backup pump.
When I switch off a pump at WOT
the engine dies pretty much instantaneously
and don't want to be fiddling with a restart
in the Glasair which glides like a brick with
the gear out in the breeze.
Regards
Steve Izett
Recently I noticed my fuel
pressure being low. Noticed because
engine did not come up in power when
advancing to full throttle. Noticed
mixture real lean. Checking fuel
pressure as low as 28 psi (normally
35 and up to 40 at full throttle).
Going over my engine logs
since first flight I now see that
fuel pressure has been trending
lower through each flight -- more
pronounced on longer flights (40+
minutes). More and more pronounced
over the months and became really
noticeable over last month. Could
explain why mixture tuning appeared to have
changed. Nice to have engine logs
from practically each flight.
But why? Pump getting weaker?
My primary fuel pump is a
GSL414. I figured it was wasted
energy to push way more fuel than
needed through the pressure
regulator back to the tank.
My secondary (backup) pump
is a GSL393. When turning that on,
fuel pressure comes back up to where
it needs to be.
Anyone have experience
with failing or weak EFI pumps,
particularly the GSL414?
Finn