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Matt Young
October 13th 04, 05:39 AM
Ok, a curious question just popped in my mind. Say that one was flying
IFR in a piston single, maybe a 172 or 182. While enroute, either in
actual or above a cloud layer, the engine fails. Will the windmilling
prop keep the vacuum pump going enough to make the AI and DG usuable
during descent through the clouds, or will the gyros keep spinning fast
enough long enough to make the vacuum pump irrelevant?

Dave Butler
October 13th 04, 03:16 PM
Matt Young wrote:
> Ok, a curious question just popped in my mind. Say that one was flying
> IFR in a piston single, maybe a 172 or 182. While enroute, either in
> actual or above a cloud layer, the engine fails. Will the windmilling
> prop keep the vacuum pump going enough to make the AI and DG usuable
> during descent through the clouds, or will the gyros keep spinning fast
> enough long enough to make the vacuum pump irrelevant?

No and no.

MC
October 13th 04, 03:33 PM
Matt Young wrote:
> Ok, a curious question just popped in my mind. Say that one was flying
> IFR in a piston single, maybe a 172 or 182. While enroute, either in
> actual or above a cloud layer, the engine fails. Will the windmilling
> prop keep the vacuum pump going enough to make the AI and DG usuable
> during descent through the clouds, or will the gyros keep spinning fast
> enough long enough to make the vacuum pump irrelevant?

Whilst doing a engine runup at about 2000 rpm my vacuum indicates
'normal', and even during taxying at around 1000 rpm the AH is stable.

So., if the engine fails *but the prop still keeps turning* at a
reasonable rate (eg above 1000rpm) then I'd expect that there
should still be sufficient 'vacuum' to operate the gyro instruments.
With *no* vacuum, (eg after engine shutdown) my gyros starts
drifting after about a minute.

Ron Natalie
October 13th 04, 05:32 PM
Matt Young wrote:
> Ok, a curious question just popped in my mind. Say that one was flying
> IFR in a piston single, maybe a 172 or 182. While enroute, either in
> actual or above a cloud layer, the engine fails. Will the windmilling
> prop keep the vacuum pump going enough to make the AI and DG usuable

Depends on your pump and what RPM's you can expect the prop to windmill
at. My pump will produce 4" at idle and if you just shut off the fuel
to the engine, the prop will windmill in the glide at well above idle
(actually, you can't really tell by the RPM's that the engine isn't
running).

Of course, if your engine siezes, you're not going to get any windmilling.

> during descent through the clouds, or will the gyros keep spinning fast
> enough long enough to make the vacuum pump irrelevant?

It's amazing how FAST the gyros spin down (and how long it takes them
to spin up). I had a pump crump on takeoff roll and before I was at
pattern altitude the AI had started to lean over (fortunately in VMC).

No Such User
October 13th 04, 06:26 PM
In article t>,
Matt Young wrote:
>during descent through the clouds, or will the gyros keep spinning fast
>enough long enough to make the vacuum pump irrelevant?

I question the wisdom of relying on an instrument that you already know to
have failed. You would need to know just how long you can stare at it
in a very stressful situation before you can no longer believe what it
tells you. I would think that immediately covering the instrument would
be your best course of action in this scenario.

Ron Natalie
October 13th 04, 08:27 PM
No Such User wrote:
> In article t>,
> Matt Young wrote:
>
>>during descent through the clouds, or will the gyros keep spinning fast
>>enough long enough to make the vacuum pump irrelevant?
>
>
> I question the wisdom of relying on an instrument that you already know to
> have failed.

What makes you think it has failed? If the vacuum guage still shows a vacuum,
then the gyro's got to spin (unless you are unlucky enough to have a second
failure of the vacuum system at the same time that the engine crumped).

What I've never understood is why there isn't more obvious indication that
there is no power (vacuum or electric as required) going to the instrument.
Jeez, the VOR which isn't as essential to instrument flight has a better
indication that it's not on.

David Megginson
October 13th 04, 08:41 PM
Dave Butler wrote:
> Matt Young wrote:
>
>> Ok, a curious question just popped in my mind. Say that one was
>> flying IFR in a piston single, maybe a 172 or 182. While enroute,
>> either in actual or above a cloud layer, the engine fails. Will the
>> windmilling prop keep the vacuum pump going enough to make the AI and
>> DG usuable during descent through the clouds, or will the gyros keep
>> spinning fast enough long enough to make the vacuum pump irrelevant?
>
>
> No and no.

Personal experience, credible sources, or just a guess?


All the best,


David

Dave Butler
October 13th 04, 09:15 PM
David Megginson wrote:
> Dave Butler wrote:
>
>> Matt Young wrote:
>>
>>> Ok, a curious question just popped in my mind. Say that one was
>>> flying IFR in a piston single, maybe a 172 or 182. While enroute,
>>> either in actual or above a cloud layer, the engine fails. Will the
>>> windmilling prop keep the vacuum pump going enough to make the AI and
>>> DG usuable during descent through the clouds, or will the gyros keep
>>> spinning fast enough long enough to make the vacuum pump irrelevant?
>>
>>
>>
>> No and no.
>
>
> Personal experience, credible sources, or just a guess?

1A. Will it keep the vacuum pump going? No, just a guess. You might have a
better shot at it with a controllable prop. That assumes, of course, that
whatever caused the engine to stop making noise didn't prevent it from spinning
'round.

1B. Will the instruments keep spinning enough? No, just a guess, reinforced by
my experience testing the Precise Flight backup vacuum system when it was
installed in the Archer I used to own. To calibrate the altitude limits on the
placard, you have to fly with varying levels of vacuum and note the instrument
performance. The vacuum doesn't have to be much below specified minimum (is it 4
inHg?) before the gauges get really squirrely. Noting how long it takes the
gyros to spin down while the plane is stationary on the ramp after you shut down
is not a useful measure.

2. It's easy to test. Try it for yourself if you really want to know.

3. I wouldn't rely on a usenet answer if it were 'yes'.

4. Even if I tested it and it worked, I wouldn't rely on it working when I need it.

Short answer: it was a guess.

David Megginson
October 13th 04, 09:21 PM
Dave Butler wrote:

> 3. I wouldn't rely on a usenet answer if it were 'yes'.

Very wise.

> 4. Even if I tested it and it worked, I wouldn't rely on it working when
> I need it.
>
> Short answer: it was a guess.

Fair enough. My gyros behave fine on an instrument approach down to 1500
rpm, so I'd be pretty comfortable trusting them as long as I could keep my
Warrior's speed up high enough to spin the prop that fast; unfortunately,
with an engine out, that might mean descending a lot faster than I really
need to. As long as my TC were usable, I would find it hard to justify
sacrificing a lot of glide range just to keep the vacuum pump working.


All the best,


David

Bill Hale
October 13th 04, 10:05 PM
Dave Butler > wrote in message >...
> Matt Young wrote:
> > Ok, a curious question just popped in my mind. Say that one was flying
> > IFR in a piston single, maybe a 172 or 182. While enroute, either in
> > actual or above a cloud layer, the engine fails. Will the windmilling
> > prop keep the vacuum pump going enough to make the AI and DG usuable
> > during descent through the clouds, or will the gyros keep spinning fast
> > enough long enough to make the vacuum pump irrelevant?
>
> No and no.

No and maybe.

Especially with a constant speed prop, you will wish to pull the
prop pitch to low rpm to get the longest glide. Your pump will be doing
about nothing -- tho the wet ones will make some vacuum even as you crank.

The gyros will typically run for ~ 5 min, but they lose the erection
function caused by the vacuum loss.

But heck, unless you are REALLY high, they will run at least sort
of until you contact the earth. It's not that many minutes.

Bill Hale

Dave Butler
October 14th 04, 02:18 PM
Bill Hale wrote:

> The gyros will typically run for ~ 5 min, but they lose the erection
> function caused by the vacuum loss.

You must have way better bearings than I do... or maybe you're measuring the
time to when they stop spinning. They become useless for attitude control way
before they stop spinning.

Not sure what the 'erection function' is. I'm afraid to ask.

Bob Moore
October 14th 04, 02:30 PM
Dave Butler wrote

> Not sure what the 'erection function' is. I'm afraid to ask.

Research pendulous vanes.

Bob Moore

Dave Butler
October 14th 04, 02:56 PM
Bob Moore wrote:

> Research pendulous vanes.

Thanks, Bob, I know what pendulous vanes are, but I was having trouble relating
pendulous vanes to the context of lost vacuum due to engine stoppage. The poster
wrote:

> The gyros will typically run for ~ 5 min, but they lose the erection
> function caused by the vacuum loss.

Ron Natalie
October 14th 04, 04:19 PM
Bob Moore wrote:
> Dave Butler wrote
>
>
>>Not sure what the 'erection function' is. I'm afraid to ask.
>
>
> Research pendulous vanes.
>
Sort of gyroscopic viagra?

Roger
October 14th 04, 08:08 PM
On Wed, 13 Oct 2004 04:39:47 GMT, Matt Young >
wrote:

>Ok, a curious question just popped in my mind. Say that one was flying
>IFR in a piston single, maybe a 172 or 182. While enroute, either in
>actual or above a cloud layer, the engine fails. Will the windmilling
>prop keep the vacuum pump going enough to make the AI and DG usuable
>during descent through the clouds, or will the gyros keep spinning fast
>enough long enough to make the vacuum pump irrelevant?

Your 're going to get answers all over the spectrum, but my take would
be it might happen, but don't count on it to save your bacon. IOW,
I'd not count on them working, or staying accurate which is
_far_worse_ than not working when you are in the clouds.

There are many variables such as the actual engine, prop, and vacuum
pump combination as well as best glide speed.

Its been my experience (which may not be typical) that a wet pump will
do better with the low RPM than the dry pump. This is assuming you
still have RPM which with a catastrophic failure you probably won't.

In my particular airplane which has a wet pump and a constant speed
prop, once the instruments are spun up even vacuum at idle (which is
well below the minimum) will keep the AI and DG working. The AI stays
accurate. The DG will start precessing but slowly although it does
hold well with a prolonged idle on the ground. Actually it's close to
being in tolerance. With full vacuum I don't have to reset it during
a 3 to 4 hour flight.

So, I'd expect to see the vacuum instruments "on mine" hold for some
time, but even knowing them as well as I do, I'd still depend on
partial panel and consider any use out of the vacuum instruments a
bonus.

Roger Halstead (K8RI & ARRL life member)
(N833R, S# CD-2 Worlds oldest Debonair)
www.rogerhalstead.com

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