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Tail lifting during full power static test

 
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JhnstnIII(at)aol.com
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PostPosted: Wed Aug 16, 2006 6:00 pm    Post subject: Tail lifting during full power static test Reply with quote

Listers--We are close to flying our RV-6. On the airworthiness certificate application it requires the builder to state that "the powerplant installation has undergone at least one hour of ground operation at various speeds from idle to full power. . . ." Yesterday during the first full power static test holding brakes and with the stick full aft the tail came up on me. Because I was approaching full power gradually (being nervous about just this sort of possibility) I was able to quickly close the throttle before the prop hit the ground.

Aircraft has an 0-360 and constant speed prop. Aircraft was light with just me aboard and a few gallons of fuel. Aircraft was recently weighed and empty CG was a few inches aft of forward limit.

I was able to complete the test by tying down the tail securely. It is still not a pleasant test to do.

Tonight checking the archives I see this characteristic has been reported previously (in 1999) for both the RV-6 and the RV-8 with constant speed props.

Thought I would mention it again for anyone out there about to do this test. Be very careful.

LeRoy Johnston in Ohio.
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pitts_pilot(at)bellsouth.
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PostPosted: Wed Aug 16, 2006 6:12 pm    Post subject: Tail lifting during full power static test Reply with quote

JhnstnIII(at)aol.com (JhnstnIII(at)aol.com) wrote:
Quote:
Listers--We are close to flying our RV-6. On the airworthiness certificate application it requires the builder to state that "the powerplant installation has undergone at least one hour of ground operation at various speeds from idle to full power. . . ." Yesterday during the first full power static test holding brakes and with the stick full aft the tail came up on me. Because I was approaching full power gradually (being nervous about just this sort of possibility) I was able to quickly close the throttle before the prop hit the ground.
Good move! Also be careful when doing a full-power runup prior to taking the runway. The nose-over syndrome should be lessened with full fuel. However, if you don't have the brakes holding completely under high power and the plane starts to move ..... the normal impulse is to press harder on the brake pedals. That small additional momentum may be enough to put the TD up on it's nose, and pulling the power may not work. Just something to think about.
Linn
do not archive
[quote]

Aircraft has an 0-360 and constant speed prop. Aircraft was light with just me aboard and a few gallons of fuel. Aircraft was recently weighed and empty CG was a few inches aft of forward limit.

I was able to complete the test by tying down the tail securely. It is still not a pleasant test to do.

Tonight checking the archives I see this characteristic has been reported previously (in 1999) for both the RV-6 and the RV-8 with constant speed props.

Thought I would mention it again for anyone out there about to do this test. Be very careful.

LeRoy Johnston in Ohio.
Quote:


[b]


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dbris200(at)sbcglobal.net
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PostPosted: Wed Aug 16, 2006 8:33 pm    Post subject: Tail lifting during full power static test Reply with quote

Also, be very careful with that hour of ground operation, if you have a new or overhauled engine you can ruin it in short order. Watch your temps closely. And, it's a bad idea to do a full power runup in any small taildragger without the tail tied down.

Dave -6 So Cal


linn Walters wrote: [quote] JhnstnIII(at)aol.com (JhnstnIII(at)aol.com) wrote:
Quote:
Listers--We are close to flying our RV-6. On the airworthiness certificate application it requires the builder to state that "the powerplant installation has undergone at least one hour of ground operation at various speeds from idle to full power. . . ." Yesterday during the first full power static test holding brakes and with the stick full aft the tail came up on me. Because I was approaching full power gradually (being nervous about just this sort of possibility) I was able to quickly close the throttle before the prop hit the ground.
Good move! Also be careful when doing a full-power runup prior to taking the runway. The nose-over syndrome should be lessened with full fuel. However, if you don't have the brakes holding completely under high power and the plane starts to move ..... the normal impulse is to press harder on the brake pedals. That small additional momentum may be enough to put the TD up on it's nose, and pulling the power may not work. Just something to think about.
Linn
do not archive
Quote:


Aircraft has an 0-360 and constant speed prop. Aircraft was light with just me aboard and a few gallons of fuel. Aircraft was recently weighed and empty CG was a few inches aft of forward limit.

I was able to complete the test by tying down the tail securely. It is still not a pleasant test to do.

Tonight checking the archives I see this characteristic has been reported previously (in 1999) for both the RV-6 and the RV-8 with constant speed props.

Thought I would mention it again for anyone out there about to do this test. Be very careful.

LeRoy Johnston in Ohio.
Quote:



[b]


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jack.lockamy(at)navy.mil
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PostPosted: Thu Aug 17, 2006 7:06 am    Post subject: Tail lifting during full power static test Reply with quote

Why not be safe and ensure the tail is TIED DOWN and SECURE while doing this type of full-power run-up(s) test? Surely there is a place on the airport you could find a well anchored tiedown.
I know of two cases at our airport where the tail came up (RV-6s) and both guys ended up buying new props and paying for an engine tiedown prior to first flight. Unbelievable.... but it still continues to happen. Doesn't have to... but it does! Amazing...
Jack [quote][b]


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gerf(at)gerf.com
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PostPosted: Thu Aug 17, 2006 7:16 am    Post subject: Tail lifting during full power static test Reply with quote

Did you're engine supplier not run your engine in the test
stand before delivering it to you ? It should be marked in the
log book, I think. I.E. do you really need to run it for a
whole hour ? Aerosport ran my engine for a total of 45 mins
before it was delivered - so apart from a short short "shake
down" run and some taxi tests - its next run will be the wild
blue yonder.

g

Quote:
Listers--We are close to flying our RV-6. On the airworthiness
certificate
application it requires the builder to state that "the powerplant
installation has undergone at least one hour of ground
operation at various speeds from
idle to full power. . . ." Yesterday during the first full
power static test
holding brakes and with the stick full aft the tail came up on
me. Because
I was approaching full power gradually (being nervous about
just this sort of
possibility) I was able to quickly close the throttle before
the prop hit
the ground.

Aircraft has an 0-360 and constant speed prop. Aircraft was
light with just
me aboard and a few gallons of fuel. Aircraft was recently
weighed and
empty CG was a few inches aft of forward limit.

I was able to complete the test by tying down the tail
securely. It is
still not a pleasant test to do.

Tonight checking the archives I see this characteristic has
been reported
previously (in 1999) for both the RV-6 and the RV-8 with
constant speed props.

Thought I would mention it again for anyone out there about to
do this test.
Be very careful.

LeRoy Johnston in Ohio.


--
__g__

==========================================================
Gerry Filby gerf(at)gerf.com
Tel: 415 203 9177
----------------------------------------------------------


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dan(at)rvproject.com
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PostPosted: Thu Aug 17, 2006 8:08 am    Post subject: Tail lifting during full power static test Reply with quote

I want to back what Kabong & Jack L. have said. Do we need to circulate that horrible Lancair engine run video again? (no) A lot of bad things can happen when an engine is running, especially if precautions haven't been taken. I've seen videos of RV first engine runs where the plane isn't even chocked, let alone tied down. Can't believe people actually do these things. To me, a not-fully-secured engine start is analogous to CFIT. Pilot error for sure, and it coulda been avoided.

For most of us, first engine run is at the end of a 2-10+ year journey. Why risk throwing ANY of that hard work away, or risk somebody getting hurt, or risk somebody else's hard work getting damaged? Don't answer that question. Just be safe.

FWIW, my RV-7 tail was tied down securely for my engine runs, and the tail still "hopped" when I did full power runs because my mains were chocked. There is no way to know beforehand whether or not it will do this. -7, or -8, or Rocket, or whatever, regardless of the powerplant. Just be safe.

Not that I want to make light of any of this, but see the attached photo to see what can happen if the plane is not secured well enough for that first engine run.

)_( Dan
RV-7 N714D
http://www.rvproject.com
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Jerry Grimmonpre'



Joined: 09 Jan 2006
Posts: 144
Location: Huntley, Illinois 60142

PostPosted: Thu Aug 17, 2006 11:07 am    Post subject: Tail lifting during full power static test Reply with quote

What is a safe method for tying down the tail on RV4, RV8. Please cover ALL details if known.
Many thanks ...
Jerry Grimmonpre'
RV4 flying
RV8A wires

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tcervin(at)valkyrie.net
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PostPosted: Thu Aug 17, 2006 6:15 pm    Post subject: Tail lifting during full power static test Reply with quote

Dan, At least the RV in the picture has the little wheel on the "Right End" so it won't nose over!
      Flame Suit On!! Tom in Ohio....RV6-A now at 40 Hours!!! DO NOT ARCHIVE
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Morocketman(at)aol.com
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PostPosted: Thu Aug 17, 2006 6:47 pm    Post subject: Tail lifting during full power static test Reply with quote

I had flown my Harmon Rocket II with IO-540 (260hp) for about half of the 25 hour flyoff time when I decided to start experimenting with what might happen when I was able to take a passenger along. I put a spare tire and wheel from my boat (estimated 20 lbs) in the baggage compartment. The airplane was sooooooooo much easier to maintain directional control on the ground, and just felt better all around. By the way, my tail weight is 43 lbs which is way more than John Harmon likes.

I very seldom fly solo now, but when I do, and when I think of it, I put a collapsible 5 gallon water jug in the pit. Not being a math whiz I think it must weigh about 40 lbs plus the tare weight of the jug. When I pickup a passenger, I just dump the water.

Not environmentally correct I suppose (creating oasis' is all the wrong places), but it really improves the airplanes manners.

I do exercise the prop at 1700 rpm, and wonder what the consequences of not doing so might be. My airplane doesn't seem to be prone to lifting the tail, but I am wary.

Be particularly careful with braking on cement or asphalt runways/taxiways or you can send her up on her nose. I had a scare on the first or second flight.

Les Featherston N206KT "Airgasm" has 281 hours, and flew just great today.
[quote][b]


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JhnstnIII(at)aol.com
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PostPosted: Thu Aug 17, 2006 7:30 pm    Post subject: Tail lifting during full power static test Reply with quote

"Did you're engine supplier not run your engine in the test
stand before delivering it to you ? It should be marked in the
log book, I think. I.E. do you really need to run it for a
whole hour ? Aerosport ran my engine for a total of 45 mins
before it was delivered - so apart from a short short "shake
down" run and some taxi tests - its next run will be the wild
blue yonder."


It was run at the factory, but now it is installed in a new airplane with new fuel lines, engine mount, exhaust system, etc. I would not have felt comfortable signing the form without running it in its current installation and knowing it would go to full power in takeoff/climb attitude.

Re the question of how to tie down the tail securely, all I can say is I used an airport tie down that looked solidly anchored with a rope in good condition. I tied it around the tail spring with three loops and two half hitches. I also added about 60 pounds to the baggage compartment.

I would not want anyone hanging on the fuselage as some have mentioned. That sounds like asking for trouble.

LeRoy Johnston in Ohio.


[quote][b]


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jsflyrv(at)verizon.net
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PostPosted: Thu Aug 17, 2006 9:12 pm    Post subject: Tail lifting during full power static test Reply with quote

Quote:
At least the RV in the picture has the little wheel on the "Right
End" so it won't nose over!
flame suit on DO NOT ARCHIVE

I will put my flame suit on first Smile

With my 180hp, sensenich fixed pitch prop I can run full throttle and
hold it with brakes and full up elevator. Having said that I can also
hold the brakes and lift the tail off of the ground and hold the plane
in level flight attitude and not be moving. It is very easy to control
the pitch attitude of the airplane with the elevator. NOW FOR THE
DISCLAIMER I do not advocate anyone here trying this, I learned to fly
in tailwheel airplanes back in the 1960s and have owned and flown many
tailwheel airplanes. 99% of all of my landings are wheel landings
so being on the two mains feels comfortable.

Jerry

do not archive


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Jeff Linebaugh



Joined: 11 Jan 2006
Posts: 48
Location: Collierville, TN

PostPosted: Sat Aug 19, 2006 7:04 am    Post subject: Tail lifting during full power static test Reply with quote



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Jeff Linebaugh
jefflinebaugh@earthlink.net
Collierville, TN
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