A aviation & planes forum. AviationBanter

If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below.

Go Back   Home » AviationBanter forum » rec.aviation newsgroups » Owning
Site Map Home Register Authors List Search Today's Posts Mark Forums Read Web Partners

Citabria Rolls to the Left



 
 
Thread Tools Display Modes
  #1  
Old August 29th 03, 11:36 PM
John
external usenet poster
 
Posts: n/a
Default

Thanks, Shawn.
That was very helpful.

I'll let all you folks know when I find out what works.
I'll be talking to my favorite mechanic in the next couple of weeks.

-john

"ShawnD2112" wrote:

Before taking your airplane's wings apart, answer a couple of questions.
You want to solve the roll problem but not add any extra drag to the
airframe, which altering a wing's incidence angle may do.

Are you sure you're straight and level when you're checking for the roll? A
slight, nearly imperceptable climb without correcting rudder will induce
left roll as a secondary effect of the yaw.

Does your airplane have rudder trim? (Most do, I think). If so, it will
only trim for staight and level at one airspeed. Try flying straight and
level at several airspeeds with your feet flat on the floor and see what it
does to the roll. Start off in 5 knt increments and you'll be able to see
the roll become more or less pronounced. If you narrow it down to a cruise
speed that gives no roll, that's the speed your rudder trim is set for. If
you can live with that as your cruise speed, no worries. If you can't,
alter the trim tab to give more or less rudder and try a few more test
flights until you get it right.

If you can't find a no-roll airspeed, or you end up with a huge amount of
rudder trim, then you've probably got a rigging problem as the others here
have suggested. On my Pitts, I had the same problem, but the roll was to
the right. I went through the test procedure just like above and concluded
my wings weren't rigged properly. Because it's experimental, I was able to
re-rig the wings myself with some help from the UK's Pitts expert and she
flies like a dream now. In fact, rerigging the wings took so much drag out
of the airframe that I got an extra 5 knts in the cruise! When I bought her
she only had 34 hours on the airframe and had never been really aerobatted.
In the ensuing 50 hours I put on her, she started to settle and things
stretched and basically settled in, so things needed to be tightened and
readjusted here and there.

If you can rerig the wings yourself, the preference is to take incidence
angle OUT of a wing, rather than put it in. So, if it's rolling left, you
want to raise the trailing edge of the right wing, if you can. Lower angle
of incidence means less induced drag and the wings aren't fighting against
each other, wasting lift.

It's a bit simplistic, but that's the essence of how we solved my rolling
problem. Best of luck with yours!

Shawn
Pitts S-1D G-BKVP
"John Shoemaker" wrote in message
.. .
With my feet flat on the floor, ... not touching the rudder pedals, my
Citabria rolls to the left.

I have to hold right stick a bit for an entire trip.

I was told the the wing had to be "bent".
There are adjustments at the base of each strut on both sides of the
fuselage. I'd like to take in a turn or two and see what happens, but I
don't know which side to adjust.

-shoe



  #2  
Old August 30th 03, 06:40 AM
ShawnD2112
external usenet poster
 
Posts: n/a
Default

You bet, John. I hope it helps. Rereading my last posting, I'm reminded to
mention that when test flying to find a no-roll airspeed, you're basically
looking to make sure the ball is centered. That's the easiest way to tell
if the rudder trim/airspeed combination is right.

Let us know how you get on.

Shawn
"John" wrote in message
...
Thanks, Shawn.
That was very helpful.

I'll let all you folks know when I find out what works.
I'll be talking to my favorite mechanic in the next couple of weeks.

-john

"ShawnD2112" wrote:

Before taking your airplane's wings apart, answer a couple of questions.
You want to solve the roll problem but not add any extra drag to the
airframe, which altering a wing's incidence angle may do.

Are you sure you're straight and level when you're checking for the roll?

A
slight, nearly imperceptable climb without correcting rudder will induce
left roll as a secondary effect of the yaw.

Does your airplane have rudder trim? (Most do, I think). If so, it

will
only trim for staight and level at one airspeed. Try flying straight and
level at several airspeeds with your feet flat on the floor and see what

it
does to the roll. Start off in 5 knt increments and you'll be able to

see
the roll become more or less pronounced. If you narrow it down to a

cruise
speed that gives no roll, that's the speed your rudder trim is set for.

If
you can live with that as your cruise speed, no worries. If you can't,
alter the trim tab to give more or less rudder and try a few more test
flights until you get it right.

If you can't find a no-roll airspeed, or you end up with a huge amount of
rudder trim, then you've probably got a rigging problem as the others

here
have suggested. On my Pitts, I had the same problem, but the roll was to
the right. I went through the test procedure just like above and

concluded
my wings weren't rigged properly. Because it's experimental, I was able

to
re-rig the wings myself with some help from the UK's Pitts expert and she
flies like a dream now. In fact, rerigging the wings took so much drag

out
of the airframe that I got an extra 5 knts in the cruise! When I bought

her
she only had 34 hours on the airframe and had never been really

aerobatted.
In the ensuing 50 hours I put on her, she started to settle and things
stretched and basically settled in, so things needed to be tightened and
readjusted here and there.

If you can rerig the wings yourself, the preference is to take incidence
angle OUT of a wing, rather than put it in. So, if it's rolling left,

you
want to raise the trailing edge of the right wing, if you can. Lower

angle
of incidence means less induced drag and the wings aren't fighting

against
each other, wasting lift.

It's a bit simplistic, but that's the essence of how we solved my rolling
problem. Best of luck with yours!

Shawn
Pitts S-1D G-BKVP
"John Shoemaker" wrote in message
.. .
With my feet flat on the floor, ... not touching the rudder pedals, my
Citabria rolls to the left.

I have to hold right stick a bit for an entire trip.

I was told the the wing had to be "bent".
There are adjustments at the base of each strut on both sides of the
fuselage. I'd like to take in a turn or two and see what happens, but I
don't know which side to adjust.

-shoe





 




Thread Tools
Display Modes

Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

vB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Forum Jump

Similar Threads
Thread Thread Starter Forum Replies Last Post
American nazi pond scum, version two bushite kills bushite Naval Aviation 0 December 21st 04 10:46 PM
Hey! What fun!! Let's let them kill ourselves!!! [email protected] Naval Aviation 2 December 17th 04 09:45 PM
rec.aviation.aerobatics FAQ Dr. Guenther Eichhorn Aerobatics 0 October 1st 04 07:27 AM
rec.aviation.aerobatics FAQ Dr. Guenther Eichhorn Aerobatics 0 June 1st 04 08:27 AM
USAF = US Amphetamine Fools RT Military Aviation 104 September 25th 03 03:17 PM


All times are GMT +1. The time now is 03:58 AM.


Powered by vBulletin® Version 3.6.4
Copyright ©2000 - 2025, Jelsoft Enterprises Ltd.
Copyright ©2004-2025 AviationBanter.
The comments are property of their posters.