Unfortunately (or fortunately depending on your view) there is no
adjustment at the wing spar mounts. Two large bolts hold the spar to the
centre section and two smaller bolts hold the trailing spare. 
Any misalignment in the centre section must be considered serious and
could
occur where very heavy landing or in flight overload has occurred and poor
annual inspection has been conducted.  There is an AD for the rear spare
carry through of the centre section. Can't remember the number but it
basically beefs up the rear spare carry through to prevent distortion and
cracking.

I know this sounds silly but are the rear spar attach bolts fitted on the
suspect wing? Easy to check.


At 23:52 31/07/00 , you wrote:
>The real question here is: Is this problem a twist in the wings, or does
it start
>right at the mounting points for the wing?  If the angle is different
right at the
>base of the wing, that could indicate some serious previous damage that
wasn't
>repaired correctly.  On the other hand, not knowing these things, it is
possible
>that the aircraft was designed this way.  Lastly, is there room for
adjustment at
>the mounting points?  Could be the wing was installed incorrectly.  We've
all
>realized that work gets done on these 50 year old planes that doesn't get
recorded
>in the logs.
>
>Don't know the answer Larry
>
>jan zanutto wrote:
>
>> Bob,
>>
>> Is your wing a rag wing or metal.  Your wing would have to be twisted
>> pretty badly to get a differing incidence angle.
>>
>> If it is a rag wing- did whoever covered the wing last install the
screws
>> on the undercamber below the leading edge?  If you have one wing with
>> screws, and one wing without (an easy mistake to make) then you will
have
>> 2 different airfoils and they will look different if you look at them
>> from the side view.
>>
>> I have my fabric off now, and one thing I've seen about these wings is
>> that they are pretty stout and dont twist hardly at all. Someone would
>> have had to have done a really bad repair job and built a twist into
the
>> wing to get it to be off.
>>
>> Or, if it's a metal wing- maybe whoever skinned it had the wing
slightly
>> twisted when they installed the skin.
>>
>> jan z
>> Fresno, ca
>>
>> On Sun, 30 Jul 2000 22:13:13 -0700 Bob Ellis <[EMAIL PROTECTED]>
>> writes:
>> > Hello All,
>> >
>> >   After the crappy first flight of last weekend, I have spent much
>> > more
>> > hours than I expected on an aircraft I was assured was safe and
>> > airworthy.
>> > Still working on that issue, I'll let you all know how that
>> > situation pans
>> > out.
>> >   Here's my new question for you:
>> >
>> >   When looking closely, it is noticable that the angle of incidence
>> > is
>> > different between wings. I am sure that this is the reason for the
>> > gross
>> > rigging adjustments necessary to keep the plane flying straight.
>> > Does anyone
>> > else have anything similar to this situation?? It appears that the
>> > left wing
>> > has a flatter angle of attack than the right wing. My only real
>> > concern is
>> > that we now have two different stall speeds to contend with! Just
>> > curious
>> > what you all think.
>> >
>> >                                      Blue Skies,
>> >                                                 Bob Ellis
>> >
>>
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Regards

Brian Garrett
Melbourne
Viewbank 3084
Australia
(613) 9459 1779
Sonerai II VH-JGB
415C VH-???

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