Today's Message Index:
----------------------
1. 09:42 AM - Re: TeamGrumman-List Digest: 1 Msgs - 05/26/05 (Brian Sandberg)
2. 01:19 PM - Cowl update? (Bruce Smith)
3. 04:54 PM - aircraft rigging (TeamGrumman@aol.com)
4. 04:55 PM - Re: Cowl update? (TeamGrumman@AOL.COM)
Message 1
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| Subject: | Re: TeamGrumman-List Digest: 1 Msgs - 05/26/05 |
7.50 BARRACUDA_HEADER_FP56 RBL: Blacklist bl.spamcop
[Blocked - see <http://www.spamcop.net/bl.shtml?64.4.51.220>]
--> TeamGrumman-List message posted by: "Brian Sandberg" <sandbag23@msn.com>
That reminds me, we rigged my plane at last annual and it was off too. One
of the problems was a mis-installed stop at the wingtip. The order of the
sandwich was corrected and the rig came in with a turnbuckle adjustment.
-Brian (still waiting on the paint shop, haven't flown a non-ferry since
January)
----- Original Message -----
From: "TeamGrumman-List Digest Server"
<teamgrumman-list-digest@matronics.com>
Subject: TeamGrumman-List Digest: 1 Msgs - 05/26/05
> *
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> Total Messages Posted Thu 05/26/05: 1
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> Today's Message Index:
> ----------------------
>
> 1. 11:03 AM - Aircraft rigging (TeamGrumman@AOL.COM)
>
>
> ________________________________ Message 1
_____________________________________
>
>
> Time: 11:03:30 AM PST US
> From: TeamGrumman@AOL.COM
> Subject: TeamGrumman-List: Aircraft rigging
>
> --> TeamGrumman-List message posted by: TeamGrumman@aol.com
>
> I had long suspected my Tiger was one of the planes with a misdrilled
aileron
> counter weight. The down travel on the left aileron barely cleared the
> bottom of the wing tip. So, I got the rigging tools and sure enough, the
down
>
> travel on the left aileron was only 3-4 degrees (it is supposed to be 7
1/2, +2
>
> 1/2, -0. Of course, this makes the up travel on the right aileron only
13
> degrees (15 +2 1/2, -0). It took some whittling on the sleeve on the 1/4
bolt
>
> and some filing on the stops, but I got the travel to agree left to right
to
> the specs. Both sides were out some. The left was the worst.
>
> Now, I'm going to start on the Flaps, and then onto the elevator and
rudder.
>
> I don't often get to work on my own plane. I'm waiting for parts so
....
>
> Gary
>
>
Message 2
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--> TeamGrumman-List message posted by: Bruce Smith <res02p3h@verizon.net>
Gary,
Any news on the Gen II cowl?
Bruce Smith
Message 3
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| Subject: | aircraft rigging |
--> TeamGrumman-List message posted by: TeamGrumman@aol.com
In a message dated 5/27/05 9:43:50 AM, sandbag23@msn.com writes:
> That reminds me, we rigged my plane at last annual and it was off too.=A0=20One
> of the problems was a mis-installed stop at the wingtip.=A0 The order of the
> sandwich was corrected and the rig came in with a turnbuckle adjustment.
>
>
I finished a 76 Tiger today. It's rigging was pretty close. On both
planes, the down limit on the elevator (17 degrees) could not be obtained because
the control column hits its stop before the limit on the back can get to 17
degrees. The tolerance is +/- 2 and getting 15 degrees was easy. Also, the
rigging tool for the elevator trim tab doesn't fit right on the elevator. =20It's
a guess at best. The ailerons on this Tiger could be adjusted to the max
limits, +17 and -10. Both sides were the same so whoever drilled this one=20got
it dead on.
Message 4
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| Subject: | Re: Cowl update? |
--> TeamGrumman-List message posted by: TeamGrumman@aol.com
waiting on process specs from the composite guy, then to the FAA. Cross
your fingers.
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