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Zenith-List Digest: 57 Msgs - 03/23/08

 
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tallow_98(at)yahoo.com
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PostPosted: Mon Mar 24, 2008 6:58 pm    Post subject: Zenith-List Digest: 57 Msgs - 03/23/08 Reply with quote

To ahontz

I have the kit not just the stinkin rudder.

Jimmy
--- Zenith-List Digest Server
<zenith-list(at)matronics.com> wrote:

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Quote:
Zenith-List Digest
Archive
---
Total Messages Posted Sun
03/23/08: 57


----------------------------------------------------------

Quote:


Today's Message Index:
----------------------

1. 01:27 AM - XL forward fuselage top thickness
(Dr. Andrew Elliott)
2. 04:07 AM - Re: CNC drilled pilot holes
(Larry H)
3. 04:29 AM - Re: Bending 40 thou (Jugle)
4. 04:56 AM - Used engine sources (James E.
Lanier)
5. 05:09 AM - Re: Used engine sources
(IFLYSMODEL(at)aol.com)
6. 06:23 AM - Re: Used engine sources (John
Short)
7. 06:36 AM - Re: Used engine sources (Clyde
Barcus)
8. 06:38 AM - Re: CNC drilled pilot holes
(Jaybannist(at)cs.com)
9. 06:49 AM - Re: XL forward fuselage top
thickness (Jaybannist(at)cs.com)
10. 07:43 AM - Re: XL forward fuselage top
thickness (LarryMcFarland)
11. 08:38 AM - Re: XL forward fuselage top
thickness (Tim Juhl)
12. 09:12 AM - Re: 701: Replace stab brackets?
(ricklach)
13. 09:49 AM - Re: Used engine sources (Gig
Giacona)
14. 10:02 AM - Ray Allen Position Sensor for
Flaps (Mark Colbeck)
15. 10:46 AM - Ray Allen Position Sensor for
Flaps (Craig Payne)
16. 11:12 AM - Re: Ray Allen Position Sensor for
Flaps (Jaybannist(at)cs.com)
17. 12:34 PM - 701 Flap control solution and
flying DVD (Les Goldner)
18. 12:34 PM - Non-hinged ailerons with
autopilot (Ronald Steele)
19. 12:57 PM - Re: XL forward fuselage top
thickness (Aerolitellc(at)aol.com)
20. 01:08 PM - trade 601xl fuselage and tail kit
(Jimmy Mathis)
21. 01:21 PM - Re: Non-hinged ailerons with
autopilot (Craig Payne)
22. 02:16 PM - Re: 701 Flap control solution and
flying DVD (kmccune)
23. 02:23 PM - Re: Used engine sources
(kmccune)
24. 02:55 PM - Re: 701 Flap control solution and
flying DVD (rroberts)
25. 03:19 PM - Re: Re: Used engine sources
(n801bh(at)netzero.com)
26. 03:39 PM - Re: Ray Allen Position Sensor for
Flaps (Terry Phillips)
27. 03:59 PM - Re: Re: 701 Flap control solution
and flying DVD (Les Goldner)
28. 03:59 PM - Re: Re: 701 Flap control solution
and flying DVD (Les Goldner)
29. 04:12 PM - Re: Re: 701 Flap control solution
and flying DVD (Craig Payne)
30. 04:53 PM - Re: Non-hinged ailerons with
autopilot (Bryan Martin)
31. 05:22 PM - Re: 701 Flap control solution and
flying DVD (rroberts)
32. 05:38 PM - Re: Non-hinged ailerons with
autopilot (Ronald Steele)
33. 05:56 PM - Re: 701 Flap control solution and
flying DVD (kmccune)
34. 06:15 PM - Re: trade 601xl fuselage and tail
kit (ashontz)
35. 06:16 PM - Re: Ray Allen Position Sensor for
Flaps (ashontz)
36. 06:17 PM - Re: Bending 40 thou (ashontz)
37. 06:20 PM - Re: Bending 40 thou (ashontz)
38. 06:26 PM - Re: Re: trade 601xl fuselage and
tail kit (Gary Boothe)
39. 06:27 PM - Re: Bending 40 thou (Jugle)
40. 06:27 PM - Re: Bending 40 thou (ashontz)
41. 06:31 PM - Re: 5th Bearing - What is the
Purpose? (ashontz)
42. 06:34 PM - Re: 5th Bearing - What is the
Purpose? (ashontz)
43. 06:47 PM - Re: Re: Bending 40 thou (Art
Olechowski)
44. 06:51 PM - Re: Used engine sources
(kmccune)
45. 07:19 PM - Re: 5th Bearing - What is the
Purpose? (kmccune)
46. 07:30 PM - Re: 5th Bearing - What is the
Purpose? (Ron Lendon)
47. 07:40 PM - Firewall spring back (lwinger)
48. 08:35 PM - Re: CNC drilled pilot holes
(JohnDRead(at)aol.com)
49. 08:56 PM - Re: CNC drilled pilot holes
(sundaypilot)
50. 09:08 PM - jRe: Non-hinged ailerons with
autopilot (T. Graziano)
51. 09:17 PM - NOTAM : FLORIDA in a New Plane
(ZodieRocket)
52. 09:40 PM - Re: NOTAM : FLORIDA in a New
Plane (Jay Maynard)
53. 09:52 PM - Re: Firewall spring back (Larry
Winger)
54. 09:56 PM - Re: NOTAM : FLORIDA in a New
Plane (Craig Payne)
55. 10:14 PM - Re: NOTAM : FLORIDA in a New
Plane (Craig Payne)
56. 10:40 PM - Re: Re: CNC drilled pilot holes
(Terry Phillips)
57. 11:02 PM - Re: Re: CNC drilled pilot holes
(Terry Phillips)



________________________________ Message 1
_____________________________________


Time: 01:27:50 AM PST US
From: "Dr. Andrew Elliott" <a.s.elliott(at)cox.net>
Subject: XL forward fuselage top
thickness

Looking for experience & opinions - I have made a
pattern and am ready
to cut the forward fuselage top skin (6C1-4). I
find that the while the
plans show it to be .020, some of the kits and
factory built aircraft
have it as .025.

I do plan to modify the sheet as many have, so that
the section between
the panel side angles, firewall and instrument panel
is removable via
lots of #8 screws, and the section where the canopy
rail goes is riveted
in place.

Estimating the area as 4 sq.ft., the weight
difference between the .020
skin and the .025 skin would be ~103.5 gms, which is
less than 4 ounces.

SO... Anyone have any comments about whether to use
the .020 or the .025
material, especially in terms of holding up in use
and maintenance?

Thanks,
Andy Elliott, Mesa, AZ
N601GE (reserved)
601XL/TD, Corvair, building...

________________________________ Message 2
_____________________________________

=== message truncated ===


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