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lwinger
Joined: 21 Jun 2006 Posts: 229 Location: Tustin, CA
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Posted: Tue Jul 31, 2007 2:29 pm Post subject: Control cables for 601XL |
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The plans (6-B-23) say 1/8" 7x19 Galvanized control cables. The folks in the shop at Zenith say they are using stainless steel.
Stainless steel makes sense to me as well. Any reason not to use it?
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_________________ Larry Winger
Tustin, CA
Plans building 601XL/650 with Corvair
Installing fuel system
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amyvega2005(at)earthlink. Guest
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Posted: Tue Jul 31, 2007 5:19 pm Post subject: Control cables for 601XL |
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use the 7x19 aviation grade. they are grease impregnated.
Juan
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lwinger
Joined: 21 Jun 2006 Posts: 229 Location: Tustin, CA
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Posted: Tue Jul 31, 2007 8:32 pm Post subject: Control cables for 601XL |
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I'm planning to purchase my cable from Aircraft Spruce, so I'm making an assumption that it is aviation grade as you described. If so, any thoughts on stainless steel in place of the specified galvanized?
Larry Winger
601XL/Corvair
Tustin, CA
On 7/31/07, Juan Vega <amyvega2005(at)earthlink.net (amyvega2005(at)earthlink.net)> wrote: [quote]--> Zenith-List message posted by: Juan Vega <amyvega2005(at)earthlink.net (amyvega2005(at)earthlink.net)>
use the 7x19 aviation grade. they are grease impregnated.
Juan
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_________________ Larry Winger
Tustin, CA
Plans building 601XL/650 with Corvair
Installing fuel system
www.mykitlog.com/lwinger |
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amyvega2005(at)earthlink. Guest
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Posted: Wed Aug 01, 2007 5:36 am Post subject: Control cables for 601XL |
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check with zenith but I beleieve I used GLAV 7x19 with 2000Lb strength versus SS7x19 with 1750 lbs strength.
Jaun
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lwinger
Joined: 21 Jun 2006 Posts: 229 Location: Tustin, CA
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Posted: Wed Aug 01, 2007 6:01 am Post subject: Control cables for 601XL |
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Juan,
If you look at my first post, you'll see that I did call Zenith and that stimulated my question to the list. The person in the shop was almost positive they were using stainless steel. Obviously, I didn't get my answer from the designer or an engineer. Maybe that is my next step (or I can just use galvanized to be safe).
Thanks,
Larry Winger
On 8/1/07, Juan Vega <amyvega2005(at)earthlink.net (amyvega2005(at)earthlink.net)> wrote: [quote]--> Zenith-List message posted by: Juan Vega <amyvega2005(at)earthlink.net (amyvega2005(at)earthlink.net)>
check with zenith but I beleieve I used GLAV 7x19 with 2000Lb strength versus SS7x19 with 1750 lbs strength.
Jaun
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_________________ Larry Winger
Tustin, CA
Plans building 601XL/650 with Corvair
Installing fuel system
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wjones(at)brazoriainet.co Guest
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Posted: Wed Aug 01, 2007 7:02 am Post subject: Control cables for 601XL |
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Larry from my standpoint ,either one is good and both are approved for certified aircraft . With any type of care they will outlast the airframe .My Tripacer is 48 years old ,I live 12 miles inland from the gulf of Mexico (very corrosive) and with little care my galvanized cables are still looking good..If you go the S.S. route use the correct nicopress fitting ,do not use the copper .
Wade Jones South Texas
601XL plans building
Cont. 0200
[quote] ---
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paulrod36(at)msn.com Guest
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Posted: Thu Aug 02, 2007 6:46 am Post subject: Control cables for 601XL |
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<?xml:namespace prefix="v" /><?xml:namespace prefix="o" /><![endif]--> Sort of a side issue----- While I wouldn't advocate using string or safety wire for control cables, it does seem a bit of overkill to use a cable stronger than the max gross weight of the aircraft. It's not possible, even under high adrenalin situations, to exert anywhere near breaking strength of the cable, particularly sitting in the cockpit. If anything, you'd rip the control surface apart first, assuming you could maintain that much air load on the part. Same goes for turnbuckles. Do we really need 900 pound breaking-strength turnbuckles on an elevator we could put, at most, 200 pounds of backstick pull?
Paul Rodriguez
601XL/Corvair
Canopy getting close to done
[quote] ---
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david_a_g_johnson(at)btin Guest
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Posted: Thu Aug 02, 2007 7:22 am Post subject: Control cables for 601XL |
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remember the leverage available, I reckon that the elevator has a leverage of about 2.5 to 1, so a pull of 200lbs will give a load of around 500lbs on the cable. The leverage on the rudder pedals is less, but you can exert a LOT more pressure with your feet! I weigh about 200lbs, when I go upstairs I am pressing with 200lbs with each foot in turn, without much effort - i would be able to push a lot harder than that with the right incentive.
Dave Johnson
601XL
do not archive
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paulrod36(at)msn.com Guest
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Posted: Thu Aug 02, 2007 8:39 am Post subject: Control cables for 601XL |
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<?xml:namespace prefix="v" /><?xml:namespace prefix="o" /><![endif]--> More or less true, but consider a: how fast must you go to exert an over 200 pound air load on something as small as a rudder? b: Even if you were going that fast, you'd certainly bend the rudder or tear off the horn before failing the cable. It's something like fishing for trout with a tow truck and a log chain
Paul R
[quote] ---
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bryanmmartin
Joined: 10 Jan 2006 Posts: 1018
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Posted: Thu Aug 02, 2007 11:00 am Post subject: Control cables for 601XL |
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The overall breaking strength of the cable is not the only criteria
involved. You want to have a generous safety factor built in and there
is the matter of abrasion resistance. If the cable for some reason
starts wearing against something to the extent that some of the wires in
the cable are damaged, you don't want the cable to fail catastrophically
before the damage can be discovered during an inspection on the ground.
That's why there is a minimum size required for control cables on
certificated aircraft.
paulrod36(at)msn.com wrote:
Quote: | Sort of a side issue----- While I wouldn't advocate using string or
safety wire for control cables, it does seem a bit of overkill to use a
cable stronger than the max gross weight of the aircraft. It's not
possible, even under high adrenalin situations, to exert anywhere near
breaking strength of the cable, particularly sitting in the cockpit. If
anything, you'd rip the control surface apart first, assuming you could
maintain that much air load on the part. Same goes for turnbuckles. Do
we really need 900 pound breaking-strength turnbuckles on an elevator we
could put, at most, 200 pounds of backstick pull?
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Bryan Martin
Zenith 601XL N61BM
Ram Subaru, Stratus redrive
Do Not Archive
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Bryan Martin
N61BM, CH 601 XL, Stratus Subaru.
do not archive. |
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dredmoody(at)cox.net Guest
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Posted: Thu Aug 02, 2007 11:31 am Post subject: Control cables for 601XL |
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I'm not an A&P or an authority of any note but I have been told that these cables are overkill-sized in order to minimize their stretching and springing back and forth like a bungee. The concept as told to me is to have something (A) strong enough to be very unlikley to fail under tension loads, (B) heavy enough to withstand surface wear (as you mentioned), and also (C) dimensionally stable in the longitudinal axis to make tension adjustment feasible.
Personally, I just trust that CH chose and or approved the choice of cable and apparently his planes aren't falling out of the sky due to cable failure. I'm reluctant to second guess the issue beyond that point. Just my two cents worth (and probably over-priced at that).
Dred
---- Bryan Martin <bryanmmartin(at)comcast.net> wrote:
Quote: |
The overall breaking strength of the cable is not the only criteria
involved. You want to have a generous safety factor built in and there
is the matter of abrasion resistance. If the cable for some reason
starts wearing against something to the extent that some of the wires in
the cable are damaged, you don't want the cable to fail catastrophically
before the damage can be discovered during an inspection on the ground.
That's why there is a minimum size required for control cables on
certificated aircraft.
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amyvega2005(at)earthlink. Guest
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Posted: Thu Aug 02, 2007 2:59 pm Post subject: Control cables for 601XL |
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sounds good, good luck.
Juan
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planecrazydld(at)yahoo.co Guest
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Posted: Fri Aug 03, 2007 10:38 am Post subject: Control cables for 601XL |
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Hi Paul;
One of the issues involved with sizing control cables is strain (stretch) before reaching breaking loads. You want the control system to be as inflexible as possible because flutter is inherent in any less than optimally stiff system.
Sometime read the account of what happened when the folks back at Wright Patterson labs in Dayton got hold of their first Zero during WWII.
paulrod36(at)msn.com wrote:
[quote] <?xml:namespace prefix="v" /><?xml:namespace prefix="o" /><![endif]--> Sort of a side issue----- While I wouldn't advocate using string or safety wire for control cables, it does seem a bit of overkill to use a cable stronger than the max gross weight of the aircraft. It's not possible, even under high adrenalin situations, to exert anywhere near breaking strength of the cable, particularly sitting in the cockpit. If anything, you'd rip the control surface apart first, assuming you could maintain that much air load on the part. Same goes for turnbuckles. Do we really need 900 pound breaking-strength turnbuckles on an elevator we could put, at most, 200 pounds of backstick pull?
Paul Rodriguez
601XL/Corvair
Canopy getting close to done
[quote] ---
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