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Tri-Q main gear for sale?
My poor, bent landing gear.I'm attempting to bend them back into shape under heat and pressure. There is a chance we may not succeed, in which case I'll be in need of a replacement gear. Any help
My poor, bent landing gear.I'm attempting to bend them back into shape under heat and pressure. There is a chance we may not succeed, in which case I'll be in need of a replacement gear. Any help
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By
Patrick Rameau
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#38238
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UV problem
I got the solution. SPF 30 sunscreen. Problem solved.Mike Q200Sent from my Windows Phone
I got the solution. SPF 30 sunscreen. Problem solved.Mike Q200Sent from my Windows Phone
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By
Mike Dwyer
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#38237
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Re: UV damage oops
That figure included 4 layers of infused 6oz fiberglass. I will need to
get the actual number from Cal Poly Pomona.
--
Larry Severson
18242 Peters Ct
Fountain Valley, CA 92708
(714) 968-9852
That figure included 4 layers of infused 6oz fiberglass. I will need to
get the actual number from Cal Poly Pomona.
--
Larry Severson
18242 Peters Ct
Fountain Valley, CA 92708
(714) 968-9852
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By
Larry Severson
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#38236
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Re: UV damage
Larry, you do realize that 0.2 inches, or 0.1969 to be precise, is nearly
1/4"??? (1/5th to be exact). Take one inch and divide it into five equal
parts- that's 1/5th of an inch.
I've NEVER seen that
Larry, you do realize that 0.2 inches, or 0.1969 to be precise, is nearly
1/4"??? (1/5th to be exact). Take one inch and divide it into five equal
parts- that's 1/5th of an inch.
I've NEVER seen that
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By
Pat Panzera <panzera@...>
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#38235
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Re: August Fly In LVK
Jim,
I have not scheduled a FAA inspection but plan to call as soon as I get
back (8-10-11) I have a couple more documents to produce and the package is
complete.
So weather permitting and if
Jim,
I have not scheduled a FAA inspection but plan to call as soon as I get
back (8-10-11) I have a couple more documents to produce and the package is
complete.
So weather permitting and if
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By
One Sky Dog
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#38234
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Re: UV damage
Cool Larry,
So care to elaborate on the "Tests that I have seen show that it takes
about 5mm of UV protecting paint over the whole surface." test data who,
what, where?
I see that you have a
Cool Larry,
So care to elaborate on the "Tests that I have seen show that it takes
about 5mm of UV protecting paint over the whole surface." test data who,
what, where?
I see that you have a
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By
One Sky Dog
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#38233
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Re: Its Changed! - New Fuel Filters
Good point Rick, it does get one hell of a lot colder in Canada than California or Florida and a frozen fuel filter, full of water, wouldn't work so well. Most of the planes in Canada are Aluminum and
Good point Rick, it does get one hell of a lot colder in Canada than California or Florida and a frozen fuel filter, full of water, wouldn't work so well. Most of the planes in Canada are Aluminum and
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By
Jim Patillo
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#38232
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Re: Slow Postings
Paul, I've had these delays in the past but never more than ~ 12 hours.
I've also noticed rare postings I made that showed on the Web-site but
never came to me. Recently Yahoo groups seem quite
Paul, I've had these delays in the past but never more than ~ 12 hours.
I've also noticed rare postings I made that showed on the Web-site but
never came to me. Recently Yahoo groups seem quite
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By
Mike Perry
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#38231
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Re: UV damage
I agree with Charley (One Sky Dog). This is an enormous amount of paint
AND weight. Is there a decimal point missing? Otherwise, I don't think
this is practical for aircraft construction.
Mike
I agree with Charley (One Sky Dog). This is an enormous amount of paint
AND weight. Is there a decimal point missing? Otherwise, I don't think
this is practical for aircraft construction.
Mike
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By
Mike Perry
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#38230
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Re: UV damage
My thoughts exactly.
How many cans of paint is that, exactly? If 2 gallons is needed to just cover the primer, then....figure like 8 at the least?
Then weight =(% dry solids)*(weight of 1 gal
My thoughts exactly.
How many cans of paint is that, exactly? If 2 gallons is needed to just cover the primer, then....figure like 8 at the least?
Then weight =(% dry solids)*(weight of 1 gal
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By
quickieaircraft
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#38228
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Angle of Incidence
Hi All,
I have a Tri Q and am getting dangerously close to being at the point of ataching the canard. Mine is a LS1 built flat (no anhedral) and I have been trying to pay close attention to the
Hi All,
I have a Tri Q and am getting dangerously close to being at the point of ataching the canard. Mine is a LS1 built flat (no anhedral) and I have been trying to pay close attention to the
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By
ericapplegate@rocketmail.com
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#38227
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Re: UV damage
Mike Dwyer wrote;
"As for your paint theory try a different thought. No idea if this is right or not. I understand fiberglass resins outgass for their entire life. If you seal over it with a super
Mike Dwyer wrote;
"As for your paint theory try a different thought. No idea if this is right or not. I understand fiberglass resins outgass for their entire life. If you seal over it with a super
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By
Richard Thomson
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#38226
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Re: UV damage
[0.1969 to be precise) Passed lab testing with top grade test equipment
( by a technical college) exposing painted epoxy part to heat, rain, and
UV equivalent to 10 years outdoors on a Florida ramp.
[0.1969 to be precise) Passed lab testing with top grade test equipment
( by a technical college) exposing painted epoxy part to heat, rain, and
UV equivalent to 10 years outdoors on a Florida ramp.
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By
Larry Severson
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#38225
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Re: UV damage
5mm (~.200 inches) are you lucid?
One Sky Dog
5mm (~.200 inches) are you lucid?
One Sky Dog
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By
One Sky Dog
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#38224
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Re: Wing Shear Web Cut
Turns out Terry called me and answered my questions.
I made the cut w/o any problems tonight.
Thanks Terry!
Joe Galletti
Turns out Terry called me and answered my questions.
I made the cut w/o any problems tonight.
Thanks Terry!
Joe Galletti
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By
Frontier
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#38222
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Re: UV damage
Hi Richard,
For the standard Q's (not Tri-Q)... If I remember my calculations of 20 years ago, when a wing develops 1G of lift it is doing so with the lift distribution over the entire wing surface.
Hi Richard,
For the standard Q's (not Tri-Q)... If I remember my calculations of 20 years ago, when a wing develops 1G of lift it is doing so with the lift distribution over the entire wing surface.
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By
Mike Dwyer
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#38220
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Re: UV damage
Hi Mike.
Can you explain your statement
I calculated that the Q200 canard has the equivalent of 4G on it when loaded to gross on the ground, plus it is supported by the wing tips. ?
It's a few
Hi Mike.
Can you explain your statement
I calculated that the Q200 canard has the equivalent of 4G on it when loaded to gross on the ground, plus it is supported by the wing tips. ?
It's a few
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By
Richard Thomson
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#38219
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Cool aviation web sites
Ran across these web sites and thought you may find them interesting.
E6B Online http://www.csgnetwork.com/e6bcalc.html
Free Charts http://skyvector.com/
TFR map
Ran across these web sites and thought you may find them interesting.
E6B Online http://www.csgnetwork.com/e6bcalc.html
Free Charts http://skyvector.com/
TFR map
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By
Mike Dwyer
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#38218
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Re: Its Changed! - New Fuel Filters
I wonder if the paper filter issue in Canada is related to water freezing in the filter.
I wonder if the paper filter issue in Canada is related to water freezing in the filter.
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By
Rick Hole
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#38229
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Re: Its Changed! - New Fuel Filters
Hi Jim,
I use these from Aircraft Spruce p/n 05-01030 http://www.aircraftspruce.com/catalog/appages/fuelfilter.php
They only come in 1/4 barb ends though. So if you need larger barb ends, I've
Hi Jim,
I use these from Aircraft Spruce p/n 05-01030 http://www.aircraftspruce.com/catalog/appages/fuelfilter.php
They only come in 1/4 barb ends though. So if you need larger barb ends, I've
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By
Rene Robertson <q2robertson@...>
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#38217
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