KR> KR2S LSA

2013-12-17 Thread Tony King
It's one thing to make a KR meet the LSA weight and performance specs.  As
I understand it, it's quite another to make it an actual LSA since that
requires the manufacturer to certify (and demonstrate I believe) that it
meets certain engineering standards - usually ASTM.

Is this thread about the former or the latter?  If the former, why would
you want to limit the performance?

Cheers,

Tony


KR> KR2S LSA

2013-12-16 Thread Dj Merrill
On 12/16/2013 6:57 PM, Lawrence Bell wrote:
> If you claim it meets LSA requirements you can certify it LSA.

Technically speaking you cannot "certify" it as an LSA.  You can, 
however, build it as an EAB (Experimental Amateur Built) that meets LSA 
specs, and fly it as a Sport Pilot.

To literally certify an airplane as an actual LSA, you need to go 
through the ATSM Consensus Standards process, which makes no sense for 
any of us to do unless you are going to start manufacturing aircraft to 
sell.

-Dj

-- 
Dj Merrill - N1JOV - VP EAA Chapter 87
Sportsman 2+2 Builder #7118 N421DJ - http://deej.net/sportsman/
Glastar Flyer N866RH - http://deej.net/glastar/



KR> KR2S LSA

2013-12-16 Thread Dan Heath
I hate to jump in on this because it has been discussed at length in the
past.  I just went thru this with another party so I would be able to
understand the significance of this being an EAB certified aircraft that
could be flown under the LSA rules.  As I understand it, you can build an
aircraft and demonstrate that it meets the LSA requirements as previously
stated.  How you fly it is your business.  Let's say that you set the max
gross weight at 1400 # and then get it EAB certified as that.  You can never
change that.  However, if you certify the aircraft at the Max gross weight
of an aircraft the meets the LSA requirements, then it can be flown LSA as
long as it meets the other requirements.  And if you are flying it as LSA,
at over the max weight, you have a problem.  You do not certify the aircraft
as an LSA aircraft, you certify it as Experimental Amateur Built ( EAB ),
and it happens to meet the LSA requirements.

The only way I could ever think that the KR could meet those requirements
would be that it was very light and had a high lift wing.  The Diehl wing
might do it, but it might not.  What if you build your plane planning on and
depending on being able to fly it under the LSA rules, and then it is not
capable of performance under the Rules.  Watcha gonna do?  

My personal opinion is that if you need LSA, build a plane that has been
proven to be able to meet those requirements.

See N64KR at http://KRBuilder.org - Then click on the pics?

Peoples Choice at 2013 - KR Gathering in Mt. Vernon, Il ? MVN 
Best KR at 2013 - KR Gathering in Mt. Vernon, Il ? MVN 
Best Interior at 2013 - KR Gathering in Mt. Vernon, Il ? MVN 
Best Paint at 2013 - KR Gathering in Mt. Vernon, Il ? MVN 
Best Firwwall Forward at 2013 - KR Gathering in Mt. Vernon, Il ? MVN 

Daniel R. Heath -?Lexington, SC







KR> KR2S LSA

2013-12-16 Thread Kenneth B. Jones
Just a slight correction to the numbers.  The LSA speed and weight numbers are:
Maximum gross takeoff weight?1,320 lbs, or 1,430 lbs for seaplanes.
Maximum stall speed?51 mph (45 knots) CAS
Maximum speed in level flight with maximum continuous power (Vh)?138 mph (120 
knots) CAS
There are other restrictions such as fixed pitch fixed gear (for land planes), 
etc., too.  

Ken Jones
KHAO


On Dec 16, 2013, at 4:39 PM, Lawrence Bell wrote:

> William, the LSA requirements have to be met when you register. Most KR
> builders want performance which will not be LSA. If you look at the
> performance chart of KR-2's some meet the requirement but most don't. Flaps
> do not help because the stall requirement is without flaps, as in what if
> they don't work. The max speed is 152 knots and stall is under 50 without
> augmentation. I would assume the right prop would limit your speed but you
> need low weight and high wing area to get stall speed.
>Larry Bell
> 
> 



KR> KR2S LSA

2013-12-16 Thread Larry Flesner

>The max speed is 152 knots and stall is under 50 without
>augmentation.
> Larry Bell
>


That seems a bit high.  I recall it being more like 120 knots (138 
mph) and 48 knots (52 mph) on the low end.

Larry Flesner






KR> KR2S LSA

2013-12-16 Thread Lawrence Bell
Tony, the manufacturer is you. The KR-2 is not a kit and does not have kit
certification. Each build is different and stands on its own when you
certify it. If you claim it meets LSA requirements you can certify it LSA.
The plans call for a retract gear making it ineligible but most of us have
fixed gear. As I mentioned to William, if you follow a build that resulted
in stats that meet LSA as indicated on the KR-2 performance chart I think
you could be comfortable claiming it will meet the specs. After you certify
it regular you can't change to LSA.
Larry Bell


On Mon, Dec 16, 2013 at 3:30 PM, Tony King  wrote:

> It's one thing to make a KR meet the LSA weight and performance specs.  As
> I understand it, it's quite another to make it an actual LSA since that
> requires the manufacturer to certify (and demonstrate I believe) that it
> meets certain engineering standards - usually ASTM.
>
> Is this thread about the former or the latter?  If the former, why would
> you want to limit the performance?
>
> Cheers,
>
> Tony
> ___
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>


KR> KR2S LSA

2013-12-16 Thread Lawrence Bell
You're absolutely right, Ken. My bad for taking the figures out of my head.
Larry


On Mon, Dec 16, 2013 at 2:30 PM, Kenneth B. Jones wrote:

> Just a slight correction to the numbers.  The LSA speed and weight numbers
> are:
> Maximum gross takeoff weight?1,320 lbs, or 1,430 lbs for seaplanes.
> Maximum stall speed?51 mph (45 knots) CAS
> Maximum speed in level flight with maximum continuous power (Vh)?138 mph
> (120 knots) CAS
> There are other restrictions such as fixed pitch fixed gear (for land
> planes), etc., too.
>
> Ken Jones
> KHAO
>
>
> On Dec 16, 2013, at 4:39 PM, Lawrence Bell wrote:
>
> > William, the LSA requirements have to be met when you register. Most KR
> > builders want performance which will not be LSA. If you look at the
> > performance chart of KR-2's some meet the requirement but most don't.
> Flaps
> > do not help because the stall requirement is without flaps, as in what if
> > they don't work. The max speed is 152 knots and stall is under 50 without
> > augmentation. I would assume the right prop would limit your speed but
> you
> > need low weight and high wing area to get stall speed.
> >Larry Bell
> >
> >
>
> ___
> Search the KRnet Archives at http://tugantek.com/archmailv2-kr/search.
> To UNsubscribe from KRnet, send a message to KRnet-leave at list.krnet.org
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>


KR> KR2S LSA

2013-12-16 Thread Lawrence Bell
William, the LSA requirements have to be met when you register. Most KR
builders want performance which will not be LSA. If you look at the
performance chart of KR-2's some meet the requirement but most don't. Flaps
do not help because the stall requirement is without flaps, as in what if
they don't work. The max speed is 152 knots and stall is under 50 without
augmentation. I would assume the right prop would limit your speed but you
need low weight and high wing area to get stall speed.
Larry Bell


On Mon, Dec 16, 2013 at 9:50 AM, William Shambrook
wrote:

> I have a set of plans dated June 1995 with the KR2S updates. Have there
> been a number of updates and if so how would I get them?  I note that there
> is a company selling KR2S plan sets.  Would it be better to just purchase a
> new set?
>
> I have noted that the question has come up whether with some modification
> the KR2S could meet the stall and cruise speed requirements to meet the
> sport pilot criteria. Is this doable or would it require too many
> modifications? In reading the krnet entries it appears that by including
> flaps you can get the stall and landing speed down somewhat but is it
> adequate?
>
> In looking at the KRSuper2 site it claims, I believe, that the aircraft can
> be built to meet the sport pilot requirements.  Do you know if that is the
> case?
>
> Thanks
> ___
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>


KR> KR2S LSA

2013-12-16 Thread Craig Williams
I believe it is possible.? The trade off for me will be useful load and cruise 
speed.? My modifications include: 120 HP, new center section spar to increase 
span to 26 feet and larger tail area.?? Obviously, it is hopeful thinking until 
flight testing proves me out or calls me liar.

Craig
Www.kr2seafury.com

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