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601HDS to LSA
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slandwcmitch(at)yahoo.com
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PostPosted: Mon Aug 17, 2009 10:43 am    Post subject: 601HDS to LSA Reply with quote

I need info on changing my HDS to LSA status. It seems that I need to change the wings to HD or ?
There has been prior discussions on this, but I can't find it. I've sent e-mail to Zenith, no reply yet. My wings are completed with tanks and lockers. Maybe a trade?? Thanks for any help.
Bill Mitchell   cont-0-200
[quote][b]


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psm(at)att.net
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PostPosted: Mon Aug 17, 2009 11:13 am    Post subject: 601HDS to LSA Reply with quote

Hi Bill,

I wonder why you might want to do this change.

If your plane is compatible with the LSA spec then you can operate it as a Sport Pilot without any paper work changes. If it is not then there is nothing you can do to make it work for that purpose.

I think the basic problem with an HDS for use as a LSA is the stall speed. Unfortunately, changing the wings to make it compliant doesn't help. I believe rule requires that any plane have always been consistent with that definition to qualify for use by a Sport Pilot.

Perhaps a trade of entire planes would work better for you.

Paul
XL awaiting engineering changes.


At 11:34 AM 8/17/2009, you wrote:
[quote]I need info on changing my HDS to LSA status. It seems that I need to change the wings to HD or ?
There has been prior discussions on this, but I can't find it. I've sent e-mail to Zenith, no reply yet. My wings are completed with tanks and lockers. Maybe a trade?? Thanks for any help.
Bill Mitchell cont-0-200


Quote:

[/b]
[b]


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grs-pms(at)comcast.net
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PostPosted: Mon Aug 17, 2009 11:13 am    Post subject: 601HDS to LSA Reply with quote

Bill:

Would the addition of vortex generators give you a sufficient decrease in stall speed to qualuify for LSA? Just a thought...

George Swinford CH601 HD project holding at 90%
[quote] ---


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larry(at)macsmachine.com
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PostPosted: Mon Aug 17, 2009 11:56 am    Post subject: 601HDS to LSA Reply with quote

Bill,
If your HDS flight envelope and stall speed agree with Light Sport
Aircraft, you have the plane you want. Some of the HDS 601s have a
higher stall speed than
required for LSA, so you need to visit your Aircraft's Operating
Handbook to find out what stall speed is for your particular plane.

Larry McFarland 601HDS at www.macsmachine.com (LSA compliant)

Bill Shirley Mitchell wrote:
Quote:
I need info on changing my HDS to LSA status. It seems that I need to
change the wings to HD or ?
There has been prior discussions on this, but I can't find it. I've
sent e-mail to Zenith, no reply yet. My wings are completed with tanks
and lockers. Maybe a trade?? Thanks for any help.
Bill Mitchell cont-0-200

*
*


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cherring



Joined: 19 May 2009
Posts: 5
Location: NC

PostPosted: Mon Aug 17, 2009 1:19 pm    Post subject: Re: 601HDS to LSA Reply with quote

If you have a plane that did not meet the LSA specs at the time it received its original airworthiness certificate, or any time since, that plane can never qualify as light-sport. It must meet the guidelines at the time of original AW cert and must have been "continuously operated" under those guidelines since that time. That means you cannot fly the plane outside the LSA criteria and then make modifications later which make the plane meet the LSA performance specs. Yes, the POH would be the place to look. If it shows the gross weight, stall & cruise speed limites within LSA, you're in luck. If not, there is nothing you can do to make it LSA.

I researched this pretty well because I have an HDS that I bought 90% complete and have almost finished. I plan to have it meet the LSA criteria by adding VG's before the inspection for the initial airworthiness certificate so it should meet the guideline for stall speed. Trying to follow the rules.


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naumuk(at)windstream.net
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PostPosted: Mon Aug 17, 2009 1:27 pm    Post subject: 601HDS to LSA Reply with quote

All-
To sum up the main points-
1. You can't add vortex generators to achieve LSA compliance because they aren't included in the original design, but are aftermarket.
2. If you haven't completed and previously registered your plane as Experimental, Owner Built, you can legally change in midstream to the HD wing configuration with the blessing of both the FAA and Zenith.
There are numerous posts on this subject in the archives.
Bill
[quote] ---


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cherring



Joined: 19 May 2009
Posts: 5
Location: NC

PostPosted: Mon Aug 17, 2009 1:48 pm    Post subject: Re: 601HDS to LSA Reply with quote

I think I am correct that adding VG's before the original AW Cert would help because it would (hopefully) allow the plane to meet the LSA stall speed limit. It isn't the VG's themselves that make it compliant or not, it is the stall speed, which is what it is as determined during initial flight testing. Agreed, adding them later does not allow a plane to meet LSA it is has been previously flown outside of the criteria.

Not sure what you mean by "aftermarket" - do you mean after the original A/W?
>>>>>>>
"1. You can't add vortex generators to achieve LSA compliance because they aren't included in the original design, but are aftermarket. "


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bryanmmartin



Joined: 10 Jan 2006
Posts: 1018

PostPosted: Mon Aug 17, 2009 2:43 pm    Post subject: 601HDS to LSA Reply with quote

If it's an E-AB, the original design doesn't mean a thing. The only
thing that matters is that the airplane meet the LSA limitations at
the time of it's original certification. For an E-AB, whatever it
takes to make the plane meet the requirements of LSA is fair game. The
entire airplane is "aftermarket". The only place the stall speed is
recorded is in the POH, which you will prove out during phase 1
testing. Make sure that your POH shows compliance with the rules.

In the E-AB airworthiness certification, there is no mention of LSA
limitations. You will certificate is as E-AB and then, if you
determine that it meets the limitations, you can fly it under LSA
rules. You will probably have no trouble flying any Zodiac under LSA
rules. The FAA would be extremely unlikely to call you on it. If you
tried it with an RV-6, it would be a different matter, it is well
known that most RVs far exceed the LSA limits.

On Aug 17, 2009, at 4:05 PM, Bill Naumuk wrote:

[quote] All-
To sum up the main points-
1. You can't add vortex generators to achieve LSA compliance
because they aren't included in the original design, but are
aftermarket.
2. If you haven't completed and previously registered your plane
as Experimental, Owner Built, you can legally change in midstream to
the HD wing configuration with the blessing of both the FAA and
Zenith.
There are numerous posts on this subject in the archives.
Bill
---


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PostPosted: Mon Aug 17, 2009 2:43 pm    Post subject: 601HDS to LSA Reply with quote

As I have said before, in this provision of the LSA rules, we have a real "Catch 22". You build an E-AB airplane, fully expecting it to be LSA compliant. Then in Phase 1, you discover that the stall speed is above allowable for LSA. You should be able to make corrections to bring it into compliance. Trouble is that you have had it certified as E-AB. That essentially establishes the physical configuration of the airplane. It has been flown outside the limitations for LSA. According to a strict interpretation of the regs, you can not now make the alterations to the airframe to bring it into compliance. In this case we are talking about adding VGs, but it would also apply to something like propeller pitch that drives the airplane faster that the LSA speed limitations. Is that bizarre and downright unfair? I think it is a serious glitch in the regs that really needs to be correct ed.

Jay Bannister
Do not archive





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bryanmmartin



Joined: 10 Jan 2006
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PostPosted: Mon Aug 17, 2009 2:49 pm    Post subject: 601HDS to LSA Reply with quote

I think Paul is just a little bit confused on the subject. I believe
you are correct, if VGs give you a low enough stall speed to meet the
LSA rules and every thing else falls within the limits, you're good to
go. It's your airplane, you built it, you write the POH.

On Aug 17, 2009, at 4:48 PM, cherring wrote:

Quote:

>

I think I am correct that adding VG's before the original AW Cert
would help because it would (hopefully) allow the plane to meet the
LSA stall speed limit. It isn't the VG's themselves that make it
compliant or not, it is the stall speed, which is what it is as
determined during initial flight testing. Agreed, adding them later
does not allow a plane to meet LSA it is has been previously flown
outside of the criteria.

Not sure what you mean by "aftermarket" - do you mean after the
original A/W?
>>>>>>>
"1. You can't add vortex generators to achieve LSA compliance
because they aren't included in the original design, but are
aftermarket. "


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N61BM, CH 601 XL,
RAM Subaru, Stratus redrive.
do not archive.


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bryanmmartin



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PostPosted: Mon Aug 17, 2009 2:56 pm    Post subject: 601HDS to LSA Reply with quote

As long as your final POH reflects the proper limitations, how is the
FAA going to know whether or not you had to make some minor
adjustments during phase 1 flight testing to meet them?

On Aug 17, 2009, at 5:37 PM, jaybannist(at)cs.com wrote:

Quote:
As I have said before, in this provision of the LSA rules, we have a
real "Catch 22". You build an E-AB airplane, fully expecting it to
be LSA compliant. Then in Phase 1, you discover that the stall
speed is above allowable for LSA. You should be able to make
corrections to bring it into compliance. Trouble is that you have
had it certified as E-AB. That essentially establishes the physical
configuration of the airplane. It has been flown outside the
limitations for LSA. According to a strict interpretation of the
regs, you can not now make the alterations to the airframe to bring
it into compliance. In this case we are talking about adding VGs,
but it would also apply to something like propeller pitch that
drives the airplane faster that the LSA speed limitations. Is that
bizarre and downright unfair? I think it is a serious glitch in the
regs that really needs to be correct ed.

Jay Bannister
Do not archive

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N61BM, CH 601 XL,
RAM Subaru, Stratus redrive.
do not archive.


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PostPosted: Mon Aug 17, 2009 3:33 pm    Post subject: 601HDS to LSA Reply with quote

Hi Jay,

I think you are taking this a little bit too literally.

For legal purposes, the only thing that matters is what appears on
paper. If your POH says your plane meets the details of the LSA
requirements then it does. You will not find an FAA inspector
chasing you around to see if your plane stalls at 45 KCAS or 46.

There is a special provision on the propeller pitch question called
maximum continuous power. If your plane goes a little too fast for
the LSA spec and you want it to meet the spec then all you need to do
is reduce the defined maximum continuous power for your
plane. Again, it is what is documented on paper that counts. If the
documents indicate it meets the required performance specs then it does.

The case of an existing HDS is a special one. If it has been
documented as having a stall speed too high for the LSA definition
then the show is over for that plane.

For any model plane, it doesn't matter what sort of airworthiness
certificate you have. It can be E-AB or E-LSA or any other thing you
can manage. If it meets the LSA definition it can be operated under
the Sport Pilot limits.

Paul
XL awaiting engineering changes
At 03:37 PM 8/17/2009, you wrote:
Quote:
As I have said before, in this provision of the LSA rules, we have a
real "Catch 22". You build an E-AB airplane, fully expecting it to
be LSA compliant. Then in Phase 1, you discover that the stall
speed is above allowable for LSA. You should be able to make
corrections to bring it into compliance. Trouble is that you have
had it certified as E-AB. That essentially establishes the physical
configuration of the airplane. It has been flown outside the
limitations for LSA. According to a strict interpretation of the
regs, you can not now make the alterations to the airframe to bring
it into compliance. In this case we are talking about adding VGs,
but it would also apply to something like propeller pitch that
drives the airplane faster that the LSA speed limitations. Is that
bizarre and downright unfair? I think it is a serious glitch in the
regs that really needs to be correct ed.

Jay Bannister


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PostPosted: Mon Aug 17, 2009 3:34 pm    Post subject: 601HDS to LSA Reply with quote

Bryan,

You are right, but remember, I said "STRICT interpretation of the regs". There are obviously ways around it; but I still think the regs need to change to keep everything on the up and up, whether the FAA knows about it or not.

Jay Bannister
Do not archive





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cherring



Joined: 19 May 2009
Posts: 5
Location: NC

PostPosted: Tue Aug 18, 2009 4:02 am    Post subject: Re: 601HDS to LSA Reply with quote

That's pretty much what the FAA told me. Just don't make a YouTube video of yourself in your "LSA" plane flying around at 150 MPH. They did notice when one guy did that.
>>>>>>>>>>>>>>>>>>>>>>>>>>>
You will not find an FAA inspector chasing you around to see if your plane stalls at 45 KCAS or 46.


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PostPosted: Tue Aug 18, 2009 6:05 am    Post subject: 601HDS to LSA Reply with quote

Why people beat themselves to death over this subject when you have organizations "out there" that have already defined aircraft that meet the definition of aircraft that a Sport Pilot can fly? They already list "Experimental Zenith 601" as acceptable. Not HD or HDS or XL...just Zenith 601. Agree with them, and FLY!

Dave

Flown in the Rockies, Desert SW, all the plains states west of the Mississippi and all in my lowly 601 HD!


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PostPosted: Tue Aug 18, 2009 6:33 am    Post subject: 601HDS to LSA Reply with quote

All-
Aftermarket was a poor choice of words; after the initial A/W inspection
is more accurate.
As I said, the question of VGs has come up many times before, there is
definitely a Catch 22 as the LSA regs apply to the HDS, and the whole mess
is as clear as mud.
Years ago I contacted EAA Technical as to whether you could build both
sets of wings and register the same airframe to HD/HDS performance
parameters and they said no. I also asked if I could add VGs to an HDS wing
to achieve LSA performance and they said no. I'm not sure whether I
specified the addition of VGs would be made before or after the Phase I
testing.
I suggest that the way to resolve this debate is to contact EAA
Technical and find out whether you're allowed to add VGs to an HDS wing
BEFORE Phase I testing, so I'm going to do just that and will post the
response.

Bill
---


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z601a(at)anemicaardvark.c
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PostPosted: Tue Aug 18, 2009 9:08 am    Post subject: 601HDS to LSA Reply with quote

On Monday 17 August 2009 17:37, jaybannist(at)cs.com wrote:
Quote:
As I have said before, in this provision of the LSA rules, we have a real
"Catch 22".? You build an E-AB airplane, fully expecting it to be LSA
compliant.? Then in Phase 1, you discover that the stall speed is above
allowable for LSA.? You should be able to make corrections to bring it into
compliance.? Trouble is that you have had it certified as E-AB.? That
essentially establishes the physical configuration of the airplane. It has
been flown outside the limitations for LSA.? According to a strict
interpretation of the regs, you can not now make the alterations to the
airframe to bring it into compliance.? In this case we are talking about
adding VGs, but it would also apply to something like propeller pitch that
drives the airplane faster that the LSA speed limitations.? Is that bizarre
and downright unfair?? I think it is a serious glitch in the regs that
really needs to be corrected.

I think it's easy to forget that Part 23, AC43, etc etc have evolved over many
years. A lot of refinment has occurred to reflect the problems in these
documents. The LSA regs are relatively recent, and have had little
opportunity for real world feedback. As this happens, I would expect
clarification to occur in the LSA regs.

Another factor is that, like a lot of other FAA regs, the onus is on the pilot
in command to insure that the aircraft he/she if flying meets FAA regs. That
seems, if anything, to be more true than usual with the LSA. It's the
responsibility of the PIC to know that the aircraft being flown meets LSA
requirements.

I have a little problem with the word "certificated" as used above. EAB
aircraft are not necessarily certificated in the usual sense of the word. A
type certificated aircraft has a published stall speed, etc, which
establishes it does or does not meet LSA requirements. The FAA does not allow
modification of these aircraft to meet LSA.

But there is no type certificate for EAB. Does this mean you can change it
later to meet LSA requirements? It seems fuzzy to me. Perhaps there will be
clarification later, although we may be better off without the
clarification. Smile
--
=============================================
Do not archive.
=============================================
Jim B Belcher
BS, MS Physics, Math, Computer Science
A&P/IA
Retired aerospace technical manager
=============================================


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PostPosted: Tue Aug 18, 2009 9:27 am    Post subject: 601HDS to LSA Reply with quote

Quote:
Jim,

My airplane has an airworthiness certificate. I guess it is a matter of
semantics; but to me, it is certified (not type certified).

Jay Bannister
Do not archive
I have a little problem with the word "certificated" as used above. EAB
aircraft are not necessarily certificated in the usual sense of the word. A
type certificated aircraft has a published stall speed, etc, which
establishes it does or does not meet LSA requirements. The FAA does not allow
modification of these aircraft to meet LSA.

But there is no type certificate for EAB. Does this mean you can change it
later to meet LSA requirements? It seems fuzzy to me. Perhaps there will be
clarification later, although we may be better off without the
clarification. Smile
--


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PostPosted: Tue Aug 18, 2009 9:41 am    Post subject: 601HDS to LSA Reply with quote

Hi Jim,

I agree with all your comments. Indeed, I want to take your thoughts
a few steps further.

The Sport Pilot and Light Sport Aircraft rules have been incredibly
successful. This is different from many other attempts to create new
pilots (e.g. Recreational Pilot) and aircraft (e.g.
ultralight). Some of the previous attempts have seen limited success
such as the part 103 ultralights, but even those didn't have a
significant impact on the National Airspace System or General
Aviation. The SP/LSA rules have had a huge impact on aircraft sales
and pilot licenses and will undoubtedly continue to do so. All you
need to see to be sure of this is the 100 new aircraft makes/models
available as factory new aircraft in the last few years.

After a few months flying an S-LSA I can tell you it gets even more
complicated to operate these aircraft after you solve the initial
go/nogo puzzle. For example, my Tecnam Echo Super has a ground
adjustable propeller. The question comes up of who has the authority
to adjust the pitch on this propeller. The answer is not at all
clear. Is this routine preventive maintenance or a minor or major
aircraft change? As a licensed pilot with no A&P or repairman
certificate I asked several knowledgeable A&Ps whether I could
legally change the pitch on this prop. I got a different answer from
each person I asked. This is not a listed preventive maintenance
activity, so it is not definitely OK for me to do this. It is also a
relatively minor thing to do and might be done before each flight to
tailor the propeller to the mission at hand. The most reasonable
answer I got was if it isn't written in the aircraft logs it didn't happen.

Given the unusual success of the new SP/LSA rules I am sure you are
right, Jim, that we will see many refinements in these
rules. Eventually, nearly all the questions will have clear
answers. For now, my advice to all is to be careful and worry a lot
more about safety and rational thinking than whether you might
exactly meet all the FAA rules or not.

Paul
XL awaiting engineering changes.
At 10:02 AM 8/18/2009, you wrote:
Quote:
I think it's easy to forget that Part 23, AC43, etc etc have evolved
over many
years. A lot of refinment has occurred to reflect the problems in these
documents. The LSA regs are relatively recent, and have had little
opportunity for real world feedback. As this happens, I would expect
clarification to occur in the LSA regs.

Another factor is that, like a lot of other FAA regs, the onus is on
the pilot
in command to insure that the aircraft he/she if flying meets FAA regs. That
seems, if anything, to be more true than usual with the LSA. It's the
responsibility of the PIC to know that the aircraft being flown meets LSA
requirements.


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PostPosted: Tue Aug 18, 2009 12:20 pm    Post subject: 601HDS to LSA Reply with quote

On Tuesday 18 August 2009 12:25, jaybannist(at)cs.com wrote:
Quote:
Jim,

My airplane has an airworthiness certificate. I guess it is a matter of
semantics; but to me, it is certified (not type certified).

My understanding of a distinction here is that the airworthiness certificate
doesn't say anything about the performance. It says the plane appears to be
constructed properly.

A type certificate goes further in that it says the plane was constructed in
accordance with the specification associated with the type certificate, and
will perform as described there. That ties it to speeds, etc etc.

Yes, they are both certificates, but their meaning is distinct. Usually, when
someone talks about a certificated aircraft, I think it is taken to mean a
type certificated aircraft.

In the LSA world, where legality is tied to performance, I don't think the
airworthiness certificate defines it as an LSA. That appears to become
dependent on the pilot. If the pilot knows that during testing, the aircraft
did not meet LSA requirements, he/she is responsible for this.

Of course, if the aircraft has a type certificate, then the performance
defined for the type certificate would indicate if the plane qualifies as an
LSA or not.

.and with all this, I'm going to get off my soap box, and hide back in my
shop, before someone starts throwing tomatoes...

--
=============================================
Do not archive.
=============================================
Jim B Belcher
BS, MS Physics, Math, Computer Science
A&P/IA
Retired aerospace technical manager
=============================================


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