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[rebel-builders] What I learned this week! - LSA specs ...

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Bob Patterson

[rebel-builders] What I learned this week! - LSA specs ...

Post by Bob Patterson » Sun Feb 19, 2012 5:16 pm

Hi Ron !

I did NOT mean to imply that there WAS a minimum empty weight
for US Experimental homebuilts - I don't know. In Canada, there IS !
The Canadian max empty weight is arrived at by some bizzare calculation
involving your hat size, wing area, & engine horespower, if I recall ...

Certainly, as you say, there is nothing that I know of preventing a
US Experimental aircraft being registered at 1,320 gross with 1,000 lb
empty weight. PROVIDED it is flown with a PPL or higher !

In any case, my understanding is that, in order to fly ANY aircraft
with a Sport Pilot licence, that aircraft must MEET <ALL> REQUIREMENTS
for LSA - ie max. empty weight, as well as max gross weight, as well as
max cruise & stall speeds, and fixed/ground adjustable pitch prop, etc..
That is only MY understanding, although it seems to be shared by many.

I'm open to correction ! ;-)

--
......bobp
bobp@prosumers.ca
http://www.prosumers.ca/Ramble09

http://bpatterson.qhealthbeauty.com
http://apatterson2.qhealthzone.com
http://apatterson2.ordermygift.com

-------------------------------orig.-------------------------
On Monday 09 March 2009 06:08, Ron Shannon wrote:
[ALERT: Another long winded epistle from Ron follows. May be headache
inducing. Read only if all issues of Readers' Digest from 1962 are missing
from all libraries with a 50 mile radius, and even then at your own risk,
which may be substantial.]

Bob,

Your mention of a max. empty weight for LSA's caught my attention. I am
not familiar with any regulation in the US of maximum empty weight for an
amateur built experimental airplane (ABE - my acronym only, doesn't appear
in any regs as such), whether flown under light sport regulations or not,
and I don't think there is one.

In the ASTM standards for Special Light Sport Aircraft (SLSA -- factory
built, turnkey aircraft) there _is_ a maximum empty weight standard. If
memory serves, I believe it is stated thusly: max GW (1320 lb.) minus two
170 lb occupants (340 lbs.), minus half the engine's horsepower in fuel. A
100 HP engine would require an allowance for a minimum 50 lbs. of fuel
(approx. 8.3 gal.), so the maximum empty weight of an SLSA so powered
would be 940 lbs. -- if my math is correct.

As you probably know, there is another category of light sport aircraft
that is very confusingly called "Experimental Light Sport Aircraft." The
ELSA is not what most of us are building, which is amateur built
experimental (ABE). The ELSA must first be an SLSA qualified and certified
design, though part of which is built by the owner. Unlike the amateur
built experimental (ABE) type, the owner-built portion of a true ELSA can
be as little as say, 5%. Because the ASTM max. empty weight applies to
SLSA's, it would also apply to ELSA's which in effect have to be approved
SLSA's before they can be sold partially completed as an ELSA.

On the other hand, when what we are building, a true amateur built
experimental (ABE), is inspected here in the US, the inspector (DAR) is
not concerned with whether it will be flown by a light sport pilot or an
ATP-rated pilot. The pilot's qualifications are irrelevant. Similarly,
within ABE aircraft regs. there is no designation or sub-classification
such as a "light sport ABE" or "ABE limited to light sport pilots", so the
light sport regulations, including ASTM standards for SLSA's, are
technically irrelevant to the inspection and certification of any ABE.
There is nothing on the airworthiness certificate (much less the
registration) which says anything about light sport.

It is the ABE builder who is responsible for establishing the GW of the
airplane he builds, because he is the manufacturer. As you probably know,
no plane, whether experimental or conventionally certificated, can ever be
flown under light sport regluations if it has _ever_ had an airworthiness
certificate issued when its gross weight was more than 1320 lbs. (That's
why a Cessna 140 can never be flown as a light sport, even if the owner
somehow gets a new airworthiness cert., or swears on a stack of whatever
never to fly it heavier than 1320 lbs., even though its original GW is
just a little too heavy. A bummer, but true.) So... in order for a sport
pilot to be able to legally fly a Rebel as a light sport plane, the only
requirement vis-a-vis the airplane paperwork is that the builder must set
its max. GW at 1320 lbs. or less at the time of its first inspection, for
its first airworthiness certificate. This is set in two places: on the
official first weight and balance statement, which will probably be
inspected, and on the permanently-affixed metal data plate, which
definitely WILL be inspected.

It is certainly possible that some DAR would refuse to issue an
airworthiness certificate for an ABE plane with a GW of 1320 lbs. that
weighed (to push this to an absurd extreme) say, 1300 lbs. empty, and that
DAR may even have in the back of his mind knowledge of the ASTM standard
for SLSA's, even though in fact there is no official FAA regulation for
maximum empty weight of any ABE. The DAR has some discretion when it comes
to something that's clearly absurd, for sure. But if I, as a sport pilot,
want to fly a 1320 GW Rebel that has an empty weight of 1090 lbs, and it
can only carry me, a chart, a toothbrush, scarf, credit card, and an
hour's worth of fuel -- it would be legal. It would be a short flight
plan, given reserve requirements, but....

As the first "from scratch" sport pilot in most of Northern California, I
was forced study this stuff quite a bit. The regs were all new and even
more ambiguous than they are now. Nobody, including the local FSDO and
DPE's knew what some of the regs meant. I bought the Rebel project 3 weeks
before I got my sport pilot ticket and would not have done so if I wasn't
sure that there was no formal max. empty weight involved for me to fly it
as a light sport plane -- because at that time I couldn't know what the
empty weight would end up being. If I'd had the slightest doubt, I
wouldn't have bought something I might not be able to fly.

Now of course my great certainty about all this doesn't make it so, and I
admit I have been wrong at least once before. :-) But if there's a
regulation for max. empty weight of a true amateur built experimental
airplane, whether flown by a light sport pilot or not, I've yet to find
it, and believe me, I'm even more highly motivated to keep a sharp eye out
for it now than I was when I bought 254R! If anyone knows of such a reg,
I'd rather know now than later, while there's still time to take out the
DVD player, air conditioning, and known ice equipment. :-)

Best,
Ron

On Sun, Mar 8, 2009 at 6:50 PM, Bob Patterson <bobp@prosumers.ca> wrote:
...

It is POSSIBLE that you could come in under the 872 lb. ?? (890 ??)
max. allowed for LSA ..... JUST... with the Lyc. O-235-L2C.


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Tim Hickey

[rebel-builders] What I learned this week! - LSA specs ...

Post by Tim Hickey » Sun Feb 19, 2012 5:16 pm

I think we have been down part of this road before. And I think that there
is a max permitted empty weight for LSA in Canada.
But I do not know of any US requirement for a max empty weight for
Experimental, amateur-built aircraft flown as Light Sport. I am going to pop
over to the EAA website, and see if they have handled this question. If not,
I will ask it, and then post the answer back here for the group.

Tim Hickey
R808
----- Original Message -----
From: "Bob Patterson" <bobp@prosumers.ca>
To: <rebel-builders@dcsol.com>
Sent: Monday, March 09, 2009 11:32 AM
Subject: Re: [rebel-builders] What I learned this week! - LSA specs ...

Hi Ron !

I did NOT mean to imply that there WAS a minimum empty weight
for US Experimental homebuilts - I don't know. In Canada, there IS !
The Canadian max empty weight is arrived at by some bizzare calculation
involving your hat size, wing area, & engine horespower, if I recall ...

Certainly, as you say, there is nothing that I know of preventing a
US Experimental aircraft being registered at 1,320 gross with 1,000 lb
empty weight. PROVIDED it is flown with a PPL or higher !

In any case, my understanding is that, in order to fly ANY aircraft
with a Sport Pilot licence, that aircraft must MEET <ALL> REQUIREMENTS
for LSA - ie max. empty weight, as well as max gross weight, as well as
max cruise & stall speeds, and fixed/ground adjustable pitch prop, etc..
That is only MY understanding, although it seems to be shared by many.

I'm open to correction ! ;-)

--


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Tim Hickey

[rebel-builders] What I learned this week! - LSA specs ...

Post by Tim Hickey » Sun Feb 19, 2012 5:16 pm

I snagged this from the EAA website, under the "Ask the Expert"
section


Question :
I have been told that there is a maximum empty weight for a light
sport aircraft as well as a max takeoff weight of 1320. It is suggested to
be 890. Is this the case?

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

Answer :
This only applies to special light-sport aircraft (SLSA) certificated
as such based on the ASTM consensus standards. It is not a maximum empty
weight, but rather a minimum useful load, and it is based on the number of
seats and the maximum horsepower of the engine. The formula is as follows:

The aircraft must have a useful at least equal to 190 lbs per seat
plus a number equal to 50% of the maximum horsepower of the engine. By this
formula, a two seat aircraft with a 100 hp engine would have to have a
useful load of at least 430 lbs (190*2+50). So if the gross weight of this
aircraft is 1320 lbs then the empty weight could be no more than 890 lbs.
This is where you got the 890 lb number you quoted in your question.

But as you can see, if the aircraft has a different horsepower engine
then the minimum useful load (and thus the allowed empty weight) will be
different. If the aircraft has a 120 hp engine then the minimum useful load
will be 440 lbs (190*2+60), so if the gross is 1320 lbs the maximum empty
weight would have to be 880 lbs or less. But if the aircraft only has an 80
hp engine the minimum useful load would only be 420 lbs, so with a gross of
1320 lbs the empty weight could be as high as 900 lbs. Of course if the
gross weight is less than 1320 then the empty weight of any of these
aircraft would have to be less as well in order to allow the minimum useful
load.

Again this only applies to SLSA certificated aircraft. Standard
category aircraft, amateur-built aircraft, or ELSA are not required to
comply with this formula for minimum useful load.




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Tim Hickey

[rebel-builders] What I learned this week! - LSA specs ...

Post by Tim Hickey » Sun Feb 19, 2012 5:16 pm

Here is another one I found there. Right down this alley.


Question :
I'm thinking of buying a Murphy Rebel project that has not been
completed and registered. It has the 1650 lb GW kit. Can I complete the
project and fly it as a Sport Pilot? Can I or do I have to limit the GW to
1320 lbs on the airplane data plate and license as an LSA?

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

Answer :
Since the aircraft has not yet been completed and certificated, it
does not "have" a 1650 lb gross weight. The kit vendor may suggest that as a
gross weight, but the individual aircraft builder sets the gross weight of a
particular aircraft during the certification and flight testing process.

You could build the aircraft and certificate it at the 1320 lb gross
weight, in which case this individual aircraft would be eligible for sport
pilots to fly (assuming it fits all the other parameters of the LSA
definition). However, you would have to make sure that the aircraft's empty
weight is such that it allows a reasonable useful load. Setting the gross
weight too low in relation to the empty weight will not make for a very
useful aircraft, so you need to use some common sense in setting the maximum
gross weight.




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Joe Ronco

[rebel-builders] What I learned this week! - LSA specs ...

Post by Joe Ronco » Sun Feb 19, 2012 5:16 pm

TIM: Here is what the EAA says (emphasis is mine):




Question :
I have been told that there is a maximum empty weight for a light sport
aircraft as well as a max takeoff weight of 1320. It is suggested to be 890.
Is this the case?





Answer :
This only applies to special light-sport aircraft (SLSA) certificated as
such based on the ASTM consensus standards. It is not a maximum empty
weight, but rather a minimum useful load, and it is based on the number of
seats and the maximum horsepower of the engine. The formula is as follows:

The aircraft must have a useful at least equal to 190 lbs per seat plus a
number equal to 50% of the maximum horsepower of the engine. By this
formula, a two seat aircraft with a 100 hp engine would have to have a
useful load of at least 430 lbs (190*2+50). So if the gross weight of this
aircraft is 1320 lbs then the empty weight could be no more than 890 lbs.
This is where you got the 890 lb number you quoted in your question.

But as you can see, if the aircraft has a different horsepower engine then
the minimum useful load (and thus the allowed empty weight) will be
different. If the aircraft has a 120 hp engine then the minimum useful load
will be 440 lbs (190*2+60), so if the gross is 1320 lbs the maximum empty
weight would have to be 880 lbs or less. But if the aircraft only has an 80
hp engine the minimum useful load would only be 420 lbs, so with a gross of
1320 lbs the empty weight could be as high as 900 lbs. Of course if the
gross weight is less than 1320 then the empty weight of any of these
aircraft would have to be less as well in order to allow the minimum useful
load.

Again this only applies to SLSA certificated aircraft. Standard category
aircraft, amateur-built aircraft, or ELSA are not required to comply with
this formula for minimum useful load.








You can check this out at:



http://www.sportpilot.org/questions/afm ... faqid=1523



J Joe R



-----Original Message-----
From: mike.davis@dcsol.com [mailto:mike.davis@dcsol.com] On Behalf Of Tim
Hickey
Sent: Monday, March 09, 2009 10:44 AM
To: rebel-builders@dcsol.com
Subject: Re: [rebel-builders] What I learned this week! - LSA specs ...



I think we have been down part of this road before. And I think that there

is a max permitted empty weight for LSA in Canada.

But I do not know of any US requirement for a max empty weight for

Experimental, amateur-built aircraft flown as Light Sport. I am going to pop


over to the EAA website, and see if they have handled this question. If not,


I will ask it, and then post the answer back here for the group.



Tim Hickey

R808

----- Original Message -----

From: "Bob Patterson" <bobp@prosumers.ca>

To: <rebel-builders@dcsol.com>

Sent: Monday, March 09, 2009 11:32 AM

Subject: Re: [rebel-builders] What I learned this week! - LSA specs ...





Hi Ron !
I did NOT mean to imply that there WAS a minimum empty weight
for US Experimental homebuilts - I don't know. In Canada, there IS !
The Canadian max empty weight is arrived at by some bizzare calculation
involving your hat size, wing area, & engine horespower, if I recall ...
Certainly, as you say, there is nothing that I know of preventing a
US Experimental aircraft being registered at 1,320 gross with 1,000 lb
empty weight. PROVIDED it is flown with a PPL or higher !
In any case, my understanding is that, in order to fly ANY aircraft
with a Sport Pilot licence, that aircraft must MEET <ALL> REQUIREMENTS
for LSA - ie max. empty weight, as well as max gross weight, as well as
max cruise & stall speeds, and fixed/ground adjustable pitch prop, etc..
That is only MY understanding, although it seems to be shared by many.
I'm open to correction ! ;-)
--







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Keith Leitch

[rebel-builders] What I learned this week! - LSA specs ...

Post by Keith Leitch » Sun Feb 19, 2012 5:16 pm

Tim,
I have been down the road you are asking about. I started my Rebel several years ago and have been building it with the idea of installing an O-320. Since then, I have had health issues that have made me decide to let my medical expire and fly under SP rules. I asked similar question to what you are asking and one of the answer you posted here may be the answer I recieved from Joe Norris of the EAA. I can still build it with an O-320 and list the GW as 1320. But it will be a very limited use plane. I don't really care. I just want STOL cababilities and fly 99% by myself anyways. My plan for now is to try and build the rest of the plane as light as possible. Might even have to avoid an electrical system. Haven't decided yet.

Bob Patterson

[rebel-builders] What I learned this week! - LSA specs ...

Post by Bob Patterson » Sun Feb 19, 2012 5:16 pm

That's great news Tim !

Sounds like you folks have 'No worries' ! :-)

I was only worried about the part that said....
" (assuming it fits all the other parameters of the LSA
definition)" I guess that's not an issue ...

Good news - now "Just get it FLYING !"(tm) :-)

--
......bobp
bobp@prosumers.ca
http://www.prosumers.ca/Ramble09

http://bpatterson.qhealthbeauty.com
http://apatterson2.qhealthzone.com
http://apatterson2.ordermygift.com

-------------------------------orig.-------------------------
On Monday 09 March 2009 16:53, Tim Hickey wrote:
Here is another one I found there. Right down this alley.


Question :
I'm thinking of buying a Murphy Rebel project that has not been
completed and registered. It has the 1650 lb GW kit. Can I complete the
project and fly it as a Sport Pilot? Can I or do I have to limit the GW to
1320 lbs on the airplane data plate and license as an LSA?

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

Answer :
Since the aircraft has not yet been completed and certificated, it
does not "have" a 1650 lb gross weight. The kit vendor may suggest that as
a gross weight, but the individual aircraft builder sets the gross weight
of a particular aircraft during the certification and flight testing
process.

You could build the aircraft and certificate it at the 1320 lb gross
weight, in which case this individual aircraft would be eligible for sport
pilots to fly (assuming it fits all the other parameters of the LSA
definition). However, you would have to make sure that the aircraft's
empty weight is such that it allows a reasonable useful load. Setting the
gross weight too low in relation to the empty weight will not make for a
very useful aircraft, so you need to use some common sense in setting the
maximum gross weight.


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Ron Shannon

[rebel-builders] What I learned this week! - LSA specs ...

Post by Ron Shannon » Sun Feb 19, 2012 5:16 pm

Fine, Bob. This isn't the first time there's been confusion on the list
about whether a particular item refers to US Light Sport Aircraft (& pilot)
context, or the Canadian Advanced Ultralight requirements. I should know.
I'm _always_ confused, even when the context is staring me in the face. ;-)

Still, as you can see from the later discussion, unless I'm missing
something again, a US Sport Pilot _can_ fly a US experimental such as you're
describing below, assuming other LSA requirements (2 seats, fixed prop,
etc.) are met. PPL not required.

Ron

On Mon, Mar 9, 2009 at 8:32 AM, Bob Patterson <bobp@prosumers.ca> wrote:
....
Certainly, as you say, there is nothing that I know of preventing a
US Experimental aircraft being registered at 1,320 gross with 1,000 lb
empty weight. PROVIDED it is flown with a PPL or higher !


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David Jackson

[rebel-builders] What I learned this week! - LSA specs ...

Post by David Jackson » Sun Feb 19, 2012 5:16 pm

Canada does not have a Light Sport Aircraft category. Bob was referring to Experimental amateur-built aircraft. The maximum weight for an experimental aircraft is calculated based on wing loading and the minimum weight is calculated from the maximum weight and the engine horsepower:



549.107 Maximum Empty Mass

To ensure that an adequate minimum useful load, including fuel, can be carried within the maximum permissible take-off mass declared by the applicant in accordance with section 549.103, the maximum empty mass MEmax (weight WEmax) of the aircraft shall not be greater than that determined by the following equation:



where:

MTOmax (WTOmax) = maximum permissible take-off mass (weight) selected by the applicant in kg (lb);
a = number of passenger seats, as defined in 549.105;
P = rated power of engine(s) in KW (BHP).


I confess that I have not done the calculations to determine what the maximum registered gross weight of a Rebel could be or how that translates into maximum empty weight.



DJ
From: tjhickey@iowatelecom.net
To: rebel-builders@dcsol.com
Subject: Re: [rebel-builders] What I learned this week! - LSA specs ...
Date: Mon, 9 Mar 2009 11:44:26 -0500

I think we have been down part of this road before. And I think that there
is a max permitted empty weight for LSA in Canada.
But I do not know of any US requirement for a max empty weight for
Experimental, amateur-built aircraft flown as Light Sport. I am going to pop
over to the EAA website, and see if they have handled this question. If not,
I will ask it, and then post the answer back here for the group.

Tim Hickey
R808
----- Original Message -----
From: "Bob Patterson" <bobp@prosumers.ca>
To: <rebel-builders@dcsol.com>
Sent: Monday, March 09, 2009 11:32 AM
Subject: Re: [rebel-builders] What I learned this week! - LSA specs ...

Hi Ron !

I did NOT mean to imply that there WAS a minimum empty weight
for US Experimental homebuilts - I don't know. In Canada, there IS !
The Canadian max empty weight is arrived at by some bizzare calculation
involving your hat size, wing area, & engine horespower, if I recall ...

Certainly, as you say, there is nothing that I know of preventing a
US Experimental aircraft being registered at 1,320 gross with 1,000 lb
empty weight. PROVIDED it is flown with a PPL or higher !

In any case, my understanding is that, in order to fly ANY aircraft
with a Sport Pilot licence, that aircraft must MEET <ALL> REQUIREMENTS
for LSA - ie max. empty weight, as well as max gross weight, as well as
max cruise & stall speeds, and fixed/ground adjustable pitch prop, etc..
That is only MY understanding, although it seems to be shared by many.

I'm open to correction ! ;-)

--


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_________________________________________________________________
Reunite with the people closest to you, chat face to face with Messenger.
http://go.microsoft.com/?linkid=9650736



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David Jackson

[rebel-builders] What I learned this week! - LSA specs ...

Post by David Jackson » Sun Feb 19, 2012 5:16 pm

The equation got stripped from the E-mail because it was a picture.

In non-metric form it reads:

Maximum empty weight = Maximum takeoff Weight - (175 + 175 x sqrt(a) + .5P)



For a 150 Hp Engine and two seats that would mean a minimum useful load of 497.5 lbs.

For a 100 Hp Engine and two seats it would be 472.5 lbs.



In theory then, a two-seater registered at a gross weight of 1320 lbs with a 100 horsepower engine would have a maximum empty weight of 1320-472.5 = 847.5 lbs.
From: canadjn@hotmail.com
To: rebel-builders@dcsol.com
Subject: RE: [rebel-builders] What I learned this week! - LSA specs ...
Date: Mon, 9 Mar 2009 13:49:37 -0400


Canada does not have a Light Sport Aircraft category. Bob was referring to Experimental amateur-built aircraft. The maximum weight for an experimental aircraft is calculated based on wing loading and the minimum weight is calculated from the maximum weight and the engine horsepower:



549.107 Maximum Empty Mass

To ensure that an adequate minimum useful load, including fuel, can be carried within the maximum permissible take-off mass declared by the applicant in accordance with section 549.103, the maximum empty mass MEmax (weight WEmax) of the aircraft shall not be greater than that determined by the following equation:



where:

MTOmax (WTOmax) = maximum permissible take-off mass (weight) selected by the applicant in kg (lb);
a = number of passenger seats, as defined in 549.105;
P = rated power of engine(s) in KW (BHP).


I confess that I have not done the calculations to determine what the maximum registered gross weight of a Rebel could be or how that translates into maximum empty weight.



DJ
From: tjhickey@iowatelecom.net
To: rebel-builders@dcsol.com
Subject: Re: [rebel-builders] What I learned this week! - LSA specs ...
Date: Mon, 9 Mar 2009 11:44:26 -0500

I think we have been down part of this road before. And I think that there
is a max permitted empty weight for LSA in Canada.
But I do not know of any US requirement for a max empty weight for
Experimental, amateur-built aircraft flown as Light Sport. I am going to pop
over to the EAA website, and see if they have handled this question. If not,
I will ask it, and then post the answer back here for the group.

Tim Hickey
R808
----- Original Message -----
From: "Bob Patterson" <bobp@prosumers.ca>
To: <rebel-builders@dcsol.com>
Sent: Monday, March 09, 2009 11:32 AM
Subject: Re: [rebel-builders] What I learned this week! - LSA specs ...

Hi Ron !

I did NOT mean to imply that there WAS a minimum empty weight
for US Experimental homebuilts - I don't know. In Canada, there IS !
The Canadian max empty weight is arrived at by some bizzare calculation
involving your hat size, wing area, & engine horespower, if I recall ...

Certainly, as you say, there is nothing that I know of preventing a
US Experimental aircraft being registered at 1,320 gross with 1,000 lb
empty weight. PROVIDED it is flown with a PPL or higher !

In any case, my understanding is that, in order to fly ANY aircraft
with a Sport Pilot licence, that aircraft must MEET <ALL> REQUIREMENTS
for LSA - ie max. empty weight, as well as max gross weight, as well as
max cruise & stall speeds, and fixed/ground adjustable pitch prop, etc..
That is only MY understanding, although it seems to be shared by many.

I'm open to correction ! ;-)

--


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Wayne G. O'Shea

[rebel-builders] What I learned this week! - LSA specs ...

Post by Wayne G. O'Shea » Sun Feb 19, 2012 5:16 pm

The reasoning behind this calculation is to be sure you can actually carry
fuel !

----- Original Message -----
From: "David Jackson" <canadjn@hotmail.com>
To: "Rebel Builders" <rebel-builders@dcsol.com>
Sent: Monday, March 09, 2009 2:02 PM
Subject: RE: [rebel-builders] What I learned this week! - LSA specs ...

The equation got stripped from the E-mail because it was a picture.

In non-metric form it reads:

Maximum empty weight = Maximum takeoff Weight - (175 + 175 x sqrt(a) +
.5P)



For a 150 Hp Engine and two seats that would mean a minimum useful load of
497.5 lbs.

For a 100 Hp Engine and two seats it would be 472.5 lbs.



In theory then, a two-seater registered at a gross weight of 1320 lbs with
a 100 horsepower engine would have a maximum empty weight of 1320-472.5 =
847.5 lbs.
From: canadjn@hotmail.com
To: rebel-builders@dcsol.com
Subject: RE: [rebel-builders] What I learned this week! - LSA specs ...
Date: Mon, 9 Mar 2009 13:49:37 -0400


Canada does not have a Light Sport Aircraft category. Bob was referring
to Experimental amateur-built aircraft. The maximum weight for an
experimental aircraft is calculated based on wing loading and the minimum
weight is calculated from the maximum weight and the engine horsepower:



549.107 Maximum Empty Mass

To ensure that an adequate minimum useful load, including fuel, can be
carried within the maximum permissible take-off mass declared by the
applicant in accordance with section 549.103, the maximum empty mass
MEmax (weight WEmax) of the aircraft shall not be greater than that
determined by the following equation:



where:

MTOmax (WTOmax) = maximum permissible take-off mass (weight) selected by
the applicant in kg (lb);
a = number of passenger seats, as defined in 549.105;
P = rated power of engine(s) in KW (BHP).


I confess that I have not done the calculations to determine what the
maximum registered gross weight of a Rebel could be or how that
translates into maximum empty weight.



DJ
From: tjhickey@iowatelecom.net
To: rebel-builders@dcsol.com
Subject: Re: [rebel-builders] What I learned this week! - LSA specs ...
Date: Mon, 9 Mar 2009 11:44:26 -0500

I think we have been down part of this road before. And I think that
there
is a max permitted empty weight for LSA in Canada.
But I do not know of any US requirement for a max empty weight for
Experimental, amateur-built aircraft flown as Light Sport. I am going
to pop
over to the EAA website, and see if they have handled this question. If
not,
I will ask it, and then post the answer back here for the group.

Tim Hickey
R808
----- Original Message -----
From: "Bob Patterson" <bobp@prosumers.ca>
To: <rebel-builders@dcsol.com>
Sent: Monday, March 09, 2009 11:32 AM
Subject: Re: [rebel-builders] What I learned this week! - LSA specs ...



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