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Rec.Aviation OSH report



 
 
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  #31  
Old August 2nd 06, 12:33 AM posted to rec.aviation.homebuilt
Ken Finney
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Posts: 190
Default Rec.Aviation OSH report


"Ron Wanttaja" wrote in message
...
On Tue, 1 Aug 2006 21:44:10 GMT, "Ken Finney"

wrote:

I am guessing that for tax purposes, calling it a "proof of concept" is
better than calling it a "prototype".


Don't know why it would make a difference, tax-wise.

My guess is that it's a combination of factors. "Prototype" implies it is
the
first aircraft of a series of aircraft, and Cessna may not yet have Board
of
Directors' approval to start production.

Also, if major changes have to be made (such as a switch to another
engine), the
"spin control" is easier with a "Proof of Concept." Big changes between
the
"Prototype" and the production aircraft implies some faulty decisions
during the
design process, but if you call it a "Proof of Concept" you can just
claim,
"Well, we were just trying different ideas, pushing the envelope, that
sort of
thing." Then you build a "prototype" that closely matches the production
model.

Ron Wanttaja


I live for tax law, but I've never owned a manufacturing company. ;^)

I'm guessing that a "proof of concept" is research and development, and
therefore deductable in the year it occurs, whereas the tooling etcetera for
a prototype would have to be amortized over time.



  #32  
Old August 2nd 06, 12:49 AM posted to rec.aviation.homebuilt
RST Engineering
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Posts: 1,147
Default Rec.Aviation OSH report


"Morgans" wrote in message
...


I can't figure out why they chose the Rotax. Wouldn't an O-200 work well
in
that plane?


WEight
Performance
1970s technology (aot 1930s)
Auto gas
Less expensive initial and parts
Reliability




I'll bet the FBO's would be more comfortable with a regular 'ole engine in
it, that they know and understand how to work on.


These are destined to be the "regular 'ole engines" in the years to come.

Jim


  #33  
Old August 2nd 06, 01:25 AM posted to rec.aviation.homebuilt
Ron Wanttaja
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Posts: 756
Default Rec.Aviation OSH report

On Tue, 1 Aug 2006 16:49:32 -0700, "RST Engineering"
wrote:


"Morgans" wrote in message
...


I can't figure out why they chose the Rotax. Wouldn't an O-200 work well
in
that plane?


WEight
Performance
1970s technology (aot 1930s)
Auto gas
Less expensive initial and parts
Reliability

I'll bet the FBO's would be more comfortable with a regular 'ole engine in
it, that they know and understand how to work on.


These are destined to be the "regular 'ole engines" in the years to come.


'An when you get to Weir's age, being "regular" is the most important thing
there is! :-)

But the Rotax is not every tolerant of 100LL fuel. The lead gets dissolved into
the oil and sludges things up...these engines don't have the sloppy tolerances
of the Lycosaurs.

From http://www.rtx-av-engines.ca/PDF/techinfofuel.pdf:

"The problems with the leaded fuels are the pollution and the heavy deposits
of lead left on the spark plugs, piston rings, oil passages, and cylinder heads.
Fuels with lead can be used if the operator is willing to increase maintenance
on these parts. In many cases the engine will require a top overhaul well before
the TBO due to the lead contamination. Additives that help purge the lead, TCP
for example, are beneficial, but, are not yet recommended by Rotax due to the
volatile nature of such an additive. The Rotax liquid cooled head is also a
problem with a lead enhanced fuel. In simple terms it runs too cold. The head
never gets hot enough to allow the lead to “purge” itself of the deposits and
they build up over time."

Most of the reports regarding Diamond's switch from the Rotax 912 to the
Continental IO-240 emphasize the increased power, but AVweb says some smaller
operators were having problems with the engine. Due to the use of 100LL?

Filling up your friendly personal LSA with car gas isn't a problem...but an FBO
considering operating a fleet as trainers may well be scared off due to the
increased maintenance and the decrease in overhaul interval.

Yes, they *should* just set up a autofuel tanking system...but we've got a
chicken and the egg situation, there.

It *does* make you wonder about all those LSA companies, selling planes that
require fuel that isn't sold at 99% of American airports....

My bet? Cessna switches to a Lycosaur, if the plane goes into production.


Ron Wanttaja
  #34  
Old August 2nd 06, 01:33 AM posted to rec.aviation.homebuilt
Morgans[_3_]
external usenet poster
 
Posts: 407
Default Rec.Aviation OSH report


"Ron Wanttaja" wrote

Don't know why it would make a difference, tax-wise.

My guess is that it's a combination of factors. "Prototype" implies it is

the
first aircraft of a series of aircraft, and Cessna may not yet have Board

of
Directors' approval to start production.

Also, if major changes have to be made (such as a switch to another

engine), the
"spin control" is easier with a "Proof of Concept." Big changes between

the
"Prototype" and the production aircraft implies some faulty decisions

during the
design process, but if you call it a "Proof of Concept" you can just

claim,
"Well, we were just trying different ideas, pushing the envelope, that

sort of
thing." Then you build a "prototype" that closely matches the production

model.

I can't figure out why they chose the Rotax. Wouldn't an O-200 work well in
that plane?

I'll bet the FBO's would be more comfortable with a regular 'ole engine in
it, that they know and understand how to work on.
--
Jim in NC

  #35  
Old August 2nd 06, 04:00 AM posted to rec.aviation.homebuilt,rec.aviation.owning,rec.aviation.piloting
Stella Starr
external usenet poster
 
Posts: 92
Default Rec.Aviation OSH report

I set out in a C-152 one nice summer day to fly across Lake Superior at
the narrow end, not so far from Duluth. The cloud cover was thin
overhead but it seemed lower ahead, and after realizing it had the
potential to A: drive me into the water scud-running, or B: make me
discover the that rising shore on the other side went up into the
clouds, I retreated and flew the long way around the shore.

I'm a great swimmer. But I've waded in Superior. It feels like dunking
your feet in a Coke full of ice, even when it's 88 up in the air.

http://www.coas****ch.msu.edu/

This indicates places along the south shore where, after a week or more
of onshore temps pushing three digits, the water temp's in the 30s.

I'd bet a couple miles from shore, Michigan is no picnic either.



Steven P. McNicoll wrote:
"Roger" wrote in message
...
I know many who cross the lake single engine and do it regularly
myself and have for years. Life jackets are a necessity as I can't
swim but the lake is too cold for long survival even in summer.


So you wear the life jacket so your body may be found?


  #36  
Old August 2nd 06, 10:00 AM posted to rec.aviation.homebuilt,rec.aviation.owning,rec.aviation.piloting
Thomas Borchert
external usenet poster
 
Posts: 1,749
Default Rec.Aviation OSH report

Matt,

No, they are prototypes.


If you want to call them something different than Cessna, do it. Cessna
calls them proof of concept. Both of them. And I've seen enough
"marketing speak" to have an idea just why they might do that.

--
Thomas Borchert (EDDH)

  #37  
Old August 2nd 06, 08:34 PM posted to rec.aviation.homebuilt
Peter Dohm
external usenet poster
 
Posts: 1,754
Default Rec.Aviation OSH report

"Ron Wanttaja" wrote in message
...
On Tue, 1 Aug 2006 21:44:10 GMT, "Ken Finney"


wrote:

I am guessing that for tax purposes, calling it a "proof of concept" is
better than calling it a "prototype".


Don't know why it would make a difference, tax-wise.

My guess is that it's a combination of factors. "Prototype" implies it is

the
first aircraft of a series of aircraft, and Cessna may not yet have Board

of
Directors' approval to start production.

Also, if major changes have to be made (such as a switch to another

engine), the
"spin control" is easier with a "Proof of Concept." Big changes between

the
"Prototype" and the production aircraft implies some faulty decisions

during the
design process, but if you call it a "Proof of Concept" you can just

claim,
"Well, we were just trying different ideas, pushing the envelope, that

sort of
thing." Then you build a "prototype" that closely matches the production

model.

Ron Wanttaja


I believe that you have smacked the nail squarely on the head!

Peter


  #38  
Old August 2nd 06, 08:39 PM posted to rec.aviation.homebuilt
Peter Dohm
external usenet poster
 
Posts: 1,754
Default Rec.Aviation OSH report

------snip---------

I can't figure out why they chose the Rotax. Wouldn't an O-200 work well

in
that plane?

I'll bet the FBO's would be more comfortable with a regular 'ole engine in
it, that they know and understand how to work on.
--
Jim in NC

I agree, and this is the primary source of my extreme irritation with the
current weight limit. If you add 25Kg to the engine, then you have to make
the airframe or usefull load that much less, with the result that
manufacturers are driven to accept finicky little engines with levels of
residual thrust that would be barely acceptable in a jet.

Peter


  #39  
Old August 3rd 06, 05:18 AM posted to rec.aviation.homebuilt
Montblack[_1_]
external usenet poster
 
Posts: 429
Default Rec.Aviation OSH report

("Bryan Martin" wrote)
The O-200 is made by Continental. Cessna is a division of Textron and so

is Lycoming. You're not going to see a Continental in a Cessna.


That would be a little like Saturn putting a Honda Pilot engine in their
VUE-SUV.


Montblack
Two-point "conversion" for working Pilot into the mix.
(Football season just around the corner)

 




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