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 Post subject: Re: Cirrus SF50
PostPosted: 17 May 2016, 19:59 
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Joined: 12/03/14
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Username Protected wrote:
So how is the Eclipse not a "personal jet"?

By being essentially out of production, having weird avionics, having support problems.

Mike C.

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 Post subject: Re: Cirrus SF50
PostPosted: 17 May 2016, 20:04 
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Joined: 01/29/08
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Location: Walterboro, SC. KRBW
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Username Protected wrote:
So how is the Eclipse not a "personal jet"?

By being essentially out of production, having weird avionics, having support problems.

Mike C.

The Eclipse is the twin SF50 you want.

How much more does it cost to operate a CJ4 compared to an Eclipse?

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 Post subject: Re: Cirrus SF50
PostPosted: 17 May 2016, 20:11 
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Username Protected wrote:
A CJ4 is definitely not a "personal jet".

Mike C.

I know of several CJ4 owner/operators that would adamantly disagree with that. The CJ4 might be the ultimate SP personal jet.

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 Post subject: Re: Cirrus SF50
PostPosted: 17 May 2016, 20:13 
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Username Protected wrote:
I know of several CJ4 owner/operators that would adamantly disagree with that. The CJ4 might be the ultimate SP personal jet.

I disagree with it too.

Anything single pilot is a "personal jet". I think all SP jets cost about the same to run. Eclipse vs. CJ4 are extreme opposites but I bet they're still a few hundred $$ apart..... Not thousands of $$ apart.

TBM vs. Pilatus vs. Meridien...... They all cost the same to run. A couple hundred $$ difference is no difference because it can't be measured.


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 Post subject: Re: Cirrus SF50
PostPosted: 17 May 2016, 20:17 
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Joined: 05/23/08
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Location: CMB7, Ottawa, Canada
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Define personal jet.
Trump as a personal 757 jet, the prince of Saudi flys a personal A380. Its all relative.



Username Protected wrote:
A CJ4 is definitely not a "personal jet".

Mike C.

I know of several CJ4 owner/operators that would adamantly disagree with that. The CJ4 might be the ultimate SP personal jet.

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 Post subject: Re: Cirrus SF50
PostPosted: 17 May 2016, 20:19 
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Joined: 11/23/12
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Company: CSRA Document Solutions
Location: Aiken, SC KAIK
I find it almost funny that anyone who buys the planes mentioned on the past 3 or 4 pages really cares about nm per gallon. It's like buying a 60 ft sport fishing boat and worrying about the price of bait....

You guys crack me up sometimes.

Peace,
Don<><


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 Post subject: Re: Cirrus SF50
PostPosted: 17 May 2016, 20:23 
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Joined: 08/20/09
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Company: Jcrane, Inc.
Location: KVES Greenville, OH
Aircraft: C441, RV7A
Username Protected wrote:
I looked up the TBM850 AFM.

At FL180, max cruise is 294 KTAS, 70.5 GPH, 4.17 nm/gal.

At FL180, long range cruise is 201 KTAS, 42.8 nm/gal, 4.70 nm/gal.

Both are quite a bit better than the SF50:

MCT 283 KTAS, 84 GPH, 3.37 nm/gal

LRC 217 KTAS, 54 GPH, 4.02 nm/gal.

The TBM850 in high speed cruise is faster and gets better mileage than the the SF50 in LRC.

We see these numbers differently, I see a wash. I'd choose between those two aircraft based on other factors (roominess, how they felt, fit/finish, chute, etc).
Oh, and price.

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 Post subject: Re: Cirrus SF50
PostPosted: 17 May 2016, 21:04 
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Joined: 10/31/14
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Aircraft: eclipse
Username Protected wrote:
So how is the Eclipse not a "personal jet"?

By being essentially out of production, having weird avionics, having support problems.

Mike C.


They made 3 in the first quarter of this year, the avionics are specifically geared to single pilot and support has been great for years,


By the way there are now more Eclipses flying in the USA than Mits

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 Post subject: Re: Cirrus SF50
PostPosted: 17 May 2016, 21:21 
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Aircraft: UMF3, UBF 2, P180 II
Username Protected wrote:
I looked up the TBM850 AFM.

At FL180, max cruise is 294 KTAS, 70.5 GPH, 4.17 nm/gal.

At FL180, long range cruise is 201 KTAS, 42.8 nm/gal, 4.70 nm/gal.

Both are quite a bit better than the SF50:

MCT 283 KTAS, 84 GPH, 3.37 nm/gal

LRC 217 KTAS, 54 GPH, 4.02 nm/gal.

The TBM850 in high speed cruise is faster and gets better mileage than the the SF50 in LRC.

We see these numbers differently, I see a wash. I'd choose between those two aircraft based on other factors (roominess, how they felt, fit/finish, chute, etc).
Oh, and price.


Cheapest is hardly ever best.

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 Post subject: Re: Cirrus SF50
PostPosted: 17 May 2016, 21:24 
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Joined: 11/03/08
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Location: Peachtree City GA / Stoke-On-Trent UK
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Username Protected wrote:
I find it almost funny that anyone who buys the planes mentioned on the past 3 or 4 pages really cares about nm per gallon. It's like buying a 60 ft sport fishing boat and worrying about the price of bait....

You guys crack me up sometimes.

Peace,
Don<><

It's not so much the cost of the fuel as how far can go before stopping, or how much fuel weight you need to carry. Better mileage=less fuel weight=faster climb and higher cruise.


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 Post subject: Re: Cirrus SF50
PostPosted: 17 May 2016, 21:31 
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Joined: 01/07/13
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Company: Tupelo Aero, Inc
Location: Pontotoc , MS (22M)
Aircraft: 1959 Twin Beech 18
Username Protected wrote:
A CJ4 is definitely not a "personal jet".

Mike C.

I know of several CJ4 owner/operators that would adamantly disagree with that. The CJ4 might be the ultimate SP personal jet.


Mike ,

Is pontificating about things beyond his(flying) experience Again! :beechslap: a Having flown a CJ 4 several times, I think it's combination of single pilot, simple operate systems, great climb, good Cruise speed and good short field preformance make it THE ultimate single pilot personal jet.

Cessna got RIGHT this time.

Sea level to Fl 430 in 18 mins
430 knots cruise
Good range

The only thing bad about the CJ4 is the price!! :woot:
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 Post subject: Re: Cirrus SF50
PostPosted: 17 May 2016, 21:51 
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Username Protected wrote:
Answered many times.

TBM and PC12 got certified long ago, prior to amendment 49 of part 23, under rules that allowed higher service ceilings without redundant pressurization. Then the rules changed in amendment 49, lowered that ceiling to Fl250. That left the TBM and PC12 grandfathered, but new designs can't get the same thing.

From AC 23-17C:

Amendment 23-49 and Subsequent

This amendment changed the 33,000 feet in § 23.841(a) to 25,000 feet based on European Joint Aviation Requirements Proposals.



So what you are saying then is there are no real technical reasons why you couldn't fly above 25,000 ft without that second source, it's just rules. Funny thing about rules - they can be changed. :peace:


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 Post subject: Re: Cirrus SF50
PostPosted: 17 May 2016, 21:51 
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Username Protected wrote:
Maybe someone isn't a fan of the SF50 but wants to see the path to a twin engine version. Assuming that's in the pipeline (not a hard assumption), as a company I'd be interested in keeping anyone active who was in the market for a jet.

If I were developing a new design, I'd be very interested in the opinions of someone who could use, and afford, my airplane but didn't want it. If there is something in my design that is turning off potential customers I'd be foolish to ignore those talking about it.

Maybe those opinions are based on incorrect assumptions and I know my product will persuade them, but if not then I'd better take their input seriously.

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 Post subject: Re: Cirrus SF50
PostPosted: 17 May 2016, 21:53 
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Joined: 05/23/13
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I agree that the CJ4 is as good as it gets for an aircraft of this category and all of the talk about operating cost is a little over blown... no other jet does as much, as well, without being a pain to operate...

And I have a client that needs to sell his 2014 CJ4 so we can buy him something else... so pony up and buy it!

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 Post subject: Re: Cirrus SF50
PostPosted: 17 May 2016, 21:54 
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Joined: 02/28/12
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Username Protected wrote:

The SF50 will not go to the high flight levels even if the rules change (which they won't regardless). The ceiling affects MANY things intrinsic to the design. It would have to be a redesign to go up there.

Mike C.


1. Well the rules are changing, there is a critical missing component in the new regs - it isn't what is there but what is missing now.

2. I have spent my career working under the FAA boot heel - All my designs have been safe, and 50% to 60% of them controversial & new. Some of these have fallen into special conditions, issue papers and ELOS, the FAA has formalized ways of bending. I have not been stopped on what needed to be accomplished. No good engineer ever is.

2. Understood on only designing to FL 280, I understand the quagmire of regulations that imposed that limit - but where has that been stated that was the design goal? Yes I remember the slowest lowest jet Alan K mentioned 7 years ago - Lots of water under the Duluth Lift Bridge since then.

3. Most of us in the business are familiar with the operational efficiencies of Jets & turbines

This really falls under how do you eat an elephant -

You are now flying an aircraft that was once vilified - It took a little time to realize its potential. It took time to mandate pilot training. Maybe that lesson wasn't lost on us all.


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