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 Post subject: Re: Cirrus SF50
PostPosted: 17 May 2016, 18:29 
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Username Protected wrote:
The TBM seems to be +35% more climb rate.

and 2X the price.

What is a "personal jet"? This term just popped up out of nowhere.

Is the TBM a "personal turboprop"?


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 Post subject: Re: Cirrus SF50
PostPosted: 17 May 2016, 18:48 
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How come the TBM can go to 310 but the Cirrus will be held to 280 ?

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 Post subject: Re: Cirrus SF50
PostPosted: 17 May 2016, 18:50 
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Username Protected wrote:
The TBM seems to be +35% more climb rate.

and 2X the price.

What is a "personal jet"? This term just popped up out of nowhere.

Is the TBM a "personal turboprop"?


I agree....Its a Cirrus JET. Personal or Not we still don´t know if this data represents maximum ROC; probably not...
So more points to the SF50: Half the price with similar performance to the TBM...

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 Post subject: Re: Cirrus SF50
PostPosted: 17 May 2016, 19:16 
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Joined: 12/17/13
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Aircraft: Aerostar Superstar 2
Username Protected wrote:
How come the TBM can go to 310 but the Cirrus will be held to 280 ?


I think because it was certified before more strenuous backup requirements were implemented. I think, but could be wrong, that today they require a redundant source of pressurization source for RSVM space, which is hard to do with just one engine.

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 Post subject: Re: Cirrus SF50
PostPosted: 17 May 2016, 19:18 
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Username Protected wrote:
How come the TBM can go to 310 but the Cirrus will be held to 280 ?


Because Socata certified to 310. They certified before RVSM, which sets the practical limit at 280 unless you plan to go a lot higher.

Tim


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 Post subject: Re: Cirrus SF50
PostPosted: 17 May 2016, 19:25 
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Username Protected wrote:

That's a pretty slick looking airplane......has some Falcon 10 look to it, IMO, albeit, an "updated" Falcon 10...... :thumbup:


It's got those Swearingen lines. The tail is just a scaled up T-tail of the gorgeous little SX300 tail. Plane is certified, they're just doing amendment to the avionics I think, so should not take too long to get to market. Heard first flight mid 2016, and deliveries 2017.

Then again, this poor plane has had at least 3 different owners since it got certified, so who knows if it'll make it this time? At $7M it's pretty competitive, though. Fastest VLJ, longest range and it has SL cabin up to 41000ft. Nobody else can match that.

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Last edited on 17 May 2016, 19:34, edited 1 time in total.

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 Post subject: Re: Cirrus SF50
PostPosted: 17 May 2016, 19:28 
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Joined: 12/03/14
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Username Protected wrote:
What is a "personal jet"?

A small low cost economical jet.

Just being SP is not enough. A CJ4 is definitely not a "personal jet".

Mike C.

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 Post subject: Re: Cirrus SF50
PostPosted: 17 May 2016, 19:30 
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Username Protected wrote:
Forced - by whose hand. Better wording would be restricted or bounded "at this time"

Forced by the regulations.

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.

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 Post subject: Re: Cirrus SF50
PostPosted: 17 May 2016, 19:32 
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Username Protected wrote:
A small low cost economical jet.

Just being SP is not enough. A CJ4 is definitely not a "personal jet".

Mike C.

So how is the Eclipse not a "personal jet"?


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 Post subject: Re: Cirrus SF50
PostPosted: 17 May 2016, 19:36 
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Joined: 12/10/07
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Username Protected wrote:
How come the TBM can go to 310 but the Cirrus will be held to 280 ?


Wait, TBM can do 310? Wonder how they can do it without that second pressurization source Mike's been harping about.

:popcorn:


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 Post subject: Re: Cirrus SF50
PostPosted: 17 May 2016, 19:42 
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Username Protected wrote:
Mike, the fuel burn seems similar to a TBM 850 in high speed cruise

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.

Quote:
What is not impressive is the climb rate. I would expect at least 2,500-3,000 FPM in a personal jet.

Something's wrong with the climb rate. The simplest explanation is that the engine is not putting out the expected thrust.

Mike C.

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 Post subject: Re: Cirrus SF50
PostPosted: 17 May 2016, 19:44 
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Joined: 10/31/14
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Aircraft: eclipse
Username Protected wrote:
A small low cost economical jet.

Just being SP is not enough. A CJ4 is definitely not a "personal jet".

Mike C.

So how is the Eclipse not a "personal jet"?


Its because Mike can't figure out any system that's not Garmin. :shrug:

Still loving mine after almost 8 years.....

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 Post subject: Re: Cirrus SF50
PostPosted: 17 May 2016, 19:45 
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Username Protected wrote:
I consider my Mustang a very viable personal jet for me. There's ONE for you.

Yes, the Mustang qualifies.

But they made only 8 last year, 1 in 2016Q1, so not really being made in volume lately.

Mike C.

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 Post subject: Re: Cirrus SF50
PostPosted: 17 May 2016, 19:53 
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Username Protected wrote:
Wait, TBM can do 310? Wonder how they can do it without that second pressurization source Mike's been harping about.

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.


Note that the two grandfathered SETPs are both made in Europe, and the change was made based on European input, and now they can fly high and new designs can't.

Think about that.

Mike C.

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 Post subject: Re: Cirrus SF50
PostPosted: 17 May 2016, 19:57 
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Joined: 12/03/14
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Username Protected wrote:
we still don´t know if this data represents maximum ROC; probably not...

You think Cirrus purposefully publishes lame performance data?

I guess that is one coping method, hoping that is so.

Mike C.

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