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 Post subject: Re: Cirrus SF50
PostPosted: 13 May 2016, 10:50 
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Joined: 01/31/09
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Location: Northern NJ
Aircraft: SR22;CJ2+;C510
Username Protected wrote:
I may be taller and clumsier than the average pilot (ok, I am) but I find cockpit access a misery in most turbines. I would love to appear at the Society of Pedestal Designers annual conference and tell them just what I think of them.


Have you sat in a Mustang, M2 or CJ3+?

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Allen


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 Post subject: Re: Cirrus SF50
PostPosted: 13 May 2016, 11:56 
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Joined: 05/23/08
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Location: CMB7, Ottawa, Canada
Aircraft: TBM - C185 - T206
I sat in those 3 and they are comfortable and easy to get in. Im 6' 2".


Username Protected wrote:
I may be taller and clumsier than the average pilot (ok, I am) but I find cockpit access a misery in most turbines. I would love to appear at the Society of Pedestal Designers annual conference and tell them just what I think of them.


Have you sat in a Mustang, M2 or CJ3+?

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Former Baron 58 owner.
Pistons engines are for tractors.

Marc Bourdon


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 Post subject: Re: Cirrus SF50
PostPosted: 13 May 2016, 13:30 
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Joined: 03/06/13
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Location: UK
Aircraft: C90XP
Username Protected wrote:
Have you sat in a Mustang, M2 or CJ3+?


I've flown a Mustang once, and loved it. Cockpit access is great, and I loved the 3point inertia reel car-style pilot seatbelt. I did say "most turbines"! TBMs are reasonable too.
I've sat in the co-pilot seat of a Cessna demo M2. I struggled to get in and out, but even worse, I couldn't fly it. The angled base of the panel was digging into my knees at full seat travel (I understand their are options for greater seat travel). Oddly, I don't remember much trouble getting into a CJ though.
PC12 was a misery. I literally couldn't figure how to get out of the pilot seat without my shoe hitting avionics or switches - it was a sort of human puzzle that took some figuring out.
Our C90 has a narrow pedestal. I hate the double width pedestal on later KAs.

I am 6'4" but I've flown most of the common piston types with no problem. My reaction to the SF50 was getting into the cockpit at an Exhibition after sitting in the M2, PC12 and King Air 250. The SF50 cabin is nice and modern in a way that some $m turbines aren't.

I also have a thing that I rarely buckle myself into the pilots seat without forgetting something and having to go back...


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 Post subject: Re: Cirrus SF50
PostPosted: 13 May 2016, 14:19 
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Joined: 11/06/10
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Username Protected wrote:
I also have a thing that I rarely buckle myself into the pilots seat without forgetting something and having to go back...


That right there is why I will never get a plane with only one door that is not the pilots door. :)

Tim


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 Post subject: Re: Cirrus SF50
PostPosted: 13 May 2016, 14:25 
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That right there is why I will never get a plane with only one door that is not the pilots door. :)

Tim


That is very limiting if you want to get into a pressurized aircraft.

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 Post subject: Re: Cirrus SF50
PostPosted: 13 May 2016, 16:26 
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Username Protected wrote:

That right there is why I will never get a plane with only one door that is not the pilots door. :)

Tim


That is very limiting if you want to get into a pressurized aircraft.


I am not going pressurized, at this point.
If I need to go faster/higher I likely would so I would go back to the Aerostar, or jump to a jet. Although I do not have the mission requirements; the incremental cost for most of the turboprops over the Aerostar are not worth the cost differential. (Think 3-4 people for the next 5-10 years, then two people for most flights.) It would likely make more sense to jump to a small jet, e.g. Mustang, Eclipse....

Tim

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 Post subject: Re: Cirrus SF50
PostPosted: 14 May 2016, 01:55 
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Joined: 12/03/14
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Company: Ciholas, Inc
Location: KEHR
Aircraft: C560V
Cirrus released a new flight profile, starting at airport elevation of 2000 ft, ISA+10, cruising at 17,000 ft, starting weight 5000 lbs (~1000 lbs under gross).

Ground takeoff roll is listed as 2408 ft. I thought that was very poor to be rolling on the ground for almost half a mile to get to liftoff.

The balanced field length for a Citation SII is 2660 ft under the same conditions (using same % of gross weight, which is 12,500 lbs), and this is accelerate to V1, engine fail, and stop, not just to liftoff.

Time to climb from 2000 ft to 17,000 ft is listed as 11 minutes, or an average of 1,360 FPM. Note that this is at 1000 lbs UNDER GROSS! That is very underwhelming. To put it in perspective, the SR22 climb rate is about the same (albeit at 0 MSL and ISA).

Cruise figures at 17,000 ft are:

MCT 283 KTAS, 84 GPH, 3.37 nm/gal

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

Obviously 17,000 ft is a bad altitude for a jet and those figures demonstrate that clearly.

Total landing distance (ground roll?) with max flaps is listed as 2658 ft. Not clear what the landing weight is, perhaps still the 5000 lbs.

The numbers are so bad, I wonder if the person making this document made errors. Is the climb rate at ISA+10 and 1000 lbs under gross REALLY that bad?

Mike C.

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 Post subject: Re: Cirrus SF50
PostPosted: 14 May 2016, 03:53 
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Username Protected wrote:
:bugeye: LOOK SQUIRREL!!!!

Pilots and A.D.D. they just go together!


Back at 'ya dude ! :bow:

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 Post subject: Re: Cirrus SF50
PostPosted: 14 May 2016, 07:47 
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Joined: 03/09/13
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Location: Byron Bay,NSW Australia
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The numbers are so bad, I wonder if the person making this document made errors. Is the climb rate at ISA+10 and 1000 lbs under gross REALLY that bad?

Mike C.


Hard to believe any one but the marketing department is involved at this point in time. From history this is as good as it gets :D

Andrew


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 Post subject: Re: Cirrus SF50
PostPosted: 14 May 2016, 07:57 
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Username Protected wrote:
Cirrus released a new flight profile, starting at airport elevation of 2000 ft, ISA+10, cruising at 17,000 ft, starting weight 5000 lbs (~1000 lbs under gross).

Ground takeoff roll is listed as 2408 ft. I thought that was very poor to be rolling on the ground for almost half a mile to get to liftoff.

The balanced field length for a Citation SII is 2660 ft under the same conditions (using same % of gross weight, which is 12,500 lbs), and this is accelerate to V1, engine fail, and stop, not just to liftoff.

Time to climb from 2000 ft to 17,000 ft is listed as 11 minutes, or an average of 1,360 FPM. Note that this is at 1000 lbs UNDER GROSS! That is very underwhelming. To put it in perspective, the SR22 climb rate is about the same (albeit at 0 MSL and ISA).

Cruise figures at 17,000 ft are:

MCT 283 KTAS, 84 GPH, 3.37 nm/gal

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

Obviously 17,000 ft is a bad altitude for a jet and those figures demonstrate that clearly.

Total landing distance (ground roll?) with max flaps is listed as 2658 ft. Not clear what the landing weight is, perhaps still the 5000 lbs.

The numbers are so bad, I wonder if the person making this document made errors. Is the climb rate at ISA+10 and 1000 lbs under gross REALLY that bad?

Mike C.


With the current price of Jet A, the cost per NM at LRC is cheaper and faster than most turbo'd pistons at 17K - which is worst case scenario for the jet. So your post tells me VFR direct departures, avoiding DPs and STARs, are feasible which will make this jet "faster" by default. If you get stuck at 17K for a couple of minutes waiting for a clearance, its NBD. If you get dropped early on arrival, cancel below 180 and go direct.

Is there a link to the chart you are quoting Mike?
-----------
Avgas 4NM/$4.00

JetA 4NM/2.50

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 Post subject: Re: Cirrus SF50
PostPosted: 14 May 2016, 08:09 
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Joined: 11/07/11
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Location: KBED, KCRE
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Does an SR22 really climb at 1300fpm to 17,000? Impressive.

Chip-


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 Post subject: Re: Cirrus SF50
PostPosted: 14 May 2016, 08:20 
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Joined: 01/29/08
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Username Protected wrote:
Does an SR22 really climb at 1300fpm to 17,000? Impressive.

Chip-

My TN Bonanza did close to that.


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 Post subject: Re: Cirrus SF50
PostPosted: 14 May 2016, 09:04 
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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:
Does an SR22 really climb at 1300fpm to 17,000? Impressive.

Chip-

No, not even close.
Neither will the 421 at a reasonable airspeed.

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 Post subject: Re: Cirrus SF50
PostPosted: 14 May 2016, 09:07 
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Company: CSRA Document Solutions
Location: Aiken, SC KAIK
I was having a hard time understanding why this discussion is so polarizing and then it became apparent it all depends on what lenses you're looking through...

If you're a piston driver with short missions - like a lot of the current Cirrus fleet - this light jet looks quite appealing, higher, faster, more automation, parachute, and new.

If you're a jet-a driver you see it's shortcoming comparable to the "jet" and "TP" marketplace.

Both positions have their merit and I can see why the legacy CJ type marketplace will remain strong and is not a real competitor to the SF50.

Different strokes for different folks.....

****thread drift alert*****

If you could see what's parked on the ramp at KAIK right now you'd be blown away. These guys are in town and there catering bills are more than my annual operating budget....

http://viewfromthewing.boardingarea.com ... xecutives/

G5's are passé with this crowd. Falcon 7X's are more the norm...

Peace,
Don


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 Post subject: Re: Cirrus SF50
PostPosted: 14 May 2016, 09:24 
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Joined: 05/23/08
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Location: CMB7, Ottawa, Canada
Aircraft: TBM - C185 - T206
Wow these numbers are bad, nobody buys a jet to go slow or fly at LRC.
11min to get to 17000 ft? :scratch:

That cant be right.

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Former Baron 58 owner.
Pistons engines are for tractors.

Marc Bourdon


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