11 Jan 2026, 04:27 [ UTC - 5; DST ]
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Post subject: Re: Cirrus SF50 Posted: 08 Dec 2014, 10:48 |
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Joined: 12/03/14 Posts: 21019 Post Likes: +26487 Company: Ciholas, Inc Location: KEHR
Aircraft: C560V
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Username Protected wrote: They are, in fact, going to build it. When/if they get to that phase, that is when the SF50 will be the greatest strain on the company. They then have a large block of early customers who bought the airplane below cost. The faster they make them, the more money they lose, and now it is real money they have to send to vendors for parts. This is what did in Eclipse more than anything else, actually building the airplanes. Quote: We'll know in 12 months more or less. No, we won't. There's no way the SF50 deliveries start in 12 months. It took 3 years after the conforming EA500s flew before deliveries. Mike C.
_________________ Email mikec (at) ciholas.com
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Post subject: Re: Cirrus SF50 Posted: 08 Dec 2014, 10:48 |
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Joined: 08/25/13 Posts: 615 Post Likes: +128
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Username Protected wrote: "Probable" leaves a lot of wiggle room. Actually, it doesn't. It is a very precise term in FAA certification language. "Probable" means a failure that would occur, on average, 1 or more times during the entire operational life of each airplane. Mathematically, the FAA deems this to be a 1 in 10^5 hours chance, or one occurrence every 10,000 hours of flight. Window failure: not probable. Engine shutdown: probable. Mike C.
And considering that even a lowly piston anymore only has a 1 in 40,000 hours statistical chance of shutdown, your reasoning in regards to a turboprop/jet engine is incorrect. Same with applying the recent TBM accident. That engine kept on running. Something else failed, probably not even related to the bleed air pickup. I am not disagreeing with majority of your points, however, with enough time and money, you can certify anything. Might not be cheaper in the long run, like you pointed out, but can be done.
A turbo prop/jet engine failure would be considered "improbable". Current stats on the PT6 are 1 in 200,000 hours to 1 in 500,000 depending on model.
Last edited on 08 Dec 2014, 10:52, edited 2 times in total.
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Post subject: Re: Cirrus SF50 Posted: 08 Dec 2014, 10:50 |
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Joined: 01/29/08 Posts: 26338 Post Likes: +13087 Location: Walterboro, SC. KRBW
Aircraft: PC12NG
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Username Protected wrote: No, we won't. There's no way the SF50 deliveries start in 12 months.
It took 3 years after the conforming EA500s flew before deliveries.
Mike C. My buddy owns a Cirrus charter/fractional company. He says 12 months and has delivery slots. I think it's unlikely too but we shall see.
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Post subject: Re: Cirrus SF50 Posted: 08 Dec 2014, 10:56 |
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Joined: 12/03/14 Posts: 21019 Post Likes: +26487 Company: Ciholas, Inc Location: KEHR
Aircraft: C560V
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Username Protected wrote: Even in this example, clearly during a high traffic time in NYC, the flight was above 30K 58% of the time, and about 75% of the distance. Being able to fly high provided significant advantage even on this flight. You have to consider that most of the distance was covered at high altitude even if the time was nearly balanced. Mike C.
_________________ Email mikec (at) ciholas.com
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Post subject: Re: Cirrus SF50 Posted: 08 Dec 2014, 11:16 |
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Joined: 12/03/14 Posts: 21019 Post Likes: +26487 Company: Ciholas, Inc Location: KEHR
Aircraft: C560V
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Username Protected wrote: And considering that even a lowly piston anymore only has a 1 in 40,000 hours statistical chance of shutdown Those numbers are for "failures", the engine broke. Engines shutdown for a lot of other reasons. Pilot error, fuel exhaustion, fuel system failure, ice ingestion, bird/fod ingestion, etc. In any case, the FAA has always defined engine failure as probable. Mike C.
_________________ Email mikec (at) ciholas.com
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Post subject: Re: Cirrus SF50 Posted: 08 Dec 2014, 11:28 |
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Joined: 08/25/13 Posts: 615 Post Likes: +128
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Username Protected wrote: And considering that even a lowly piston anymore only has a 1 in 40,000 hours statistical chance of shutdown Those numbers are for "failures", the engine broke. Engines shutdown for a lot of other reasons. Pilot error, fuel exhaustion, fuel system failure, ice ingestion, bird/fod ingestion, etc. In any case, the FAA has always defined engine failure as probable. Mike C.
Ok, now you're just being silly Fuel exhaustion is going to shut down both engines, so will fuel system failure, ice ingestion and I've yet to see a bird/FOD over FL250. Like I said, the way you read it, the FAR section is impossible to comply with, with any number of engines.
First you state 1 in 10,000. Then it becomes any possibility.
You will be proven wrong with the next SETP that gets certified, and there will be another one eventually.
Anyways, done. The Cirrus Jet will happen. It will sell. It will eventually get certified higher, and your original point of contention, RVSM, isn't even an issue. The avionics package is already RVSM certified. Whether it will continue to sell after the initial wave, is a whole another question. Back to work so I can afford to feed my PT6s and my Continentals…
Probable != Possible
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Post subject: Re: Cirrus SF50 Posted: 08 Dec 2014, 11:54 |
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Joined: 05/17/11 Posts: 1878 Post Likes: +1322 Location: KFRG
Aircraft: 421C
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Username Protected wrote: Hey Mike. I think that after 39 posts on the subject, we understand that you think building a SEJ is a bad idea, destined to fail.
The SF50 is a SEJ. I believe it's too late for you to save Cirrus.
Can we move on with life now? I haven't read where Mike has attacked anybody personally. I have seen Mike lay out some arguments that seem fact based. Not sure why we would want to try to kill the thread unless it's purpose is just a "feel good" thread for everything positive about Cirrus. People can choose to read or not...
Agreed... as I posted yesterday, I find this thread very interesting and have no idea why people would suggest someone stop posting?!
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Post subject: Re: Cirrus SF50 Posted: 08 Dec 2014, 12:47 |
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Joined: 01/11/10 Posts: 3833 Post Likes: +4140 Location: (KADS) Dallas, TX
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Username Protected wrote: They are, in fact, going to build it. When/if they get to that phase, that is when the SF50 will be the greatest strain on the company. They then have a large block of early customers who bought the airplane below cost. The faster they make them, the more money they lose, and now it is real money they have to send to vendors for parts. This is what did in Eclipse more than anything else, actually building the airplanes. Quote: We'll know in 12 months more or less. No, we won't. There's no way the SF50 deliveries start in 12 months. It took 3 years after the conforming EA500s flew before deliveries. Mike C.
How do you know they are selling below cost? How do you know the delivery schedule? Because the EA500's took longer? Can we really compare two different companies? They sure knocked out some major changes to the SR22 without missing a beat. Is it even remotely possible to you that they know something about aircraft manufacturing?
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Post subject: Re: Cirrus SF50 Posted: 08 Dec 2014, 13:07 |
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Joined: 08/21/14 Posts: 185 Post Likes: +119
Aircraft: C33A, Challenger 604
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Username Protected wrote: I'm not sure why you're being so difficult. What's your motive?
We're discussing how ATC dictates altitude and speed on most of my routes and therefore a jet did not make sense for me. Flights into TEB are brought down low early to stay out of JFK, LGA, etc.. That's the only point I'm trying to make. This will be the case with any single pilot airplane.
Telling me to post a pic of a PC12 at 410 is not moving the discussion forward. I'm not trying to be difficult, I'm trying to be factual. You made some statements that were spoken in such a way that it looked like you knew what you were talking about. For example, for the trip between PDK & NYC airplanes won't get above FL210. Or, the CJ that was referenced via Flightaware flew "the exact same route and altitude" as you'd fly in your PC-12. Others and myself easily proved your statements to not be factual. You're clearly one of the more respected and trusted forum members. People look to members like yourself as a source of accurate information, and often blindly trust it. As such, when incorrect info is spoken, I believe it's important that the information be cleared up so as to avoid confusion now or in the future when the topic is read. I hope that you now have a better understanding of my motive. I simply want to do my part to be sure that accurate info is available; not hearsay.
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Post subject: Re: Cirrus SF50 Posted: 08 Dec 2014, 14:25 |
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Joined: 11/09/13 Posts: 1910 Post Likes: +927 Location: KCMA
Aircraft: Aero Commander 980
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Username Protected wrote: I don't think a window is part of the pressurization system. If it was then the wing, tail, fuselage, door would also be part of pressurization. You certainly need those components to have a pressurized airplane but you also need fuel and oil! They have no intention of trying to meet the requirement. They are well on the final certification process with the sub RVSM limit. Why are you guys arguing about things that don't matter?
I was responding to a question as I am now!
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Post subject: Re: Cirrus SF50 Posted: 08 Dec 2014, 14:49 |
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Joined: 02/14/08 Posts: 3133 Post Likes: +2674 Location: KGBR
Aircraft: D50
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You want to compare Eclipse to Cirrus, the most successful new aircraft manufacturer in years? The company that straight out dominates the markets it competes in? I don't get it. And you think the chute doesn't matter? 
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Post subject: Re: Cirrus SF50 Posted: 08 Dec 2014, 15:38 |
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Joined: 11/06/10 Posts: 12201 Post Likes: +3086 Company: Looking Location: Outside Boston, or some hotel somewhere
Aircraft: None
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Username Protected wrote: A chute matters in that it will change peoples risk management. This is like the twin vs single debate. Beatin like a dead pony!  My wife was afraid of flying, what first got her to fly with me was the chute in the SR20 I used to fly. A cute or a second engine I view as required equipment for night IMC flying, and since I like to fly at night.... But you are correct, it comes down to risk mitigation. If I end up flying a plane without a chute or a second engine, I am gonna be flying during the day and avoiding most low IMC. Tim
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Post subject: Re: Cirrus SF50 Posted: 08 Dec 2014, 16:21 |
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Joined: 08/05/11 Posts: 5248 Post Likes: +2426
Aircraft: BE-55
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Username Protected wrote: Hey Mike. I think that after 39 posts on the subject, we understand that you think building a SEJ is a bad idea, destined to fail.
The SF50 is a SEJ. I believe it's too late for you to save Cirrus.
Can we move on with life now? I haven't read where Mike has attacked anybody personally. I have seen Mike lay out some arguments that seem fact based. Not sure why we would want to try to kill the thread unless it's purpose is just a "feel good" thread for everything positive about Cirrus. People can choose to read or not...
+1000
Nice to have a different knowledge base coming to BT. Just Seems like he's assaulting the "status quo". I like it because it's progress rather than "stasis".
_________________ “ Embrace the Suck”
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Post subject: Re: Cirrus SF50 Posted: 08 Dec 2014, 16:47 |
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Joined: 02/14/08 Posts: 3133 Post Likes: +2674 Location: KGBR
Aircraft: D50
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Username Protected wrote: A chute matters in that it will change peoples risk management. This is like the twin vs single debate. Beatin like a dead pony!  The chute matters because of how it affects sales. Mike C. said he doesn't think the chute matters in regards to sales. I beg to differ.
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