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06 Jun 2025, 15:13 [ UTC - 5; DST ]


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 Post subject: Re: Twin Turboprop Safety Analysis
PostPosted: 28 Dec 2014, 01:02 
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In my mind, its major "fault" is being high performance, does everything fast so pilots can be behind the airplane.

With performance comes responsibility.

Mike C.


Mike,

This is what you have missed about SF50 the whole time in all your posts. Nothing will happen in the SF50 much faster than it happens in SR22. At least not when it matters, as in take off and landing. People don't get behind during cruise. This is the major reason why SETP are so popular with owner pilots. This is why SF50 will be as popular. 80knot approach speed. It will be popular precisely because it is not a high performance airplane. It will actually be even easier to fly than a SR22 because of FADEC.


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 Post subject: Re: Twin Turboprop Safety Analysis
PostPosted: 28 Dec 2014, 01:08 
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Joined: 07/30/12
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Company: Aerlogix, Jet Aeronautical
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I agree with this ^^^^ for the most part. The ability of the plane to get from 140 down to 80 kts will dictate its safety record IMO. Piston/turboprop guys have no issues losing airspeed on final with the props, but the jet makes that phase of flying much more critical. I can't wait to fly one! :thumbup:


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 Post subject: Re: Twin Turboprop Safety Analysis
PostPosted: 28 Dec 2014, 02:06 
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They maintain a database of Hobbs hours by serial number. Data comes from several sources, usually warranty cards in the first 3-5 years of operation, airworthiness directive compliance cards over the life of the aircraft, service bulletins when kits are ordered, and parachute repacks. Occasionally, Cirrus will certify a used aircraft and start a new warranty, so they get data on such older aircraft.

This method does not catch all Cirrus aircraft.

I suspect, but can't prove, those aircraft that are missing are going to average fewer flight hours.

Quote:
BTW, they have data for about 75% of the fleet.

So 25% are missing.

Of the 75%, some of the data could be years old, as well.

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As you correctly pointed out, in the 2011 era, a major correction in that distribution was made.

I don't understand. You supposedly had the data prior to 2011, so why the correction? Which distribution is more truthful?

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Since those planes were all 10 years old, it indicated that the first 3-5 years under warranty, the planes flew on average about 225 hours per year, while in the next six years, the planes flew only about 500 hours, or about 83 hours per year. Quite a difference.

Yes, I believe this drop off after a few years to be quite typical.

Quote:
Then we started seeing some interesting shifts. As used Cirrus aircraft were sold after repacks, their usage became much closer to new aircraft in their first 3-5 years. This suggests that owner/operators of new-to-them Cirrus aircraft fly them a lot.

So do you assume repacked Cirrus fly 225 hours a year?

Or do you assume newly purchased used Cirrus fly 225 hours a year regardless of chute repack?

The chute repack is a normal maintenance function. I don't see how it causes triple usage for the next 3-5 years.

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See this wiki page for details: Cirrus Accident Rates

950K hours in 12 months on 5600 airframes is 170 hours each. Seems high. For every 80 hour airframe, you have to have one flying 260 hours. Even if people do that the first 3 years, most planes are now older than that.

Here is the fundamental problem with your method. At the end, you compare the accident rate of Cirrus, computed using the "new" fleet hours you compute using the new formulas since 2011, with other aircraft using no similar method to compute fleet hours.

So your accident rate numbers are not computed in the same way as the FAA numbers so they should not be compared against each other.

Your number MAY be more accurate, but the issue is treating both sides equally.

Mike C.

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 Post subject: Re: Twin Turboprop Safety Analysis
PostPosted: 28 Dec 2014, 06:02 
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...fascinating discussion here about twin turboprop safety.. :duck:

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 Post subject: Re: Twin Turboprop Safety Analysis
PostPosted: 28 Dec 2014, 09:23 
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...fascinating discussion here about twin turboprop safety.. :duck:

+1 :peace: Image


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 Post subject: Re: Twin Turboprop Safety Analysis
PostPosted: 28 Dec 2014, 12:04 
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Nothing will happen in the SF50 much faster than it happens in SR22. At least not when it matters, as in take off and landing.

I thought that too before I moved up to my Mits. But it turns out that by far the busiest time in my cockpit due to the performance is just after takeoff - departure climb. You are climbing at 2000fpm or better at 180 KIAS and getting vectors or whatever with rapid handoffs to the next controller, etc. Re-routes to initial fixes or airways are not uncommon.

I have never noticed landing speed as any kind of issue flying high performance aircraft, it's the departure.

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