Rob,
The only difference is that sitting in the mooney is like sitting in a sardines can. Not very useful for traveling with other poeple, as they only have 1 door.
Uhhhh, lots and lots of planes have one door. Heck airliners board through one door.
Rob,
The only difference is that sitting in the mooney is like sitting in a sardines can. Not very useful for traveling with other poeple, as they only have 1 door.
I may be wrong on that, but the 65 limit applies to aircraft that can show an equal level of safety for crash resistance at the higher speed.
80kts would mean coming over the fence at jet speeds in case of a flap or electrical failure. Not sure I would consider that a desireable characteristic. The record of hot-rods like the Lancair IVp that have to be flown that way is not that promising.
Hearing from people who shopped the later Mooneys new, their main problem was the death spiral and lack of capital. As their sales took a dip, they started to raise prices, and then sales went down faster, and so on. In the end, a G-36 was cheaper, just as fast, but more roomy and comfortable, with a better equipment, so the choice became a no-brainer.I love the looks of the Panthera, and the speed and efficiency targets seem encouraging... but then I remind myself about the (lack of) success Mooney's had lately offering aircraft with similar numbers.
Pipistrel's success is going to be determined in a large part by their ability to secure investment and find the right price.
I
As for the Panthera
One constraint for top speed in singles is the FAA mandated flaps up stall speed of 61kts.
Hearing from people who shopped the later Mooneys new, their main problem was the death spiral and lack of capital. As their sales took a dip, they started to raise prices, and then sales went down faster, and so on. In the end, a G-36 was cheaper, just as fast, but more roomy and comfortable, with a better equipment, so the choice became a no-brainer.
Pipistrel's success is going to be determined in a large part by their ability to secure investment and find the right price.
IAS or CAS?SR22 stalls between 68 and 70 with flaps up.
SR22 stalls between 68 and 70 with flaps up.
SR22 stalls between 68 and 70 with flaps up.
SR22 stalls between 68 and 70 with flaps up.
IAS or CAS?
Plane and Pilot found different numbers
http://www.planeandpilotmag.com/aircraft/specifications/cirrus/cirrus-sr22-g3.html
And we see how well that worked out given the number of RLOC accidents in Cirri.
Do not confuse poor business acumen with poor product or market performance.
Good point, of course.
When I first saw the Panthera in an article a few months back, I immediately thought "that reminds me of something" but I didn't click on the Mooney comparison until reading Paul Bertorelli's notes from Aero 2012, where he mentions the tight cabin.
A slick SEP, low-wing airframe maximized for efficiency and performance over cabin accommodations. Like the Mooney before it, I just don't see a wide market for such an aircraft, just a specific niche. I hope that's enough for Pipistrel to find success with the Panthera, because Heaven knows we need some variety out there!
One constraint for top speed in singles is the FAA mandated flaps up stall speed of 61kts.
As for the Panthera
Unless the slovenians have found some previously unknown aerodynamic principle, the Panthera will cruise <185ktas at 75%. The 204 number is going to be flat out and we know how realistic that is.
The FAR 23 stall speed requirement of 61 KCAS is for VS0 - flaps extended in the landing configuration, not flaps up.
(emphasis mine)That's the big thing. We rarely reward innovation these days. ......
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Plane and Pilot found different numbers
http://www.planeandpilotmag.com/aircraft/specifications/cirrus/cirrus-sr22-g3.html
My bad. It is flaps down.
Still, unless someone does something fancy like leading edge devices or multi-piece fowler flaps, the 61kts lower end puts creates somewhat of a limit for wing loading and top end speed. Look at the TBM, all flaps, tiny ailerons.
According to their own paperwork, there will be "possible delivery of some units in 2014, otherwise 2015". That's for the Experimental Build-it-yourself unit. The factory unit isn't expected to be available until "late 2015". Throw in some fudge-factor and certification bumps, and I'll bet we won't see this quite some time. And if I'm spending $400-$600K, you can be sure I'd want some serious service/support. Hey, at least they got a few years to grow a sales/service organization.
That's what I thought, until I found out that these guys have a two-seater that'll do 140 knots on 3 and change gallons per hour. They've also won lots of "green flight" awards. If anyone can do it, it's Pipistrel.