![]() |
If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below. |
|
|
Thread Tools | Display Modes |
|
#1
|
|||
|
|||
![]() "C J Campbell" wrote in message ... "Thomas Borchert" wrote in message ... Mike, If you are prone to spinning airplanes during the turn from base to final in the pattern, please don't buy a Cirrus. Pleas don't buy ANY airplane, in that case. None are any more recoverable than the other. That is just plane silly (sorry). :-) Seriously, are you suggesting that roll rate and other maneuverability factors are equal in all airplanes? I am certain that it is possible to recover from even an inverted spin from 500 feet in some airplanes. I would bet that it is even possible in a Cessna 172. I haven't tried it, but in such a situation I would add rudder opposite the spin, push the yoke forward to break the stall, add power if not nose down and the engine is still running, otherwise reduce power until the nose comes up. Once the stall is broken then roll wings level and let the engine restart (it probably will quit if you are inverted). Of course, I would be miffed that I managed to get myself into a skidding base to final in the first place. No you are plane silly. I know how to spin. I like spins. I know how to recover. Just like the FAA, I slowly realized that spin recovery has little to do with spin danger for non acro operations. This past Saturday a pilot lost his life a few hundred yards from my house in a stall spin accident. Since the a/c was an extremely manueverable model, it entered the spin quickly. The fact that it occurred about 2 wingspans above the ground made recovery difficult. The point is *not spinning* in normal ops. |
#2
|
|||
|
|||
![]()
Maule Driver wrote:
This past Saturday a pilot lost his life a few hundred yards from my house in a stall spin accident. Since the a/c was an extremely manueverable model, it entered the spin quickly. The fact that it occurred about 2 wingspans above the ground made recovery difficult. Do you by any chance live at Lake Ridge Aero in North Carolina? This sounds a lot like an accident that happened there this past weekend. |
#3
|
|||
|
|||
![]()
C,
Yep, and all that in 500 ft. Nice of you to be on the forum, Superman. -- Thomas Borchert (EDDH) |
#4
|
|||
|
|||
![]()
I'm a newbie here but airplanenoise.com seems like its straight out of
Cessna's marketing department? I don't think I've ever seen such blatant self-serving product marketing dressed-up as ersatz objective analysis!! ....except maybe in the case of Bose Corporation. In the comparisons with every other aircraft make, the message is "Buy anything except a Cessna and you'll go broke on the way to killing yourself". That kind of message doesn't lend itself to much credence in my book. "C J Campbell" wrote in message ... This article pretty much describes the differences between the two airplanes and points up the issues that I have with the Cirrus. http://www.airplanenoise.com/article....%20Cirrus.pdf -- Christopher J. Campbell World Famous Flight Instructor Port Orchard, WA If you go around beating the Bush, don't complain if you rile the animals. |
#5
|
|||
|
|||
![]()
H.P. wrote:
I'm a newbie here but airplanenoise.com seems like its straight out of Cessna's marketing department? I don't think I've ever seen such blatant self-serving product marketing dressed-up as ersatz objective analysis!! ...except maybe in the case of Bose Corporation. In the comparisons with every other aircraft make, the message is "Buy anything except a Cessna and you'll go broke on the way to killing yourself". That kind of message doesn't lend itself to much credence in my book. True, but the most egregious error is that it fails to mention that real airplanes have the wing on top! :-) Matt |
#6
|
|||
|
|||
![]()
CJ,
Badly out of date, slanted piece. I'd suggest that one look to Aviation Consumer for a balanced look at the airplanes. On top of that, I can't see why one would compare the two airplanes as they are not targeted at the same market, given that one is turbocharged and one is normally aspirated. The turbo 182 is a superb airplane for the person who has a need to go high, otherwise it's far slower than the Cirrus, so the comparison isn't really accurate from that standpoint. What the heck is "special white paint"? The material I've seen indicates that the Cirrus has a white primary color with various accent colors available, just as is offered for the 182. While testing has indicated that even with black paint the airframe does not come close to exceeding the temperatures that might cause it to weaken, even when parked in the Sahara desert, the FAA has been extremely conservative in the certification of composites and calls for overall white paint. The article was in error in a number of places, while emergency egress is much better in the 182, it is not "impossible" in the SR20 and 22. As part of testing Cirrus inverted an SR20 with its smallest employee inside. She used the hammer that is standard equipment in the airplane, broke out a window and was out within seconds. The Cirrus has been spin tested, its recovery is conventional, as is the 182. Neither are certified for intentional spins. The Cirrus did not undergo the full regime of spin testing during original certification and thus the published recovery method for departure from controlled flight is to deploy the CAPS. The article does not mention handling at all. While I like flying the 182, the Cirrus is far, far nicer and more enjoyable to fly, with much more responsive handling. There was no comparison of crashworthiness where the 182 does well, the Cirrus does better because it has no yoke to hit, there is more "flail" space for the front seat occupants. There is also more rear seat room in the Cirrus, giving more "flail" space for those occupants. For minor damage, composites are easier to fix, hail tends to bounce off, where it dents aluminum. If there is actually hangar rash to a composite aircraft, you fix it by stirring up the epoxy, brushing it on and smoothing to match, then heating it with a hair dryer. If it's major damage, you replace the component. Aluminum is much more labor intensive with far more parts, so composite construction is cheaper and, due to the FARs, stronger than aluminum. At this point the insurers like aluminium better because something like a loss of control where the airplane goes up on a wingtip involves just repairing the wing, which is cheaper than the needed wing replacement on the composite airplane. I'm wondering who wrote up the article as the ground handling is quite comparable in the airplanes, the only place the castoring nosewheel can be a handful is pushing the airplane backwards into a hangar, something that is not a problem with the 182. Yes, a brake failure in a castoring nosewheel airplane tends to cause one to discover that taxiing is difficult if not impossible. The airframe life and engine TBO numbers for the Cirrus were wrong. I'm not sure I'd compare a turbocharged 182 to anything but another turbocharged airplane, so until GAMI and Tornado Alley turbonormalize a Cirrus, I would put this article in the dumper. All the best, Rick "C J Campbell" wrote in message ... This article pretty much describes the differences between the two airplanes and points up the issues that I have with the Cirrus. http://www.airplanenoise.com/article....%20Cirrus.pdf |
#7
|
|||
|
|||
![]()
C J Campbell wrote:
This article pretty much describes the differences between the two airplanes and points up the issues that I have with the Cirrus. http://www.airplanenoise.com/article....%20Cirrus.pdf It's telling that the article starts with flyover noise comparisons and prop clearance. It's a poorly done attempt at a smear and shouldn't be taken seriously by anyone with the ability to recognize obvious bias. I have no vested interest in either aircraft, although I instruct in both Cessna and Cirrus products. The Cirrus is an "interesting airplane," and overall the value for the average prospective owner (let's say, private pilot with an instrument rating) undergoing the average mission (regional travel, 100-300 hours of flight time per year) is just not there with the Cessna products anymore. Single-engine piston airplane sales trends reflect this. As a Cirrus Standardized Instructor, I have my own set of issues with the SR-20 and SR-22. The cited article barely hints at the real problems (which are NOT the chute or the composite airframe), and it reads much like it was written by a person who has flown neither aircraft. I believe that over time the Cirrus product will improve and flourish, while the Cessna line has been taken as far as it can go, G1000 or no. In summary, if you operate from short/unimproved fields, the Cirrus is not a realistic choice for you. If you want to rocket along at 180+ knots with a fairly advanced (although not overly redundant) avionics package, the SR-22 might fit you like a glove. Side note, the SR-22 is among the most spin-resistant airplanes on the market today. Spins in the SR are a red herring - think electrical system and avionics redundancy if you want to dive into the real can of worms. -Ryan |
#8
|
|||
|
|||
![]() "Ryan Ferguson" wrote in message om... C J Campbell wrote: This article pretty much describes the differences between the two airplanes and points up the issues that I have with the Cirrus. http://www.airplanenoise.com/article....%20Cirrus.pdf It's telling that the article starts with flyover noise comparisons and prop clearance. It's a poorly done attempt at a smear and shouldn't be taken seriously by anyone with the ability to recognize obvious bias. Have you seen the "Stop the Noise" thread? |
#9
|
|||
|
|||
![]()
Well, I wish it was a buying decision I expect to face...
CJC - I've always taken your posts seriously in the past. Will be difficult after that biased pile of dung. I hope you do work for Cessna - it's the only reasonable excuse. "C J Campbell" wrote in message ... This article pretty much describes the differences between the two airplanes and points up the issues that I have with the Cirrus. http://www.airplanenoise.com/article....%20Cirrus.pdf -- Christopher J. Campbell World Famous Flight Instructor Port Orchard, WA If you go around beating the Bush, don't complain if you rile the animals. |
#10
|
|||
|
|||
![]() "Maule Driver" wrote in message .com... Well, I wish it was a buying decision I expect to face... I wish it was, too. CJC - I've always taken your posts seriously in the past. Will be difficult after that biased pile of dung. I did not write the biased pile of dung. However, I think it is no more biased than Cirrus' advertising. I believe it brings up a serious number of legitimate issues. I hope you do work for Cessna - it's the only reasonable excuse. Most know that I work for a CSTAR, but not Cessna itself. Personally, I enjoyed flying the Diamond far more than I did the 182. I am also not yet convinced that the G-1000 (or any other flat panel display) is really worth the premium. It is pretty and I could get used to it, maybe even proficient with it, but how much additional utility do I get out of it? |
Thread Tools | |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
Cirrus for Duats | Charles | Piloting | 2 | July 17th 04 11:16 PM |
Cirrus SR22 Purchase advice needed. | C J Campbell | Piloting | 122 | May 10th 04 11:30 PM |
Cirrus attracting pilots with 'The Wrong Stuff'? | Jay Honeck | Piloting | 73 | May 1st 04 04:35 AM |
Cirrus report | Cub Driver | Piloting | 14 | April 30th 04 06:05 PM |
Cirrus Airframe Life Limits | Dave | Piloting | 16 | April 27th 04 05:58 PM |