![]() |
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
|
|||
|
|||
![]()
Personally I think you are burying the hatchet deeply
for personal reasons, and I really believe you had no intention to buy this ship. That said, lets look at your list. Many of your suggestions are just common sense stuff, but many are tainted with your personal feelings. Item 2 is subjective at best. You may FEEL that all controls should be of the auto-hookup type, but that is not a certification requirement. Your opinion here is irrelevant........ Item 4 is subjective at best. The aircraft meets JAR 22. Item 5 is conjecture on your part. You are presupposng a failure mode not in evidence by inferring that it is problematic. Item 8 is patently incorrect. Carbon structures do not "store energy". Your description of the failure mode shows a lack of understanding of composite structures. Item 13 is again subjective. Properly assembled trailing edges do not delaminate regardless of their construction method. Your presupposition that fabric wrapped edges are superior is not based in fact, just an opinion you hold. Attempting to show one Trailing Edge construction method as superior to another again shows the limitations of your composite construction background. Item 15 is pure conjecture. You are asking that a JAR 22 aircraft manufacturer test for a condition that occurs only when a pilot makes an error and flys the aircraft incorrectly. IF this test was required, the conservative folks adninistering JAR 22 would see that it was added to the cert plan. YOU appear to be afraid of the small crosssection of the tail boom and seem to be inventing a reason to make it appear less than desirable. Item 17 is a prudent thought, but horribly skewed your personal perspective. You said the paint is too thin. Compared to what?? Is that viewpoint based on cosmetics or a by a MIL thickness check against the manufacturers recommended film thicknesses? I suspect you have no idea how much or little paint is needed for UV protection and what the finish requirements are.. Absent the specific resin used and the finish content, you are in no position to comment on UV protection issues. Yes you may FEEL the finish was "very thin", but in fact, that is your PERCEPTION, not a fact per se. I would hope that you would try to post facts on your site instead of opinions. It would be a nice change......... |
#2
|
|||
|
|||
![]()
pbc76049 wrote:
Item 4 is subjective at best. The aircraft meets JAR 22. I'm not aware of any standardized crash testing procedure for gliders, and if the the manufacturer of my ASH 26 E has knowledge of such tests, they haven't shared it with any of the customers I know. It would be wonderful if such data was available, but if you must have this data for any glider in production, I think you will have pay someone to do a crash test on it. Unless you are an engineer competent in composite design for crash protection, I don't think you will learn anything about the design by asking "where the Kevlar is". Item 5 is conjecture on your part. You are presupposng a failure mode not in evidence by inferring that it is problematic. I don't think any of the manufacturers test their gliders until they flutter, because it is very dangerous. The glider is likely to be so damaged or uncontrollable, the test pilot will have to parachute out of it. Certification requires testing to a certain speed beyond the Vne; above that, and you are a test pilot. If you want to "know what margin you will have when you are in an emergency" then you should fly so that your emergencies do not exceed Vne. Even if the manufacturer the exact flutter speed, he would be smart not to reveal that speed, for fear that pilots would then use that speed as the "real" Vne. Item 13 is again subjective. Properly assembled trailing edges do not delaminate regardless of their construction method. Your presupposition that fabric wrapped edges are superior is not based in fact, just an opinion you hold. Attempting to show one Trailing Edge construction method as superior to another again shows the limitations of your composite construction background. My ASH 26 E does not use fabric wrapped trailing edges, nor did my ASW 20, yet they both seem like fine machines. I would feel rather foolish telling Gerhard Waibel or Martin Heide the proper way to build a glider! It appears Neshe sets very high and very unusual standards for a glider. If I were a glider manufacturer, I would pray he became interested in some other manufacturer's glider. -- Change "netto" to "net" to email me directly Eric Greenwell Washington State USA |
#3
|
|||
|
|||
![]()
Hi Eric,
On Sun, 16 Oct 2005 20:48:49 -0700, Eric Greenwell wrote: Unless you are an engineer competent in composite design for crash protection, I don't think you will learn anything about the design by asking "where the Kevlar is". Well... extremely light weight of a fuselage definitely makes me wonder about crash protection - something Germany glider manufacturers have a lot of experience with. I think there's a good cause why their gliders are so heavy compared to the Diana 2. I don't think any of the manufacturers test their gliders until they flutter, because it is very dangerous. Wilhelm Dirks did that with the DG-600... ![]() Flutter testst are not performed inflight, but any aircraft needs to perform static flutter tests before it's certified in Germany (a very expensive thing to do - these tests are usually performed by Prfessor Niedbal). Even if the manufacturer the exact flutter speed, he would be smart not to reveal that speed, for fear that pilots would then use that speed as the "real" Vne. The design maximum speed is Vne + 15 percent - this is what the glider is designed for (and being flight-tested). Obviously this is the proven speed where no flutter occurs... at least in a perfectly maintained (prototype) glider. I certainly wouldn't risk to fly that fast... do you think that someone is so stupid to exceed Vne? I think most flutter cases happen at speeds between Va and Vne due to unexpected turbulence. Bye Andreas |
#4
|
|||
|
|||
![]()
At 12:00 16 October 2005, Ian Johnston wrote:
On Sat, 15 Oct 2005 16:38:08 UTC, Don Johnstone wrote: You have to be kidding. Whatever happened to 'the customer is always right'. It's a load of nonsense. No-one has a right to fly any aircraft. Ian What you say is absolutely true but on the other hand no-one is forced to buy it either. If the company do not sell aircraft they have failed in their aim and lets us be frank this company are not Schemp Hirth, DG-Flugzeugbau / Glaser-Dirks or Schleicher and do not have a track record of building excellent gliders. I would have thought that a company trying to sell a new glider would want to encourage sales but obviously my idea of business is outdated. What ever the rights and wrongs it does not seem to me that the manufacturers of the Diana 2 are going out of their way to encourage customers in fact I detect a certain arrogance in their approach. Building gliders does not make money, you actually have to sell them, and what does this debacle say about their likely after sales service I wonder. If someone who wanted to sell me a glider would not let me fly it I would certainly take my money elsewhere. |
#5
|
|||
|
|||
![]()
At 13:00 17 October 2005, Chester D wrote:
Stefan schreef: Alexander wrote: The testing customers were positively thrilled about the way Diana 2 is flying. Some feedback: the glider is easy to fly and also safe. None of the pilots (among them also competition pilots and instructors) could make the glider spin or stall completely. ... Mr Sharma said to me personally that he had only 200 hours and no experience on racing class gliders. Hmmm... Now, you must decide: Is that glider (15m!) 'easy and safe to fly' or do you need more than 200 hours to be able to handle it? Stefan There are plenty of glider pilots, even with 500 hours or more who can`t handle performance gliders. They can in common situations like a local flight but when in trouble the plane is too fast, too nervous, just too hard for them to handle. We are not talking open class here, the Diana is a 15 metre glider, unflapped with a claimed LD of 50. Nothing special about that except the performance so what is so difficult. I don't hear people saying that a Discus (1 or 2) LS8 or any of the Scheilcher gliders are anything but straightforward providing the pilot has received the proper training. One wonders what makes this glider so different from those marketed by the established manufacturers apart from the seeming determination of the makers to only sell to those they deem suitable. No wonder that gliding is in decline if it is so difficult to find someone who is prepared to treat customers as a valuable commodity. However good the product an uncaring and arrogant supplier will put me off every time. Most of those pilots know that themselves, others buy a glider and get scared in flight, few try to test-fly someone elses glider. Not the case here is it. |
#6
|
|||
|
|||
![]() "Don Johnstone" wrote in message We are not talking open class here, the Diana is a 15 metre glider, unflapped with a claimed LD of 50. Nothing special about that except the performance so what is so difficult. I don't hear people saying that a Discus (1 or 2) LS8 or any of the Scheilcher gliders are anything but straightforward providing the pilot has received the proper training. Heres the rub, you said proper training. The owner didn't let him fly. There are conflicting reports on flying ability. The owners, if they made a mistake, erred on the side of caution. TOTALLY UNDERSTANDABLE ACTIONS. The pilot who didn't fly is ****ed off and making a lot of noise about it. TOTALLY UNDERSTANDABLE ACTIONS. What I have a hard time with is the "tire kicker" rooting around and using his OPINIONS to slap around a sailplane. If he has technical issues of merit, he is doing us a favor by posting them, but as most here can see., he is acting childishly and with vindictiveness. I'm done here and hope everyone else is also.......... |
#7
|
|||
|
|||
![]()
At 20:06 17 October 2005, Ian Johnston wrote:
On Mon, 17 Oct 2005 10:09:02 UTC, Stefan wrote: Hmmm... Now, you must decide: Is that glider (15m!) 'easy and safe to fly' or do you need more than 200 hours to be able to handle it? 200 hours in 1250 flights is quite suggestive, don't you think? Ian Sorry, I don't get it. Suggestive of what? |
#8
|
|||
|
|||
![]()
On Mon, 17 Oct 2005 21:15:29 UTC, Don Johnstone
wrote: At 20:06 17 October 2005, Ian Johnston wrote: 200 hours in 1250 flights is quite suggestive, don't you think? Sorry, I don't get it. Suggestive of what? Quite a lot, really. 9 minutes 36 seconds per flight, on average. Ian |
#9
|
|||
|
|||
![]() "Don Johnstone" wrote in message ... At 20:06 17 October 2005, Ian Johnston wrote: On Mon, 17 Oct 2005 10:09:02 UTC, Stefan wrote: Hmmm... Now, you must decide: Is that glider (15m!) 'easy and safe to fly' or do you need more than 200 hours to be able to handle it? 200 hours in 1250 flights is quite suggestive, don't you think? Ian Sorry, I don't get it. Suggestive of what? An Air Cadet ? |
#10
|
|||
|
|||
![]()
At 14:12 17 October 2005, Don Johnstone wrote:
We are not talking open class here, the Diana is a 15 metre glider, unflapped with a claimed LD of 50. Nothing special about that except the performance so what is so difficult. I don't hear people saying that a Discus (1 or 2) LS8 or any of the Scheilcher gliders are anything but straightforward providing the pilot has received the proper training. Don get your basic facts right matey - Diana is a FLAPPED 15m glider!! |
Thread Tools | |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
AOPA Stall/Spin Study -- Stowell's Review (8,000 words) | Rich Stowell | Aerobatics | 28 | January 2nd 09 02:26 PM |
ramifications of new TSA rules on all non-US and US citizen pilots | paul k. sanchez | Piloting | 19 | September 27th 04 11:49 PM |
PC flight simulators | Bjørnar Bolsøy | Military Aviation | 178 | December 14th 03 12:14 PM |
12 Dec 2003 - Today’s Military, Veteran, War and National Security News | Otis Willie | Naval Aviation | 0 | December 12th 03 11:01 PM |
AOPA Stall/Spin Study -- Stowell's Review (8,000 words) | Rich Stowell | Piloting | 25 | September 11th 03 01:27 PM |