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#31
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JS wrote:
Have not flown the DG800, just 300/500/600/1000. All those flew nicely. One thing I found out about the AS-W26 is that it's a BEAUTIFUL flying glider... Like an oversized 27, with perhaps an even more comfortable cockpit. Coordination seems perfect (it has a big enough rudder). Mine has the heavier wings (they'll chase your friends away unless you have a one-man rigger) but higher MGW and therefore higher maximum wing loading. The lower serial numbers are also certified Experimental in the USA, handy unless you're sending it overseas. The LONG trailer is going to get my "lift kit" mod, a 2" square steel tube between the axle and the trailer chassis. This helps with ground clearance and is hardly noticeable for rigging. I suggest you tow it around for a couple thousand miles before making any changes, as you might discover it's not so bad! I've towed my Cobra trailer behind our 23 foot motorhome (which has a moderate overhang) for 100,00+ miles all over the country. The hitch height is set so the trailer is slightly higher in the back(about 1"). The back end drags occasionally going in and out of parking lots and gas stations, but it doesn't harm the trailer because it's designed to accept that abuse. A vehicle with a shorter overhang, like a car, mini-van, or SUV, wouldn't drag it as often. I did finally wear out those little aluminum skids on the rear end this year, but replacements are on the way. -- Eric Greenwell - Washington State, USA Change "netto" to "net" to email me directly "Transponders in Sailplanes" on the Soaring Safety Foundation website www.soaringsafety.org/prevention/articles.html "A Guide to Self-launching Sailplane Operation" at www.motorglider.org |
#32
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Eric Greenwell wrote:
I suggest you tow it around for a couple thousand miles before making any changes, as you might discover it's not so bad! I've towed my Cobra trailer behind our 23 foot motorhome (which has a moderate overhang) for 100,00+ miles all over the country. The hitch height is set so the trailer is slightly higher in the back(about 1"). The back end drags occasionally going in and out of parking lots and gas stations, but it doesn't harm the trailer because it's designed to accept that abuse. A vehicle with a shorter overhang, like a car, mini-van, or SUV, wouldn't drag it as often. I did finally wear out those little aluminum skids on the rear end this year, but replacements are on the way. I've towed mine for a little over 1000km and I've dragged the skids somewhere each trip regardless of how careful I am about going over stuff diagonally. Even if it does it nowhere else, it does it on the drain at the entrance to the Club's field. ![]() I'm stuck with a fixed tow ball height so I think JS's suggestion is a good idea. GC |
#33
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"Gary Evans" wrote in message
... A couple of DG800 advantages that bumper overlooked. 1) An engine that doesn't cost $17000 to replace. 2) An engine that can be worked on with out having to remove it from the fuselage. While this may not seem like something you will ever have to do you'll want to keep a couple of big friends around for spark plugs changes. I believe there were at least three engines pulled for one problem or another at this years ASA Parowan camp. They also had their own cart to haul the engines around for repairs but I'm not sure if thats a standard 26 option. 3) A superior engine management system (DEI) with manual back up. IMO the engine related issues sum up the big difference between these two ships as performance both in glide and under power are way similar. The 26 has a smoother engine and the 800 has one, which is easier and cheaper to maintain. They are both state of the art ships and you won't be sorry for buying either. DG has done a pretty fair comparison between the 26/800/Ventus 2cM that can be viewed here - http://tinyurl.com/yz4shs Gary, I agree that performance wise they're essentially equal. On your other points: 1) The 17K figure may seem a lot, however, the need to completely replace one of these engines is quite rare. Replacing the Wankel's major engine parts costs around $8K Euro. Those few cases were this was necessary were most likely due to oil starvation and a Chernobyl type melt down. You do need to keep oil in the tank and pay attention to engine temperatures. Otherwise the Wankel, besides having small size which allows a narrow fuselage, has excellent power density and vibration free smoothness. The Wankel is also remarkably reliable and trouble free. The lack of vibration means that stuff doesn't crack, break or fall off the motor and things nearby - - a major positive attribute as compared to most 2-strokes. I heard that two of the 26E engines pulled at Parowan where to replace broken drive belts. This is an unusual occurrence, as the Wankel, with it's multiple smaller power pulses per revolution, is gentle to the drive train as compared to a 2-stroke. There was talk of a change in formulation used in manufacturing the Gates Poly-Chain drive belts. AFAIK, the reason for this breakage hasn't been 100% resolved/confirmed. I do know that some owners have 150 hours and more with no drive belt issues. For the whole 26E fleet, I'm aware of only the Parowan failures and one prior failure caused by a bearing failure in one of the guide pulleys. Belt failures have occurred on the 2-stroke powered ships as well, a backfire on start up will do the deed. 2) Yup, on my 26E the engine must be pulled to change plugs. There is a factory mod that provides an access hole to allow plug service without pulling the engine. It's retrofitable to my ship, but since I've never had to service the plugs, I don't plan on adding this mod. Besides, the engine package is easy enough to remove and can be done solo in about an hour (maybe half that with good help). Remove 3 bolts, 3 wiring cable plugs, a couple of Bowden cable connections (throttle and prop stop) and a fuel line. A "cherry picker" engine hoist is needed if removing the engine solo. I've only done this once in the 4 years and 23 engine hours I've had the ship, but plan on doing it for the next annual just to look at things. 3) When shopping, I considered DG's DEI engine control a plus, but after using the simple ILEC engine control, as used on the 26E and many other self-launch gliders, I'm not so sure. To put away the prop on the 26E: a- turn off ignition b- when prop stops, engage manual prop-stop lever (this swings a rubber stopper into the prop arc) and nose over slightly to windmill prop into stop as viewed in rear view mirror. c- push pylon switch down until prop just disappears from view in mirror (this is the cool down position), at thermalling speeds, the additional drag caused by the partially extended prop/radiator is minimal and still allows reasonable climb performance. d- In my ship, the cool down period takes 3 - 4 minutes. After observing a 2 C drop in engine coolant temp, push switch to retract prop fully. Simple, reliable, almost no maintenance required . . . even a cave man could do it. A DEI? Kind of like the automatic parking option on the new Lexus - - why bother? (g) I agree the most prominent mechanical difference between these two ships is the power train. I do not agree that the DG's 2-stroke engine is easier and cheaper to maintain. Given, replacing a 2-stroke engine is much less expensive than replacing the Wankel. However, this needs to be tempered by the fact that the Wankel will hardly need replacement if operated with reasonable care and its on-going maintenance is usually less expensive. After talking to Tom and Billy Stowers (High Country Soaring, and who have worked on all manner of these ships), my impression is that the 2-stroke maintenance issues they experience is an order of magnitude greater with 2-strokes than on the Wankel powered ships. This is also borne out by a check of the relevant AD's. The ASH26E has but two airworthiness directives (rotor cooling fan and muffler), both early-on teething problems that were resolved years ago. The many more subtle differences between the two ships are perhaps more subjective. I talked with Larry Mansberger about the "beneath the skin" differences between DG and Schleicher as I was not in a position to take a chain saw and see for myself. Keeping in mind that this was several years ago and the wing sections I saw were made prior to current DG factory ownership, the innards of the Schleicher wing looked to be assembled with the same care and attention to detail as the outer parts the customer normally sees - - not so inside the DG wing. Many of the DG's at Minden have gel-coat surface cracks on the wings, commonly around the spoiler boxes. I haven't seen this on Schleichers, though some earlier 26E's did show the wing spar profile after several years - - later versions, my 2002 model included, have not done this - so far. Subjectively, the 26E cockpit finish is nicer and ergonomics, even for taller pilots, is excellent. The DG's pigeon-toed rudder pedals, when I was trying it on, gave me foot cramps. I've asked several DG800 series owners, on the Minden ramp, why they chose the DG-800 series over the ASH26E. At the time, purchase cost was essentially the same for either ship and probably is still close. By a large margin the answer was availability, the delivery wait for the 26E then being two years, more than double that for the DG at the time. For one DG owner, the 800's two piece wing was a deciding factor (the 26E's one piece wing means the trailer must be longer, at about 35"). All that said, owners of both these ships seem happy with their decisions, and that's what really counts. My strong bias in favor of the ASH26E may well be indicative of a underlying personality flaw (g), I have little tolerance for things mechanical that could have, or should have, been done better. bumper |
#34
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In the Antares 20E, to extend and start the motor:
Push the power control forward. 10 seconds later you're under power. THATS ALL. To retract the motor: Pop up the little mirror Pull the power control back. For your entertainment, watch the prop step to vertical and disappear. Put away the little mirror. 15 seconds later you're clean. No cool-down cycle. No prop-stop fiddling. No multiple controls to operate. No priming fiddling or "automatic" primer flooding. No fussing with throttle setting to start. No fuel valve. No ignition switch to forget (laugh, but many times per year this happens). No starter button. No engine master switch. No extension/retraction controls. No backfires. No belt to break or adjust. No manual pnuematic input switching. No fun at all, eh ? See ya, Dave http://www.nadler.com PS: You can leave the little mirror out if that's still too complicated ! PPS: OK, its true, you do have to turn it on before you go flying. |
#35
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At 19:12 28 October 2006, Bumper wrote:
'Gary Evans' wrote in message ... A couple of DG800 advantages that bumper overlooked. 1) An engine that doesn't cost $17000 to replace. 2) An engine that can be worked on with out having to remove it from the fuselage. While this may not seem like something you will ever have to do you'll want to keep a couple of big friends around for spark plugs changes. I believe there were at least three engines pulled for one problem or another at this years ASA Parowan camp. They also had their own cart to haul the engines around for repairs but I'm not sure if thats a standard 26 option. 3) A superior engine management system (DEI) with manual back up. IMO the engine related issues sum up the big difference between these two ships as performance both in glide and under power are way similar. The 26 has a smoother engine and the 800 has one, which is easier and cheaper to maintain. They are both state of the art ships and you won't be sorry for buying either. DG has done a pretty fair comparison between the 26/800/Ventus 2cM that can be viewed here - http://tinyurl.com/yz4shs Gary, I agree that performance wise they're essentially equal. On your other points: 1) The 17K figure may seem a lot, however, the need to completely replace one of these engines is quite rare. Replacing the Wankel's major engine parts costs around $8K Euro. Those few cases were this was necessary were most likely due to oil starvation and a Chernobyl type melt down. You do need to keep oil in the tank and pay attention to engine temperatures. Otherwise the Wankel, besides having small size which allows a narrow fuselage, has excellent power density and vibration free smoothness. The Wankel is also remarkably reliable and trouble free. The lack of vibration means that stuff doesn't crack, break or fall off the motor and things nearby - - a major positive attribute as compared to most 2-strokes. I heard that two of the 26E engines pulled at Parowan where to replace broken drive belts. This is an unusual occurrence, as the Wankel, with it's multiple smaller power pulses per revolution, is gentle to the drive train as compared to a 2-stroke. There was talk of a change in formulation used in manufacturing the Gates Poly-Chain drive belts. AFAIK, the reason for this breakage hasn't been 100% resolved/confirmed. I do know that some owners have 150 hours and more with no drive belt issues. For the whole 26E fleet, I'm aware of only the Parowan failures and one prior failure caused by a bearing failure in one of the guide pulleys. Belt failures have occurred on the 2-stroke powered ships as well, a backfire on start up will do the deed. 2) Yup, on my 26E the engine must be pulled to change plugs. There is a factory mod that provides an access hole to allow plug service without pulling the engine. It's retrofitable to my ship, but since I've never had to service the plugs, I don't plan on adding this mod. Besides, the engine package is easy enough to remove and can be done solo in about an hour (maybe half that with good help). Remove 3 bolts, 3 wiring cable plugs, a couple of Bowden cable connections (throttle and prop stop) and a fuel line. A 'cherry picker' engine hoist is needed if removing the engine solo. I've only done this once in the 4 years and 23 engine hours I've had the ship, but plan on doing it for the next annual just to look at things. 3) When shopping, I considered DG's DEI engine control a plus, but after using the simple ILEC engine control, as used on the 26E and many other self-launch gliders, I'm not so sure. To put away the prop on the 26E: a- turn off ignition b- when prop stops, engage manual prop-stop lever (this swings a rubber stopper into the prop arc) and nose over slightly to windmill prop into stop as viewed in rear view mirror. c- push pylon switch down until prop just disappears from view in mirror (this is the cool down position), at thermalling speeds, the additional drag caused by the partially extended prop/radiator is minimal and still allows reasonable climb performance. d- In my ship, the cool down period takes 3 - 4 minutes. After observing a 2 C drop in engine coolant temp, push switch to retract prop fully. Simple, reliable, almost no maintenance required . . . even a cave man could do it. A DEI? Kind of like the automatic parking option on the new Lexus - - why bother? (g) I agree the most prominent mechanical difference between these two ships is the power train. I do not agree that the DG's 2-stroke engine is easier and cheaper to maintain. Given, replacing a 2-stroke engine is much less expensive than replacing the Wankel. However, this needs to be tempered by the fact that the Wankel will hardly need replacement if operated with reasonable care and its on-going maintenance is usually less expensive. After talking to Tom and Billy Stowers (High Country Soaring, and who have worked on all manner of these ships), my impression is that the 2-stroke maintenance issues they experience is an order of magnitude greater with 2-strokes than on the Wankel powered ships. This is also borne out by a check of the relevant AD's. The ASH26E has but two airworthiness directives (rotor cooling fan and muffler), both early-on teething problems that were resolved years ago. The many more subtle differences between the two ships are perhaps more subjective. I talked with Larry Mansberger about the 'beneath the skin' differences between DG and Schleicher as I was not in a position to take a chain saw and see for myself. Keeping in mind that this was several years ago and the wing sections I saw were made prior to current DG factory ownership, the innards of the Schleicher wing looked to be assembled with the same care and attention to detail as the outer parts the customer normally sees - - not so inside the DG wing. Many of the DG's at Minden have gel-coat surface cracks on the wings, commonly around the spoiler boxes. I haven't seen this on Schleichers, though some earlier 26E's did show the wing spar profile after several years - - later versions, my 2002 model included, have not done this - so far. Subjectively, the 26E cockpit finish is nicer and ergonomics, even for taller pilots, is excellent. The DG's pigeon-toed rudder pedals, when I was trying it on, gave me foot cramps. I've asked several DG800 series owners, on the Minden ramp, why they chose the DG-800 series over the ASH26E. At the time, purchase cost was essentially the same for either ship and probably is still close. By a large margin the answer was availability, the delivery wait for the 26E then being two years, more than double that for the DG at the time. For one DG owner, the 800's two piece wing was a deciding factor (the 26E's one piece wing means the trailer must be longer, at about 35'). All that said, owners of both these ships seem happy with their decisions, and that's what really counts. My strong bias in favor of the ASH26E may well be indicative of a underlying personality flaw (g), I have little tolerance for things mechanical that could have, or should have, been done better. bumper While the major 26 engine parts may cost $8k Euro a replacement engine can cost $17k US as one unhappy owner found out the hard way. I sure hope it isn't a common problem, because that would bankrupt a lot of people. I understand that a belt break which stops the water pump results in almost instant over heating which can fry the engine resulting in one of those big bills but as long as you constantly watch the temp gauge and keep one hand on the off switch that shouldn't be a big issue. When two belts break at the same meet however I would no longer call it an unusual occurrence. Interesting that DG's engine management system which automated the process beyond the 26 would be viewed as unnecessary like the parking option on the new Lexus. I guess that means that all development should have just stopped with the 26. Hmmm! Quote bumper ' My strong bias in favor of the ASH26E may well be indicative of a underlying personality flaw (g), I have little tolerance for things mechanical that could have, or should have, been done better.' I know for a fact that you have this flaw so it must have been especially painful when you realized there were so many areas for improvement in your 26. I'm sure Kemp was exaggerating when he said you've made 1000 changes but exactly how many changes have you made? Ps. As I said before IMO both of these ships are good choices but both have advantages and disadvantages. Were that not the case one of these two manufactures would have been out of business by now. You can measure how well DG is doing by the sales volume and innovations. I assume Schleicher is doing as well. You pay your money and take your choice. I do suggest interested buyers research beyond owners opinions as they (we) tend to be a tad biased as you may have noticed. |
#37
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One question from someone who will eventually have a self launcher
The Antares quote range in vertical metres it can climb, The ASH26 and DG808C have extra tanks that can increase range, What would be the climb height expected from say a normal tank of 15 litres for the ASH or DG . gary Andor Holtsmark wrote: At 04:30 22 October 2006, Roger wrote: So which one would you choose today? The Antares is much more expensive so that limits the market. I'd like to object to this comment. Before you decide on an aircraft (or make comments about their pricing), please get up to date offers for all brands you would concider, make sure that the offers include ALL the itimes you will need to operate the aircraft, then look at the BOTTOM line. The bottom line Antares pricing is competitive with similar infernal combustion based products. It must also be said that ALL sailplane manufacturers offer an amazing amount of product for the money they charge. There is a lot of idealism in the business. Anyway, if you are seriously interrested in an antares, then you are also more than welcome to make an appointment for a visit to Lange Flugzeugbau, including a test flight. Then you will know where the money goes. Contact information can be found at www.Lange-Flugzeugbau.com Cheers, Andor (yep, I work there) |
#38
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wrote:
One question from someone who will eventually have a self launcher The Antares quote range in vertical metres it can climb, The ASH26 and DG808C have extra tanks that can increase range, What would be the climb height expected from say a normal tank of 15 litres for the ASH or DG . gary Andor Holtsmark wrote: At 04:30 22 October 2006, Roger wrote: So which one would you choose today? The Antares is much more expensive so that limits the market. I'd like to object to this comment. Before you decide on an aircraft (or make comments about their pricing), please get up to date offers for all brands you would concider, make sure that the offers include ALL the itimes you will need to operate the aircraft, then look at the BOTTOM line. The bottom line Antares pricing is competitive with similar infernal combustion based products. It must also be said that ALL sailplane manufacturers offer an amazing amount of product for the money they charge. There is a lot of idealism in the business. Anyway, if you are seriously interrested in an antares, then you are also more than welcome to make an appointment for a visit to Lange Flugzeugbau, including a test flight. Then you will know where the money goes. Contact information can be found at www.Lange-Flugzeugbau.com Cheers, Andor (yep, I work there) Hi Gary - Unfortunately its a bit of apples and oranges. The Antares has no noticeable density-altitude penalty, so it can climb unaffected until around 16k where the prop speed-limits and the climb-rate slows (and you can't climb under power this high from sea-level). But, it has less range than a gas powered machine. A gas-powered machine may prove "interesting" at Ely or Telluride (without turbocharger), but has more range, especially with long-range tanks. Just don't expect to climb over some of the peaks out west when its hot. Its OK if you don't mind tooling around Ely after launch not real high until you find a thermal; certainly this is doable and plenty including me have done so. You have to pick which parameter is more important for your flying (and don't forget to include stress level as an independent and important parameter)... Hope this helps ! Best Regards, Dave PS: To emphasize Andor's point regarding cost, the all-up delivered and equipped cost of an Antares 20E is *not* substantially more than the other machines discussed here, make sure to compare the real total cost to your driveway... |
#39
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I may have missed it on this thread...but is the cost
of these things a secret? I can go to Ebay and price Ferraris and Maseratis..... Can we safely guess somewhere between $150k-$200k? Or put another way... a new selflauncher=towplane, 10 year old glider and hangar? |
#40
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![]() On Oct 28, 7:21 pm, wrote: A gas-powered machine may prove "interesting" at Ely or Telluride (without turbocharger), but has more range, especially with long-range tanks. Just don't expect to climb over some of the peaks out west when its hot. Its OK if you don't mind tooling around Ely after launch not real high until you find a thermal; certainly this is doable and plenty including me have done so. I operate my ASH-26E from an airport S of Denver that is at 7,000' MSL. During the summer, density altitude is 10K or so at the time I launch. The climb profile compared to a tow bekind a 250 HP Pawnee is quite similar. I'm climbing at about 50 knots and behind the Pawnee it would be 70 knots. So I'm actually higher about 1500' down the runway, but about the same at the end of the runway (about 200' AGL on this 3800' long runway) and typically 800' or so passsing abeam the departure point on downwind. Actual climb rate is about 300 fpm. Check my OLC flight logs for some comparisons as I sometimes take a tow in order to have a full fuel load for the end of the day. During the winter, I've still had a positive rate of climb at 16,500 while exploring for wave. In summer, I've made a few self retrieves from the other side of 13-14K' ridges in the Colorado Rockies. With the higher density altitude, I stop climbing at about 15K. I only have the fuselage tank (16 litres), so endurance is about 90 minutes. So the bottom line is that at high altitudes, either physically, or due to density, one must use whatever thermals there are, and try to avoid areas of sink. But so far, in the 5 years I've been flying the ship there has never been a situation where I wished for more power. -Tom ASH-26E 5Z Black Forest Soaring Society - for OLC logs |
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