Lightning-List Digest Archive

Tue 08/22/06


Total Messages Posted: 8



Today's Message Index:
----------------------
 
     1. 12:13 AM - Lightning Pilot Report Repost (Brian Whittingham)
     2. 12:13 AM - 5/8 bolts (Tex Mantell)
     3. 12:23 AM - Re: Re: RV-9A v. Lightening (Pete)
     4. 12:25 AM - Re: Re: RV-9A v. Lightening (Brian Whittingham)
     5. 03:38 AM - Re: 5/8 bolts (Kayberg@AOL.COM)
     6. 11:49 AM - Re: 5/8 bolts (nick otterback)
     7. 08:03 PM - Re: Lightning Cargo Capacity Questions (N1BZRich@AOL.COM)
     8. 11:01 PM - Re: Lightning Cargo Capacity Questions (Daniel Vandenberg)
 
 
 


Message 1


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    Time: 12:13:27 AM PST US
    From: "Brian Whittingham" <dashvii@hotmail.com>
    Subject: Lightning Pilot Report Repost
    --> Lightning-List message posted by: "Brian Whittingham" <dashvii@hotmail.com> Ok, I'll bite. I've got several hours in the Lightning now. Hopefully this won't bore all of you and I'll try not to be too technical. Let me start with a little history on the Lightning. The Lightning was developed around the same idea as the Esqual, a light, fast, fun, and affordable sport plane. The Vol Medici company that marketed the Esqual sold off the company and (so far) stop producing the Esqual kits. Jabiru USA was the US importer for Esqual. This aircraft complemented the Jabiru line of aircraft as well as providing for a low wing alternative to the high wing Jabirus. The wing of the Lightning was designed much like the pressure recovery wheelpants. The wheelpants are from the RV series of aircraft and modified to suit our own needs. RV borrowed the design from Cessna. The idea is that there was a better way to fair the landing gear that would result in less drag. At the point where the airflow starts to detach from the surface of the gear, the shape would create a suction that would reattach the boundry layer. The wing was designed as a kind of teardrop shape with concave trailing edge shape. It is a high laminar flow wing. Now the wing that is on the Lightning is kind of a reverse engineered wing that was originally on the Esqual wing. For various reasons that airfoil was traded for a different one and the molds were destroyed. The new Esqual wing is more of a Clark Y "Hershey Bar" type. That wing will allow for a shorter takeoff run, but at the same time will float forever if you come in hot and get in ground effect. In Europe, operating out of grass strips the lower takeoff run and slower liftoff speeds were more desirable on a sport plane than all out speed. The Lightning wing is whole different beast. The speeds are higher on the plane for takeoff and landing. The flaps work much better than the Esqual in that they provide the needed drag where the Esqual is mostly lift and a means of not accelerating when pointing the nose down, kind of more like a speed brake. As with any glass plane it will accelerate rapidly when the nose is pointed down in a clean configuration. On one particular flight test in an Esqual I tested for aileron flutter after finding and tightning a loose aileron. With the power to idle in almost a vertical down line the Esqual will quit accelerating and hold about 185-195 mph indicated. The Lightning will eagerly pass through 200 and rapidly accelerate past Vne. There were two "hybrids" and one prototype aircraft. The first hybrid, which we refer to as the "Frankensqual" is an Esqual fuselage with the prototype set of Lightning wings. It has an old 80hp Jabiru 2200 engine and will do 160mph flat out! The airplane is about twice as pitch sensitive as the Lightning with much lighter feeling on the controls. It has a far aft CG because of the light weight of the engine and had each wing that was 60lbs. heavier. Very impressive performance and after about 15 minutes of flying it you get used to the sensitivity. The next was Buzz's plane which tested the wheelpants, gear leg fairings, and the cowling for the lightning. Buzz built the fastest Esqual in the world, by about 40-50mph! In fact, his plane is similar in performance to the Lightning. In an all out speed comparison at 5,000 feet the prototype Lightning pulled away from Buzzes plane by about 1-2 knots. The pitch of the prop wasn't set to the optimal level on the prototype at the time in its defense. Some of the speed can certainly be attributed to Buzzes craftmanship and attention to detail. For those of you who have seen it you know what I mean. Getting everything faired over and making sure that you have a tight fit and smooth finish amounts to drag reduction, and superb looks. Buzz also got custom leather interior and foam fitted seats put in. I encourage any of you builders to do something similar. The cloth seats are comfortable, but those leather/foam seats just really feel nice and make for a comfortable ride. The prototype, as did Greg Hobbs' plane had a thicker tail section which was the result of a miscommunication. The fiberglass layups were extremely thick in the tail which resulted in a much heavier fuselage with an aft CG. While this is great for speed, it is horrible for loading arrangements and total useful load. All of the newer planes have a lighter fuselage which should mean better takeoff performance and acceleration. The prototype also had an early horizontal stabilizer that was (I think) 6lbs heavier per side. It has since been replaced with a production tail. Nick is continually finding little ways to improve performance, looks, functionality, etc. This is as much his baby as anybody's and he continually tweaks things. The prototype eventually got to a little over 200mph TAS in level flight. That was at greater than 3300 rpm though. Now on to the Pilot Report: First off, approaching the airplane you notice that it is a very nice looking plane. The complex curves of the composite aircraft look very similar to that of a Lancair or Cirrus. The plane is smaller than either and looks fast just sitting there. A walk around is similar to any other light airplane with attention to the composites. I like to get down to eye level with the surface and look for any chips or cracks that may indicate delamination. So far I've never found any, which is the way it should be for a newly built plane, but it is a different type of a thing than you look for in a metal airplane. I pay careful attention to the tail area and stabilizers. The wings are extremely strong and both main wing spars cross through the fuselage, under the seat. The rear of the wing attaches to the fuselage without a carry through structure. Getting in the airplane is accomplished by climbing up on the wing, being careful to avoid stepping on the flaps. The sides of the plane are fairly low and you can easily throw a leg over into the cockpit. At this point you want to step into the seat and then your other leg goes over and into the floorboard. Once seated you find that there is adequate room for two adults to fit comfortably, even for long trips. The center console does get in the way, keeping you from moving the stick to the stops because it hits your knees. Future planes will have a console that terminates at the edge of the seat. This should fix the problem. Sitting in the plane the seats are reclined a bit. I find that on a long trip this made me want to raise my head forward and that was uncomfortable after a while. If the plane is going to be used for some long trips I would suggest fasioning some type of head rests. This of course would limit the useful load some though. The visibility is incredible with that bubble canopy. The canopy itself is much clearer and free of distortion when compared to the Esqual. Another thing is that the Lightning has a longer nose and gives a difference perspective than flying in an Esqual. With two on board and 10 degrees of flaps the plane will Flying Greg's airplane I found that the airplane was very responsive. The airplane will rotate the nosewheel to a degree or so at about 50 mph and will hop into the air at a little less than 60mph. Once airborne a speed of 80mph will give you greater than 1000 feet per mintue climb. The airplane is nimble, about 90 degrees of rolls per second. It has a really nice feel to it. The pushrods give a direct feedback from the plane and have a firm, but not heavy feel. This gives the plane a sporty feel, but not a twitchy overly sensitive feel. In a climb with high RPM and low speeds the plane requires some good rudder input. Again the controls are firm, but not heavy. Greg's airplane had a trim control issue at first which caused us to run out of trim and the nose would still fall at certain speeds. The plane can be flown in all operating configurations without trim, but it is more comfortable and easy to fly with the use of trim. The plane can be flown hands off when in unaccelerated steady-state flight in trimmed configuration. Again, on a long trip a dual axis autopilot would be nice to have, especially when coupled with the Grand Rapids EFIS. That would even do virtual approaches on autopilot. Landing speeds seemed to fall right in place if you can enter the pattern at no more than 110mph and slow to around 100 on downwind. The plane flies a nice at the 65mph final approach speed. The plane seems to have good rudder control and excellent aileron control authority in these lower speed ranges as well. Landing is more challenging in some ways than the Esqual. The Lightning doesn't really float. It is similar to a high performance Mooney in that the laminar flow wing flies to a point and then it stops. The trick is to round out the flare with a slight nose high attitude just as you reach the stall speed of between 45-55mph depending on configuration. I liked using 20 degrees of flaps instead of 30 degrees. For me it seemed to give a flatter and better feel on the approach. 30 degrees of flaps led to a good decent angle and although the plane will land just as smooth, I felt that this wing wanted to fly onto the runway. Flying Greg's plane out to the Tucson area we covered around 500 miles in a little over 2.7 hours. We burned approximately 6.0 gph at 2950 RPM (slightly high side of cruise RPM) Greg admitted that the jets weren't quiet tweaked as well as they could be and that a slightly lower fuel burn would be in the near future for his plane. We also didn't have the plane all fastened up and as sleek as it could be. The plane still had a slight right roll which resulted in about an inch of each aileron being deflected and causing undue drag. Greg had planned on fairing over some small parts around the wheelpants and gear leg intersections. We had hotter than normal CHT's due to an 'experiment' with adding a ramp to one side of the cylinder heads at the entrance. This proved to actually make the majority of the air go over the cylinders at any angle of attack and out the outflow. I understand that with the ramp removed the CHT's are more uniform now. With these little improvements that Greg has done I imagine he'll pick up another 10 knots or so at least. There had been the thought of testing some gap seals on the prototype to get some additional speed for free type of an improvement. I had also suggested a winglet design for cruise performance, looks, and the added stability for long cruise flights. If correctly designed they would slightly increase speed, increase range and climb rates, decrease takeoff roll, but I believe the looks are worth as much if not more than the performance gains. If any of you know Greg or if he is part of the list, tell him that I'd be happy to make the journey out west to fly any of the customer planes on some of the first flights. They all are a little bit different and all have their own special needs as far as setting them up. Once you get things right though you get a "Lightning" fast airplane that is comfortable and stable. Hope you all enjoyed the read and any little improvements to the plane that you want to suggest I'll be sure to relay to Nick. Brian Whittingham


    Message 2


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    Time: 12:13:36 AM PST US
    From: "Tex Mantell" <wb2ssj@earthlink.net>
    Subject: 5/8 bolts
    I have 3 5/8 bolts. 2 are 5" long, one is 6" long. I believe the two 5" one's hold the wings to the central beam. Where does the 6" bolt go? Anyone? Tex


    Message 3


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    Time: 12:23:39 AM PST US
    From: "Pete" <pete@flylightning.net>
    Subject: Re: RV-9A v. Lightening
    --> Lightning-List message posted by: "Pete" <pete@flylightning.net> All, Here's a email that has me just chomping at the bit to correct some real inaccuracies from someone who didn't sign his name! Let's start with stability for cross country. We had the opportunity to fly a RV-6 for a few hours a few weeks ago to compare handling. The RV was great but - the Lightning was its equal. The Lightning was more stable in roll and about the same in pitch. The RV pitch forces got quite heavy with advancing speed while Lightning's did not. If you are equating the stability of Lightning to Esqual you are on the wrong track and putting out an opinion not based on any fact. The Lightning cruises 5 knots slower than the 160 hp RV 6 that we flew. On a three hour flight that would equate to 5 minutes difference. Yes - it is a bit slower but it uses 5.5 gph vs the 9 that the RV was using. On that three hour flight with gas at $4.00 it cost $42 to gain those 5 minutes. Engine maintenance is probably easier with the Jabiru engine. If you are out in the boondocks you can get Jabiru plugs, dust caps, rotors, and even mags at most auto stores. Try walking into your autozone in a town where there is no aircraft maintenance and asking for parts for your Lycoming mag! Granted, there are not many A&P's with Jabiru experience but the number is growing and in a few short years there will be a selection of places near home where you can take your Jabiru engine for repairs that cost far, far less than a Lycoming repair. As far as the "heating issues" you mention with Jabiru: those are installation issues that are no fault of the engine. If a Lycoming was installed with the same engineering as most of the Jabiru's with :heating issues" were installed you'd be telling us about Lycomings with heating issues - but you'd have to leave off the bit about smooth running. As far as the Rotax being an alternative - only the earlier Esquals in Europe were Rotax powered. Since 2003 when Jabiru was introduced as an option the vast majority of Esquals have been Jabiru powered. As far as structural strength - you are wrong again about Lightning. Esqual probably is not as strong as an RV but Lightning is built stronger than the Van's product. We can show you photos of Lightning wings loaded to 11 G positive & negative. I'd like to see the Vans wing loaded to 11G. I have the feeling there would be some crumpled metal. The final point of your email is a good one - it needs to come down to pilot preference. As you say - it's "your money, time, and life". That's why when an unsigned email comes along with facts that are just wrong or unsupported opinions disguised as facts - it is good to hear the other side. That's what the internet is for, right? Anyone can say anything at any time - right or wrong - and not take responsibility for it. Pete -----Original Message----- From: owner-lightning-list-server@matronics.com [mailto:owner-lightning-list-server@matronics.com] On Behalf Of jackb911 Sent: Thursday, August 17, 2006 12:06 PM Subject: Lightning-List: Re: RV-9A v. Lightening --> Lightning-List message posted by: "jackb911" <jackb911@yahoo.com> John, I'm sure that the decision is not easy. I managed to get some time in both an RV6 and an Esqual. (The Esqual is very similar to the Lightning and was sold by the Lightning folks, but it looks like they no longer support it. However, the Esqual continues to be sold and supported in Europe. The European people are advertising for a new US dealer). On a cross country platform it is my opinion that the Lightning will not be as stable or as fast as the RV. But then it won't burn as much fuel either. Your mpg in the Lightning should be better. Balanced control surfaces on the RV were great, the Esqual and I suspect the Lightning not as good. Either plane might be able to be tweaked. You might tweak the Lightning to higher speeds than normal, but the RV9 can likewise be tweaked higher. Stability for cross country was better in the RV than the Esqual; I suspect primarily due to a combination of wing loading and overall increased weight and well harmonized control input. In IFR, I would rather be in the Vans. Mile for mile, the Lightning should fly at a lower fuel cost. Engine maintenance - I haven't talked with enough Jabiru people to feel like I have a good comparison. It is easy to take the Lycoming O-360 to several places near home no matter where you live for needed attention. The Jabiru doesn't have the same options. It continues to suffer from heating issues but seems to be a great little engine and is very smooth. An alternative to the Jabiru might be the Rotax 912 or 914. Almost all of the Esquals flying in Europe use the Rotax with favorable results. But again, even with the Rotax there are not as many service options. The Vans has thousands of RV's flying and years of experience. The Lightning is new with good potential, but little track record (The Esqual has several years of favorable track record in Europe and a few in the US). I would guess that you should be able to get the Lightning in the air faster with less build time. If you would rather be flying than building then the Lightning seems to have the advantage. On structural strength my nod goes to the RV especially if aerobatics are considered. The RV has maybe a 1/4 to 1/3 more baggage area available. The Esqual is a less complex aircraft for flying, better suited for low time pilots. The low handling speeds were great! I'm not sure if the Lightning can get as close to the lower handling speeds, but if so that would be a nice positive. The looks of the Lightning are impressive! With the right paint job I think that it (and the Esqual) are my favorites on curb appeal. Bottom line? The decision will come down to pilot preference. Both planes appear to be good planes. One has a long track record, the other is just starting to build one. Before you decide, you should definitely spend some time flying in both, research the power plant pros and cons, and consider what support you might need for your plane down the road and will it be there. Don't get so caught up in your dreams that you overlook the realities of how each plane flies today. After you have listened to me and everyone else, it is your money, time, and life that are on the line. Just another opinion out of many. Good luck! Read this topic online here: http://forums.matronics.com/viewtopic.php?p=55330#55330


    Message 4


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    Time: 12:25:38 AM PST US
    From: "Brian Whittingham" <dashvii@hotmail.com>
    Subject: Re: RV-9A v. Lightening
    --> Lightning-List message posted by: "Brian Whittingham" <dashvii@hotmail.com> IMile for mile, the Lightning should fly at a lower fuel cost. Engine maintenance - I haven't talked with enough Jabiru people to feel like I have a good comparison. It is easy to take the Lycoming O-360 to several places near home no matter where you live for needed attention. The Jabiru doesn't have the same options. It continues to suffer from heating issues but seems to be a great little engine and is very smooth. An alternative to the Jabiru might be the Rotax 912 or 914. Almost all of the Esquals flying in Europe use the Rotax with favorable results. But again, even with the Rotax there are not as many service options. The Vans has thousands of RV's flying and years of experience. The Lightning is new with good potential, but little track record (The Esqual has several years of favorable track record in Europe and a few in the US). I would guess that you should be able to get the Lightning in the air faster with less build time. If you would rather be flying than building then the Lightning seems to have the advantage. On structural strength my nod goes to the RV especially if aerobatics are considered. The RV has maybe a 1/4 to 1/3 more baggage area available. The Esqual is a less complex aircraft for flying, better suited for low time pilots. The low handling speeds were great! I'm not sure if the Lightning can get as close to the lower handling speeds, but if so that would be a nice positive. John, I have not flown an RV-6, although I plan to get some time in one before too long. I have flown both the Lightning and Esqual though. It is my underdstanding that the Esqual company has sold out and possibly reforming another company to market the Esqual. Right now in Shelbyville there are two Esquals which are being built. These will be the last two built here unless they start making new kits again. Although I have not flown the RV6, Nick that test flew the first Lightning has flown both. So I do have some basis for comparison here. Nick relayed that the RV-6 was less stable in roll than the Lightning. The pitch is fairly comparable. Fuel burn at 75% cruise is about 5.5 gph on the Lightning. This is a 120hp engine that will give you a cruise of 185mph which is almost identical to a 150hp RV. So I would have to say that the Lightning would be better for cross-country flying. The only way that I would deviate from that is if you needed a lot of cargo room. You're probably not going to get a couple of suit cases in there, but then again you won't get a whole lot in the RV either. If we ever made the Lightning with the 180hp 8 cylinder Jabiru it would be faster than any of the RV series of aircraft. On a 1500 mile + trip from TN to Arizona the ride was smoother than an Esqual and the only turbulence was where you'd expect it and it wasn't more than minor chop. The Lightning does have slightly reclined seating and I think that for long trips, fashioning some sort of headrest would be more comfortable as I kept wanting to bend my neck forward so that my head was up straight. We covered the last 500 miles in 2 hours 45 minutes which averages out to about 181mph. The control feel for the Lightning is totally different than the Esqual is. The controls are counterweighted and the inputs have more of a solid and fluid feel to them. In IFR conditions the Lightning does not have static wicks and therefore could be a no-go if flying around thunderstorms. Jack was right that finding a person to work on the Jabiru engine might be a little harder to find. There is an engine seminar program here in Shelbyville that can be taken. Then there are kits that can be sent out for overhaul or you can bring it in for overhaul. The Jabiru requires little maintenance other than the normal oil change. It is much cheaper to overhaul than either a Lycoming or Continental. We have had several people "convert" to at least looking at the Lightning over the RV series simply due to the short build times. I would look carefully at the structural strength. The Lightning is not considered an aerobatic aircraft, so if that is a consideration then you might want to look at the RV. On the other hand the Lightning wing had an Ultimate Load Factor that will surpass over 95% of aircraft that are built today. The Lightning comes in just slightly faster than a standard Esqual, but less than 10mph faster if I remember correctly. I come in at 70mph in the Lightning and rotate around 60. So that is a pretty slow speed. The Lightning, however does fly much differently than the Esqual. You aim for a landing point and if you are on speed then you land where you want. The Esqual would float forever. The Lightning does not. I would rate the Lightning as harder to fly than the Esqual, but not difficult. It isn't any harder to fly than an RV6. I would not put a low time pilot in one without getting some transition training. One last thought. The RV is metal, and the Lightning is composite. You don't get the curves with the metal. It is a different kind of construction as well. If you want to fly fast in a short amount of time and have great looks and superb handling I'd go with the lightning. If you want a little longer to get in the air and fly a few knots faster with up to twice the fuel burn and still good handling, I'd go with the RV. Just my observations, Brian W.


    Message 5


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    Time: 03:38:04 AM PST US
    From: Kayberg@AOL.COM
    Subject: Re: 5/8 bolts
    In a message dated 8/22/2006 3:14:20 AM Eastern Standard Time, wb2ssj@earthlink.net writes: I have 3 5/8 bolts. 2 are 5" long, one is 6" long. I believe the two 5" one's hold the wings to the central beam. Where does the 6" bolt go? Anyone? Tex Nose gear axel? doug


    Message 6


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    Time: 11:49:49 AM PST US
    From: nick otterback <vettin74@yahoo.com>
    Subject: Re: 5/8 bolts
    th 6 inch is the nose axle nick Kayberg@aol.com wrote: In a message dated 8/22/2006 3:14:20 AM Eastern Standard Time, wb2ssj@earthlink.net writes: I have 3 5/8 bolts. 2 are 5" long, one is 6" long. I believe the two 5" one's hold the wings to the central beam. Where does the 6" bolt go? Anyone? Tex Nose gear axel? doug ---------------------------------


    Message 7


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    Time: 08:03:11 PM PST US
    From: N1BZRich@AOL.COM
    Subject: Re: Lightning Cargo Capacity Questions
    Dan, As a follow up on your Lightning baggage space area, it looks like you could install the floor about 15 inches below the seat back. The baggage area average width is about 40 inches, and the length is about 24 inches. Rough estimate is a baggage space of 8.35 cubic feet without loading things about the back of the seats. There would be no problem with light and soft things being above the back of the seat backs. Hope this helps. Blue Skies, Buz


    Message 8


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    Time: 11:01:40 PM PST US
    From: Daniel Vandenberg <djvdb63@yahoo.com>
    Subject: Re: Lightning Cargo Capacity Questions
    Buz... Your response to my series of questions is greatly appreciated. The Lightning is most impressive. With the uncertainty of fuel prices in the coming years I am particularly enamored by the thought of possibly achieving 30 mpg in an aircraft that is actually a serious travelling machine (in addition to being fun). I will be watching the Lightning closely in the coming several months. By the way, there was an F-4 at Gary, IN (GYY) this past weekend...I think for the Chicago Air & Water Show. I had thought these were all in mothballs. Dan N1BZRich@aol.com wrote: Dan, As a follow up on your Lightning baggage space area, it looks like you could install the floor about 15 inches below the seat back. The baggage area average width is about 40 inches, and the length is about 24 inches. Rough estimate is a baggage space of 8.35 cubic feet without loading things about the back of the seats. There would be no problem with light and soft things being above the back of the seat backs. Hope this helps. Blue Skies, Buz ---------------------------------




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