Allegro-List Digest Archive

Fri 12/08/06


Total Messages Posted: 4



Today's Message Index:
----------------------
 
     1. 12:23 AM - Matronics Fund Raiser - 2006 List of Contributors (Matt Dralle)
     2. 03:54 AM - Re: Empty weight and C.G. Location (TIM MOSES)
     3. 05:49 AM - Re: Empty weight and C.G. Location (Thom Riddle)
     4. 07:38 AM - Re: Empty weight and C.G. Location (Hugh McKay III)
 
 
 


Message 1


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    Time: 12:23:51 AM PST US
    From: Matt Dralle <dralle@matronics.com>
    Subject: Matronics Fund Raiser - 2006 List of Contributors
    Dear Listers, I would like to thank everyone that made a Contribution in support of the Lists this year! It was really nice to hear all great comments people had regarding the Lists! As I have said many times before, running these Lists is a labor of love. Your generosity during the List Fund Raiser only underscores the great sentiments people have made regarding the Lists. If you haven't yet made a Contribution in support of this year's Fund Raiser please feel free to do so. The nice List gifts will be available on the site for just a little while longer, so hurry and make your Contribution and get your great gift. Once again, the URL for the Contribution web site is: http://www.matronics.com/contribution I would like to thank Andy Gold of the Builder's Bookstore ( http://www.buildersbooks.com ), Paul Besing of Aeroware Enterprises ( http://www.kitlog.com ), Jon Croke of Homebuilt HELP ( http://www.homebuilthelp.com ) and Bob Nuckolls of AeroElectric ( http://www.aeroelectric.com ) for their extremely generous support during this year's Fund Raiser through the contribution of merchandise. These are great guys that support the aviation industry and I encourage each and every Lister to have a look at their products. Thank you Andy, Paul, Jon and Bob!! Your support is very much appreciated! And finally, below you will find a web link to the 2006 List of Contributors current as of 12/7/06! Have a look at this list of names as these are the people that make all of these List services possible! I can't thank each of you enough for your support and great feedback during this year's Fund Raiser! THANK YOU! http://www.matronics.com/loc/2006.html I will be shipping out all of the gifts in the next few weeks and hope to have everything out by the end of the month. In most cases, gifts will be shipped via US Postal Service. Kitlog Pro serial numbers should go out via email this weekend. Once again, thank you for making this year's List Fund Raiser successful! Best regards, Matt Dralle Matronics Email List Administrator


    Message 2


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    Time: 03:54:42 AM PST US
    From: "TIM MOSES" <tcmoses@earthlink.net>
    Subject: Re: Empty weight and C.G. Location
    Hugh, I have an Allegro and a GT-500 that I just weighed for conversion to E-LSA. I can not help but wonder is your scales are accurate or if they jamed due to side movement of the main gear. As Ken Arnold said this is very worrisome. I used 3 - 400 pound digital scales to weigh the GT-500 and had no problems with repeatability of the scales each time I jacked the plane off of them and reapplied the weight. Tim Moses ----- Original Message ----- From: Ken Arnold To: allegro-list@matronics.com Sent: Thursday, December 07, 2006 7:18 PM Subject: Re: Allegro-List: Empty weight and C.G. Location I have a Zenith CH701 kit on order. For the past year of so, I observe that most builders are significantly over the published empty weight. I can understand a small overage but nearly 100 lbs over with what appears to be standard installs is worrisome. Ken Arnold CH701 on order ----- Original Message ----- From: Hugh McKay III To: allegro-list@matronics.com Sent: Thursday, December 07, 2006 11:41 AM Subject: Allegro-List: Empty weight and C.G. Location Gentlemen: I have just weighed my kit built Allegro 2000 (empty weight*) to compare with the published empty weight in the Fantasy Air Flight and Operating Manual. * empty weight = weight of plane with standard instruments, engine, coolant, oil, ELT, & Battery (no fuel and no BRS). My empty weight* is 320 Kg, or 704 lbs. (Nose wheel = 154 lbs., Right Main wheel = 270 lbs., Left Main wheel = 280 lbs.) The Flight and Operating Manual states that the empty weight should be 275 Kg or 605 lbs. I am 99 lbs (16%) heavier than what is published for the empty weight! The published MTOW is 520 Kg, or 1144 lbs. This leaves me only 440 lbs for a BRS, Fuel and 2 occupants. Those numbers are as follows: Main fuel tank fuel 14.5 gal. = 88.97 lbs. BRS = 35.00 lbs. Wing Tanks Fuel 10.4 gal. = 64.00 lbs. My Weight = 150.00 lbs Total = 337.97 lbs. 440 lbs. minus 337.97 lbs is 102.03 lbs max weight for the passenger in order not to exceed the MTOW of 1144 lbs. With these numbers, in reality I can't take a passenger unless he is a child or a very light weight adult. What is the basis of the 275 Kg (605 lbs.) stated in the F and O Manual? I don't understand why I am 99 lbs over the published empty weight! I have nothing more in this plane at empty weight* other than what I have stated above with the *. What are the empty weights running for the ready to fly Allegros with similar items? With a total empty weight of 704 lbs. the c.g. is 12.18 inches behind the leading edge. The maximum allowable distance is 390 mm or 15.35" behind the leading edge. 12.18" is 81% of the limit. The F & O Manual states that the c.g. of the empty aircraft is almost exactly the same for the aircraft with one or two pilots and with an empty or full fuel tank. According to this, the empty c.g. and the MTOW c.g. stays the same (i.e I do not have to weigh the plane with fuel, and passengers to calculate a new c.g. . Is this correct? I have sent this information to the US Distributor, Fantasy Air USA, but I would like to get some independent feedback concerning the weight issue (605 lbs. Vs. 704 lbs.). Do any of you know your comparable empty weights, and would you share them with me? Any and all help will be deeply appreciated. Hugh McKay Allegro 2000 Rotax 912UL N661WW href="http://www.aeroelectric.com">www.aeroelectric.com href="http://www.buildersbooks.com">www.buildersbooks.com href="http://www.kitlog.com">www.kitlog.com href="http://www.homebuilthelp.com">www.homebuilthelp.com href="http://www.matronics.com/contribution">http://www.matronics.com/c href="http://www.matronics.com/Navigator?Allegro-List">http://www.matro nics.com/Navigator?Allegro-List


    Message 3


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    Time: 05:49:12 AM PST US
    From: Thom Riddle <jtriddle@adelphia.net>
    Subject: Re: Empty weight and C.G. Location
    Hugh, I am guessing the "book" empty weight of 605 lb. is the lightest one ever built in the Czech Republic which probably had nothing but the legal minimum in the way of instruments, i.e., airspeed, tachometer, oil pressure gauge, fuel gauge. You can be sure the "book" empty weight airplane had not wheel pants or any other options installed for the official weigh-in. I would not be surprised if the fuel tank (main only - no wing tanks) did not even have the 1/2 gallon of unusable fuel (3 lb.). Also, the early models had thinner main gear legs and had fabric on the upper and lower wings between the main and trailing edge spars. If you calculate all these differences it would not surprise me if the lightest possible empty weight at that time was what their out-of-date documents state. Speaking of out-of-date documents, the MTOW figure in your manual is the way it was certificated in Europe because of their micro-light (or whatever they call that category) legal limitations. The MTOW in the LSA category here is 1,232 lb. which gives you another 88 lb. to play with but don't forget to add in the 3 lb. for the 1/2 gal. of unusable fuel into your empty weight, if you weighed it before adding fuel. I never bothered trying to do the W&B with the formulas in the manual. I do not doubt that they are mathematically equivalent to the way we do it here but I just used the US method. Keep in mind that the 1144 lb. MTOW was used to establish the 4G+ and 2G- load limits. The actual load limits for the 1232 lb. MTOW would be factored down a bit. I posted something about this on the Allegro List many months ago. I suspect the 1232 lb. limit for the LSA category is to keep the max stall speed Vs1 at 45 knots or less as required by the LSA regs. Our Allegro #03-202 has a current empty weight of 649 lb. with the empty CG at 11.13" aft of wing root leading edge. This is based on the documentation that came with the aircraft when we bought it as a demo unit from the Nebraska dealer plus the few small additions we made to it since the purchase. We've never done an actual accurate weighing of the airplane so this could be off somewhat. It would not surprise me that it is off several pounds. I suspect there was some equipment added between the time it was imported and the time we bought it and the new items not added into the official W&B documents. I don't know this for certain. Our Allegro is the only one in the US with the fabric wing panels and it had the older thinner gear legs too until we replaced them with the newer heavier ones. We did not add anything to the empty weight for the legs because the factory didn't tell us they were heavier but I can tell you from measuring them that they are thicker and hopefully stronger. No problems so far with the new legs. Our airplane has only the main fuel tank but it also has the electric artificial horizon, Icom A-200 radio, intercom, King transponder (we install after purchase) electric engine pre-heater (~4 oz) an oil thermostat (~2 lb.), wing tip nav and strobes, and landing lights. That said, one of my partners weighs 280 lb. and our check-out instructor weighs 210 lb, so when they flew together with full main fuel, they were close but not over the 1232 lb. MTOW with no handling issues at all according to my partner's reports. I've personally flown it at nearly 1200 lb. and it flies great at that weight though the ROC is not as good. I hope this helps a bit. Thom in Buffalo do not archive


    Message 4


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    Time: 07:38:14 AM PST US
    From: "Hugh McKay III" <hgmckay@bellsouth.net>
    Subject: Empty weight and C.G. Location
    Thom: Thanks for your excellent explanation. I am going to check my scales and their calibration again to make sure my weights are correct. I thought the MTOW for LSA in the USA was 1320 lbs. not 1232 lbs. Am I wrong? If it is 1320 lbs., the real question is; "is the Allegro 2000 designed to safely fly with a MTOW of 1320 lbs, or only 1146 lbs. (520 Kg)? Hugh -----Original Message----- From: owner-allegro-list-server@matronics.com [mailto:owner-allegro-list-server@matronics.com]On Behalf Of Thom Riddle Sent: Friday, December 08, 2006 8:49 AM Subject: Re: Allegro-List: Empty weight and C.G. Location Hugh, I am guessing the "book" empty weight of 605 lb. is the lightest one ever built in the Czech Republic which probably had nothing but the legal minimum in the way of instruments, i.e., airspeed, tachometer, oil pressure gauge, fuel gauge. You can be sure the "book" empty weight airplane had not wheel pants or any other options installed for the official weigh-in. I would not be surprised if the fuel tank (main only - no wing tanks) did not even have the 1/2 gallon of unusable fuel (3 lb.). Also, the early models had thinner main gear legs and had fabric on the upper and lower wings between the main and trailing edge spars. If you calculate all these differences it would not surprise me if the lightest possible empty weight at that time was what their out-of-date documents state. Speaking of out-of-date documents, the MTOW figure in your manual is the way it was certificated in Europe because of their micro-light (or whatever they call that category) legal limitations. The MTOW in the LSA category here is 1,232 lb. which gives you another 88 lb. to play with but don't forget to add in the 3 lb. for the 1/2 gal. of unusable fuel into your empty weight, if you weighed it before adding fuel. I never bothered trying to do the W&B with the formulas in the manual. I do not doubt that they are mathematically equivalent to the way we do it here but I just used the US method. Keep in mind that the 1144 lb. MTOW was used to establish the 4G+ and 2G- load limits. The actual load limits for the 1232 lb. MTOW would be factored down a bit. I posted something about this on the Allegro List many months ago. I suspect the 1232 lb. limit for the LSA category is to keep the max stall speed Vs1 at 45 knots or less as required by the LSA regs. Our Allegro #03-202 has a current empty weight of 649 lb. with the empty CG at 11.13" aft of wing root leading edge. This is based on the documentation that came with the aircraft when we bought it as a demo unit from the Nebraska dealer plus the few small additions we made to it since the purchase. We've never done an actual accurate weighing of the airplane so this could be off somewhat. It would not surprise me that it is off several pounds. I suspect there was some equipment added between the time it was imported and the time we bought it and the new items not added into the official W&B documents. I don't know this for certain. Our Allegro is the only one in the US with the fabric wing panels and it had the older thinner gear legs too until we replaced them with the newer heavier ones. We did not add anything to the empty weight for the legs because the factory didn't tell us they were heavier but I can tell you from measuring them that they are thicker and hopefully stronger. No problems so far with the new legs. Our airplane has only the main fuel tank but it also has the electric artificial horizon, Icom A-200 radio, intercom, King transponder (we install after purchase) electric engine pre-heater (~4 oz) an oil thermostat (~2 lb.), wing tip nav and strobes, and landing lights. That said, one of my partners weighs 280 lb. and our check-out instructor weighs 210 lb, so when they flew together with full main fuel, they were close but not over the 1232 lb. MTOW with no handling issues at all according to my partner's reports. I've personally flown it at nearly 1200 lb. and it flies great at that weight though the ROC is not as good. I hope this helps a bit. Thom in Buffalo do not archive




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