Allegro-List Digest Archive

Wed 07/19/06


Total Messages Posted: 3



Today's Message Index:
----------------------
 
     1. 04:49 AM - Re: Allegro 2000 - Rotax 912UL Engine (Thom Riddle)
     2. 11:01 AM - Re: Allegro 2000 - Rotax 912UL Engine (hgmckay)
     3. 01:51 PM - Re: Allegro 2000 - Rotax 912UL Engine (Thom Riddle)
 
 
 


Message 1


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    Time: 04:49:39 AM PST US
    From: Thom Riddle <jtriddle@adelphia.net>
    Subject: Re: Allegro 2000 - Rotax 912UL Engine
    --> Allegro-List message posted by: Thom Riddle <jtriddle@adelphia.net> Hugh, I know you did not address this to me and I can't answer your question about the stall warning but I can tell you something about the five point fuel distribution block. There is only one tiny restrictor orifice in mine and it is in the branch that goes to the fuel pressure gauge. The purpose of this is to restrict flow to an absolute minimum in case this fuel line ruptures. If a fuel line going into the cockpit ruptures and you don't have this restrictor, the cabin could be flooded with fuel. A very hazardous condition. This pressure gauge does not need flow but only pressure to do its job and restrictors in pressurized fuel lines that go to the cabin are standard on GA aircraft. If I remember correctly, your airplane has the aux. fuel tanks. Ours does not, so I don't know how the extra fuel lines are plumbed. I know that you do NOT want a restrictor in a fuel SUPPLY line as it would starve the carburetors. I would ask Doug at B Bar D about where the second restrictor is supposed to be. It may have been installed in the distribution block by mistake. Thom in Buffalo


    Message 2


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    Time: 11:01:36 AM PST US
    From: "hgmckay" <hgmckay@bellsouth.net>
    Subject: Re: Allegro 2000 - Rotax 912UL Engine
    --> Allegro-List message posted by: "hgmckay" <hgmckay@bellsouth.net> Thom: I did ask Doug Hempsted about the two restrictor orifices. His reply was that both are are required. he did not explain why, but based on your explanation two would apply in my case because there are two fuel lines coming back into the cockpit. One being the fuel pressure gauge, the other the fuel return line to the main fuel tank (see the Rotax engine installation manual page 38 of 66). On another topic, (Static rpm test), can I safely do this test with the wings off the plane? As you know I do have wing tanks, but I am waiting on the new replacement aluminum tanks so I don't want to put the wings on and then have to take them off again to insert and attach the wing tanks. I would connect all the fuel lines in the cockpit, but cut off the fuel lines going to the wing tanks with their respective cut-off valves at the two side cover sheets adjacent to the root of each wing. Any comments about this test without the wings on? Hugh Read this topic online here: http://forums.matronics.com/viewtopic.php?p=48596#48596


    Message 3


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    Time: 01:51:37 PM PST US
    From: "Thom Riddle" <jtriddle@adelphia.net>
    Subject: Re: Allegro 2000 - Rotax 912UL Engine
    --> Allegro-List message posted by: "Thom Riddle" <jtriddle@adelphia.net> Hugh, I see no problem with doing static run-up w/o wings. Not much chance of it getting airborne that way :-). As long as you do the fuel line configuration as you stated, the engine won't care and the fuel won't be flying out all over the place. It should go without saying but it does not hurt to remind you to make sure the airframe is well secured before doing a full throttle static run-up. If you are doing carb idle speed adjustments in the process, make sure the engine is up to normal operating temperature(190F min) before doing so. You may not be able to finalize the idle speed until after you've flown it. The idle speed at 120F can be 200-300 rpm different than at 190F or higher. At higher oil temps, the idle speed is higher. -------- Thom in Buffalo Read this topic online here: http://forums.matronics.com/viewtopic.php?p=48647#48647




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