Europa-List Digest Archive

Sat 08/19/06


Total Messages Posted: 8



Today's Message Index:
----------------------
 
     1. 03:23 AM - Re: Oshkosh by air - return by Avis UPDATE (William Daniell)
     2. 05:21 AM - Re: Retro Fitting MG Wings  (Jim Butcher)
     3. 10:03 AM - Hot Jabaru in AZ (Steve Hagar)
     4. 12:04 PM - Re: Oshkosh by air - return by Avis UPDATE (Thomas Scherer)
     5. 03:44 PM - Re: Oshkosh by air - return by Avis UPDATE (R.C.Harrison)
     6. 08:56 PM - Oshkosh by air - return by Avis UPDATE (Fergus Kyle)
     7. 10:26 PM - FW: Hot Jabaru in AZ (R.C.Harrison)
     8. 10:55 PM - Wing Pip Pins (Richard Schultz)
 
 
 


Message 1


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    Time: 03:23:37 AM PST US
    From: "William Daniell" <wdaniell@etb.net.co>
    Subject: Oshkosh by air - return by Avis UPDATE
    there was an aeroperu 757 that crashed with 150 pax off lima for exactly the same problem _____ From: owner-europa-list-server@matronics.com [mailto:owner-europa-list-server@matronics.com] On Behalf Of Richard Schultz Sent: 18 August, 2006 18:43 Subject: Europa-List: Oshkosh by air - return by Avis UPDATE For those keeping up with the story of the engine problem. I used my enclosed trailer to recover the aircraft from its temporary exile in Iowa and have returned it to Houston. I had hoped that the time apart would give the plane a chance to think about it attitude. I was off today and finally got around to pulling the cowls and going back through the engine fuel system one step at a time. The fuel filters, as before were clean. Testing the pumps showed the normal amount of unregulated fuel flow of about 5 gallons in 10 minutes. Looking at the carburetor system for how it works the mixture. I pulled each of the vacuum lines and checked them for holes and cracks. I also inspected the 3-way valve for any dirt or blockage. I pulled the airbox pressure sensor and checked that it was clean of dirt and open to the back. I then pulled the static port that plugs in through the firewall. I was surprised to feel it stick in the firewall as I pulled it out. Looking back through the hole I noticed a rubber tube end facing the inside of the hole? Not remembering adding a vent hose to the sensor end I opened the access panel to the firewall and removed the radios from the stack to get my hands inside the panel to see what I had done.. I found the source of my problem attached to a 3 inch piece of tape clearly marked REMOVE BEFORE FLIGHT. I had left the cover over the end of the static port during sanding and painting and had made plans to remove it before installing the instrument panel. Guess what I forgot to do! UGH I left the rubber end cap on the static port. I guess the first 80 hours the engine was run in a lower and cooler environment then the last part of the Oshkosh trip. The added height and temp was enough the cause the fuel-air mixture to be too lean with the static port plugged. I will give the plane a good going over this weekend while I have it stripped down as I am at the 100 hour mark and want to check every thing but I plan to get a flight test in the early part of next week weather permitting. Lesson learned if you plan to do something later, ADD it to your annex E check list so you double check you got back to it. While this had a happy ending it could have been a lot more exciting if the power failure had been complete and at night. _____


    Message 2


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    Time: 05:21:35 AM PST US
    From: "Jim Butcher" <europa@triton.net>
    Subject: Re: Retro Fitting MG Wings
    --> Europa-List message posted by: "Jim Butcher" <europa@triton.net> To update this thread, we talked to Bob Berube who confirmed that the top skin needs to be trimmed. He suggested 1/2 inch gap to the fuselage. We still have a pretty large gap between the jigs and lift drag pin, 30 mm at the stbd aft. But there is plenty of length on the pin, so we bonded in three plates at the aft position on each wing. The forward pins only required one or two plates. The top skin will need to be trimmed to clear the flap cross tube, but the fairings will cover that. We didn't do the string but the measurements should ensure sweep. Yes, the spar bushings definitely make the spar thicker. We'll have to modify the spar cup that is attached to the stbd side of the cockpit module as well as the one that goes on the port MG wing. We think the pip pin is probably long enough, but will require a different number of washers than fitted for the short wings. Jim & Heather Butcher N241BW


    Message 3


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    Time: 10:03:54 AM PST US
    From: "Steve Hagar" <hagargs@earthlink.net>
    Subject: Hot Jabaru in AZ
    A friend of mine has a 6cyl Jabaru installed in a Thorpe. He has been dogged by high oil temperatures even after several iterations of oil coolers and scoops. There are several Europa installations out there. Has any one fought the high temps on their Jab installation in the Europa. We have had discussions at length on hot Rotaxes. Are there any thoughts on the hot Jabaru? Steve Hagar N40SH About 9 hrs airtime on the plane All with 2 people aboard Next flight will be single, looking forward to enhanced takeoff performance have never flown in a Europa with just myself aboard. Steve Hagar hagargs@earthlink.net


    Message 4


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    Time: 12:04:28 PM PST US
    From: "Thomas Scherer" <thomas@scherer.com>
    Subject: Re: Oshkosh by air - return by Avis UPDATE
    --> Europa-List message posted by: "Thomas Scherer" <thomas@scherer.com> Thank you for sharing your findings. I have developped the practice of writing right onto the airplane (wing, cowling, windshield) with a felt pen and erase with acetone after completing the task. be well, <Thomas, N81EU> ----- Original Message ----- From: "Ralph Hallett" <n100rh@sbcglobal.net> Sent: Friday, August 18, 2006 5:17 PM Subject: Re: Europa-List: Oshkosh by air - return by Avis UPDATE > --> Europa-List message posted by: Ralph Hallett <n100rh@sbcglobal.net> > > Richard, > Thanks for the follow up! Maybe, maybe you can keep me from doing the > same... ;) > > Ralph > > > Richard Schultz wrote: >> >> For those keeping up with the story of the engine problem. >> >> I used my enclosed trailer to recover the aircraft from its temporary >> exile in Iowa and have returned it to Houston. I had hoped that the time >> apart would give the plane a chance to think about it attitude. >> >> I was off today and finally got around to pulling the cowls and going >> back through the engine fuel system one step at a time. The fuel filters, >> as before were clean. Testing the pumps showed the normal amount of >> unregulated fuel flow of about 5 gallons in 10 minutes. Looking at the >> carburetor system for how it works the mixture. I pulled each of the >> vacuum lines and checked them for holes and cracks. I also inspected the >> 3-way valve for any dirt or blockage. I pulled the airbox pressure sensor >> and checked that it was clean of dirt and open to the back. I then pulled >> the static port that plugs in through the firewall. I was surprised to >> feel it stick in the firewall as I pulled it out. Looking back through >> the hole I noticed a rubber tube end facing the inside of the hole? >> >> Not remembering adding a vent hose to the sensor end I opened the access >> panel to the firewall and removed the radios from the stack to get my >> hands inside the panel to see what I had done. I found the source of my >> problem attached to a 3 inch piece of tape clearly marked REMOVE BEFORE >> FLIGHT. >> >> I had left the cover over the end of the static port during sanding and >> painting and had made plans to remove it before installing the instrument >> panel. Guess what I forgot to do! UGH I left the rubber end cap on the >> static port. I guess the first 80 hours the engine was run in a lower and >> cooler environment then the last part of the Oshkosh trip. The added >> height and temp was enough the cause the fuel-air mixture to be too lean >> with the static port plugged. >> >> I will give the plane a good going over this weekend while I have it >> stripped down as I am at the 100 hour mark and want to check every thing >> but I plan to get a flight test in the early part of next week weather >> permitting. >> >> Lesson learned if you plan to do something later, ADD it to your annex E >> check list so you double check you got back to it. While this had a happy >> ending it could have been a lot more exciting if the power failure had >> been complete and at night. >> >> ------------------------------------------------------------------------ >> * >> >> >> * > > >


    Message 5


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    Time: 03:44:04 PM PST US
    From: "R.C.Harrison" <ptag.dev@tiscali.co.uk>
    Subject: Oshkosh by air - return by Avis UPDATE
    --> Europa-List message posted by: "R.C.Harrison" <ptag.dev@tiscali.co.uk> Hi! Not Acetone on the windshield please unless you want it dissolved ! Regards Bob Harrison G-PTAG -----Original Message----- From: owner-europa-list-server@matronics.com [mailto:owner-europa-list-server@matronics.com] On Behalf Of Thomas Scherer Sent: 19 August 2006 20:03 Subject: Re: Europa-List: Oshkosh by air - return by Avis UPDATE --> Europa-List message posted by: "Thomas Scherer" <thomas@scherer.com> Thank you for sharing your findings. I have developped the practice of writing right onto the airplane (wing, cowling, windshield) with a felt pen and erase with acetone after completing the task. be well, <Thomas, N81EU> ----- Original Message ----- From: "Ralph Hallett" <n100rh@sbcglobal.net> Sent: Friday, August 18, 2006 5:17 PM Subject: Re: Europa-List: Oshkosh by air - return by Avis UPDATE > --> Europa-List message posted by: Ralph Hallett <n100rh@sbcglobal.net> > > Richard, > Thanks for the follow up! Maybe, maybe you can keep me from doing the > same... ;) > > Ralph > > > Richard Schultz wrote: >> >> For those keeping up with the story of the engine problem. >> >> I used my enclosed trailer to recover the aircraft from its temporary >> exile in Iowa and have returned it to Houston. I had hoped that the time >> apart would give the plane a chance to think about it attitude. >> >> I was off today and finally got around to pulling the cowls and going >> back through the engine fuel system one step at a time. The fuel filters, >> as before were clean. Testing the pumps showed the normal amount of >> unregulated fuel flow of about 5 gallons in 10 minutes. Looking at the >> carburetor system for how it works the mixture. I pulled each of the >> vacuum lines and checked them for holes and cracks. I also inspected the >> 3-way valve for any dirt or blockage. I pulled the airbox pressure sensor >> and checked that it was clean of dirt and open to the back. I then pulled >> the static port that plugs in through the firewall. I was surprised to >> feel it stick in the firewall as I pulled it out. Looking back through >> the hole I noticed a rubber tube end facing the inside of the hole? >> >> Not remembering adding a vent hose to the sensor end I opened the access >> panel to the firewall and removed the radios from the stack to get my >> hands inside the panel to see what I had done.. I found the source of my >> problem attached to a 3 inch piece of tape clearly marked REMOVE BEFORE >> FLIGHT. >> >> I had left the cover over the end of the static port during sanding and >> painting and had made plans to remove it before installing the instrument >> panel. Guess what I forgot to do! UGH I left the rubber end cap on the >> static port. I guess the first 80 hours the engine was run in a lower and >> cooler environment then the last part of the Oshkosh trip. The added >> height and temp was enough the cause the fuel-air mixture to be too lean >> with the static port plugged. >> >> I will give the plane a good going over this weekend while I have it >> stripped down as I am at the 100 hour mark and want to check every thing >> but I plan to get a flight test in the early part of next week weather >> permitting. >> >> Lesson learned if you plan to do something later, ADD it to your annex E >> check list so you double check you got back to it. While this had a happy >> ending it could have been a lot more exciting if the power failure had >> been complete and at night. >> >> ------------------------------------------------------------------------ >> * >> >> >> * > > >


    Message 6


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    Time: 08:56:59 PM PST US
    From: "Fergus Kyle" <VE3LVO@rac.ca>
    Subject: Oshkosh by air - return by Avis UPDATE
    --> Europa-List message posted by: "Fergus Kyle" <VE3LVO@rac.ca> Time: 04:44:41 PM PST US From: "Richard Schultz" <Rschultz5@houston.rr.com> Subject: Europa-List: Oshkosh by air - return by Avis UPDATE "For those keeping up with the story of the engine problem. I used my enclosed trailer to recover the aircraft from its temporary exile in Iowa and have returned it to Houston. I had hoped that the time apart would give the plane a chance to think about it attitude. I was off today and finally got around to pulling the cowls and going back through the engine fuel system one step at a time. The fuel filters, as before were clean. Testing the pumps showed the normal amount of unregulated fuel flow of about 5 gallons in 10 minutes. Looking at the carburetor system for how it works the mixture. I pulled each of the vacuum lines and checked them for holes and cracks. I also inspected the 3-way valve for any dirt or blockage. I pulled the airbox pressure sensor and checked that it was clean of dirt and open to the back. I then pulled the static port that plugs in through the firewall. I was surprised to feel it stick in the firewall as I pulled it out. Looking back through the hole I noticed a rubber tube end facing the inside of the hole? Not remembering adding a vent hose to the sensor end I opened the access panel to the firewall and removed the radios from the stack to get my hands inside the panel to see what I had done.. I found the source of my problem attached to a 3 inch piece of tape clearly marked REMOVE BEFORE FLIGHT. I had left the cover over the end of the static port during sanding and painting and had made plans to remove it before installing the instrument panel. Guess what I forgot to do! UGH I left the rubber end cap on the static port. I guess the first 80 hours the engine was run in a lower and cooler environment then the last part of the Oshkosh trip. The added height and temp was enough the cause the fuel-air mixture to be too lean with the static port plugged. I will give the plane a good going over this weekend while I have it stripped down as I am at the 100 hour mark and want to check every thing but I plan to get a flight test in the early part of next week weather permitting. Lesson learned if you plan to do something later, ADD it to your annex E check list so you double check you got back to it. While this had a happy ending it could have been a lot more exciting if the power failure had been complete and at night." Richard, This perhaps not everybody's best idea (and too late for those already built) but: Anywhere in the build manual where I have not carried out the instruction to the letter (saving distortion nuts till later or whatever) I have put a red dot on the outer top corner of the sheet and a red line opposite the applicable direction - so that in review I can scan through the manual and correct the installation to its final state, put an 'X' throught the red dot, initial and date the correction, and annotate the applicable sentence. Then I ran a notice on the title page, describing this process for the examiner and any one else, so that it became an intrinsic part of the build. The Binx nuts were a typical sample. Ferg Kyle Europa A064 914 Classic


    Message 7


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    Time: 10:26:41 PM PST US
    From: "R.C.Harrison" <ptag.dev@tiscali.co.uk>
    Subject: Hot Jabaru in AZ
    -----Original Message----- From: R.C.Harrison [mailto:ptag.dev@tiscali.co.uk] Sent: 19 August 2006 23:42 Subject: RE: Europa-List: Hot Jabaru in AZ Hi! Steve Please advise him that he must have a dedicated and closed duct to intake the oil cooling air down through and under the sump fins and be ducted through the oil cooler to exhaust overboard at the rear of the cowl. Also he must not have more than half level of oil on the dip stick with the engine horizontal. Please have him visit the Europa support web page at :- www.crix.org.uk <http://www.crix.org.uk/> click on to " Bob Harrison's Europa G-PTAG " then scroll down to "oil cooler" I have done some more oil circuitry which allows me to control the oil through the cooler and I find I don't actually need the cooler in circuit except with ambient over 30 deg. and perhaps on a sustained climb or a "go round". I have also made provision for the oil cooler air to be used for cabin heat or exhausted into the cowl top to assist down flow of general cooling air. BTW I may be about to change to a Rotax 914! Regards Bob Harrison G-PTAG Europa MKI/Jabiru 3300 ..600 hours but grounded due to nose wheel departure on landing. -----Original Message----- From: owner-europa-list-server@matronics.com [mailto:owner-europa-list-server@matronics.com] On Behalf Of Steve Hagar Sent: 20 August 2006 18:07 Subject: Europa-List: Hot Jabaru in AZ A friend of mine has a 6cyl Jabaru installed in a Thorpe. He has been dogged by high oil temperatures even after several iterations of oil coolers and scoops. There are several Europa installations out there. Has any one fought the high temps on their Jab installation in the Europa. We have had discussions at length on hot Rotaxes. Are there any thoughts on the hot Jabaru? Steve Hagar N40SH About 9 hrs airtime on the plane All with 2 people aboard Next flight will be single, looking forward to enhanced takeoff performance have never flown in a Europa with just myself aboard. Steve Hagar hagargs@earthlink.net


    Message 8


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    Time: 10:55:19 PM PST US
    From: "Richard Schultz" <Rschultz5@houston.rr.com>
    Subject: Wing Pip Pins
    Is there a US source for the AVK BLS4R11N wing pip pins? I misplaced one during my recover efforts and am on the prowl for a local (quick) source I have tried to sort a match and the only thing close the company wants min order of 500. A few more then I currently need.




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