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Q1 Wing/ Canars
Hi Q-Comment, First install elevator / ailerons on canard/wing and than installed all together in the fuselage or the other way around? Which installation step would be a better choice? Any suggestion
Hi Q-Comment, First install elevator / ailerons on canard/wing and than installed all together in the fuselage or the other way around? Which installation step would be a better choice? Any suggestion
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By
Eugen Pilarski
· #55480
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Q2
So what’s the price? Von meinem iPhone gesendet
So what’s the price? Von meinem iPhone gesendet
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By
Eugen Pilarski
· #55474
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Q1 Tail wheel diameter
Hello Chris, thank you for your email. I just order this wheel, it’s a 6 x 1 1/4 inch pneumatic wheel (150mm) with a weight of 310g. I will follow the re-design of the Q2 tail wheel like in the Q-news
Hello Chris, thank you for your email. I just order this wheel, it’s a 6 x 1 1/4 inch pneumatic wheel (150mm) with a weight of 310g. I will follow the re-design of the Q2 tail wheel like in the Q-news
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By
Eugen Pilarski
· #55430
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Q1 Tail wheel diameter
Hello Q-Communitty, I am looking for a tail wheel for the Q1. Do you have a suggestion which one I could use. I read in the Q-news that pneumatic tyres would work particularly well. Here is an example
Hello Q-Communitty, I am looking for a tail wheel for the Q1. Do you have a suggestion which one I could use. I read in the Q-news that pneumatic tyres would work particularly well. Here is an example
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By
Eugen Pilarski
· #55418
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Q1 - Pitot pipe static system
Hi Q-community, anybody are available to send me a picture about the pitot pipe at BL34? Where the pipe will go out of the Canard? How long the tube should go out? Best regards Eugen Von meinem iPhone
Hi Q-community, anybody are available to send me a picture about the pitot pipe at BL34? Where the pipe will go out of the Canard? How long the tube should go out? Best regards Eugen Von meinem iPhone
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By
Eugen Pilarski
· #55415
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What epoxy, what foam
Some more details about foam and resin. https://aerobase.weebly.com/q1-bill-of-material---source--spec.html Best regards from Germany Eugen Von meinem iPhone gesendet
Some more details about foam and resin. https://aerobase.weebly.com/q1-bill-of-material---source--spec.html Best regards from Germany Eugen Von meinem iPhone gesendet
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By
Eugen Pilarski
· #55361
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[Quickie-1] Tail wheel support - steel/foam
Hello Chris, After you note I double check the quick head webside and found this Q-talk #12 information from Bob, please follow link. He had a issue after seven hours flying with his Q2. http://www.qu
Hello Chris, After you note I double check the quick head webside and found this Q-talk #12 information from Bob, please follow link. He had a issue after seven hours flying with his Q2. http://www.qu
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By
Eugen Pilarski
· #55226
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[Quickie-1] Tail wheel support - steel/foam
Hello Q-Community, What type of material is used for the tail wheel support? It’s a rod of 1.4310 (x10CrNi18-8) in US 301 (UNS S30100)? Which wheel diameter on the tail wheel would you recommend? A so
Hello Q-Community, What type of material is used for the tail wheel support? It’s a rod of 1.4310 (x10CrNi18-8) in US 301 (UNS S30100)? Which wheel diameter on the tail wheel would you recommend? A so
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By
Eugen Pilarski
· #55195
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Q1 - Fuel Cap - Filler Neck
Hello Q-Community, just a short question about the Fuel cap/fillet neck. Any proposal for a semi professional solution for that issue? Should they fix a part of the household bottle neck to the fusela
Hello Q-Community, just a short question about the Fuel cap/fillet neck. Any proposal for a semi professional solution for that issue? Should they fix a part of the household bottle neck to the fusela
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By
Eugen Pilarski
· #55105
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Q1 - Main wing - Flip tabel
Hello Q Community, Thank you for your messages and tips. I have now implemented it according to the procedure from a Q-talk #9 from 1983, attached the link to it. Just Duck tape, micro, resin, glass,
Hello Q Community, Thank you for your messages and tips. I have now implemented it according to the procedure from a Q-talk #9 from 1983, attached the link to it. Just Duck tape, micro, resin, glass,
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By
Eugen Pilarski
· #53632
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Q1 - Main wing - Flip tabel
Hi @ all, thanks for your comments and hints, after I spend two weekends to listen all Q-News letters and looks around for a solution that cover that issue. Currently the solution that Terry indicate
Hi @ all, thanks for your comments and hints, after I spend two weekends to listen all Q-News letters and looks around for a solution that cover that issue. Currently the solution that Terry indicate
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By
Eugen Pilarski
· #53549
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Q1 - Main wing - Flip tabel
Hello Q-Community, Im on my way to build the main wing, please find in the attachment picture from ailerons slot with 1 bid 45° with some peelply on the top. Additional to that it´s necessary to flip
Hello Q-Community, Im on my way to build the main wing, please find in the attachment picture from ailerons slot with 1 bid 45° with some peelply on the top. Additional to that it´s necessary to flip
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By
Eugen Pilarski
· #53543
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Fuel pump & condition inspection
Sam, did you have a part# from your pump and the filter? Best regards Eugen
Sam, did you have a part# from your pump and the filter? Best regards Eugen
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By
Eugen Pilarski
· #53206
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Quickie Q1 - Elevator Foam cut
Hello Q-Groupe, so far the Canard is cut out from blue foam. The next steps are to cut the elevator BL10, BL49 and BL88 form the blue foam. After study the foam cut section about the elevator, is not
Hello Q-Groupe, so far the Canard is cut out from blue foam. The next steps are to cut the elevator BL10, BL49 and BL88 form the blue foam. After study the foam cut section about the elevator, is not
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By
Eugen Pilarski
· #53068
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Quickie Q1 - Canard
David, thanks for that detail information end explain the interrelations. So the center section foam unit for the Canard is 20“ to 18 1/2“ (14“+ 4 1/2“) with the 0.7“ slope and has no elevator slots c
David, thanks for that detail information end explain the interrelations. So the center section foam unit for the Canard is 20“ to 18 1/2“ (14“+ 4 1/2“) with the 0.7“ slope and has no elevator slots c
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By
Eugen Pilarski
· #52913
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Quickie Q1 - Canard
Hello Q-Groupe, we are just about to cut the canard out of the foam. What is not clear to me at the moment is why the separation of the rear segments in the middle segment has to take place along line
Hello Q-Groupe, we are just about to cut the canard out of the foam. What is not clear to me at the moment is why the separation of the rear segments in the middle segment has to take place along line
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By
Eugen Pilarski
· #52886
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Quickie Q1 Canard and wing foam cut
Dear Q-Team, in the next step I would like to cut out the canard and wing units based on the blue foam. Which further openings in the wings or canard from your personal experience you would place? For
Dear Q-Team, in the next step I would like to cut out the canard and wing units based on the blue foam. Which further openings in the wings or canard from your personal experience you would place? For
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By
Eugen Pilarski
· #52626
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Q1 Fuselage comes up
Hi Q-Community, So far the glass is placed on the fuselage outside of my Q1. The foam for wing and canard is coming already from the supplier. The next steps will be to start up my DIY CNC Foam cutter
Hi Q-Community, So far the glass is placed on the fuselage outside of my Q1. The foam for wing and canard is coming already from the supplier. The next steps will be to start up my DIY CNC Foam cutter
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By
Eugen Pilarski
· #52365
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Q1 Fuselage comes up
Dear Q-list members, thank you very much for your notes! That’s great! From a German guy I got the original Q1 plans from 1981 and every time I picked up the roll of paper it’s fell like magic. Thank
Dear Q-list members, thank you very much for your notes! That’s great! From a German guy I got the original Q1 plans from 1981 and every time I picked up the roll of paper it’s fell like magic. Thank
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By
Eugen Pilarski
· #52311
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Q1 Fuselage comes up
Dear Q-Team, in the plans on Page 07-13 the fuselage outside glassing start, please find the link below Page 07-13 Did I understand the Q1 plans right, that only the area between STA 14.8 and STA 110
Dear Q-Team, in the plans on Page 07-13 the fuselage outside glassing start, please find the link below Page 07-13 Did I understand the Q1 plans right, that only the area between STA 14.8 and STA 110
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By
Eugen Pilarski
· #52285
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