Dear all, Unless somebody has a bright idea I think I have come to the end of planning to install the fuel tank without bonding it in. I now have a tightly fitting bed of 2 layers of bid and a quanti
New day, new courage. Thank you. I agree, Frans, no movement allowed and no antistatic (conducting) materials - that was a wrong turn I took. There exists a "triboelectric series" (for instance: http
Concerns G-BWDP / Harold Linke in the year 2000. There are pictures of the aircraft taken in 2006 so it was repaired. Not much information searching in archives or googleing. There has been a lot of
Checking with John and Roger at the factory re tank installation. 1. The last of the original (2004) Ltd crew is retiring and having its last day at the office today. The end of a period - again. Rog
Hi William, No - not mentioned. But assuming that stresses add up I would personally try to apply some relief as Ron Parigoris did. And maybe avoid opportunities for parking on hot asphalt when there
Good evening, I would like to ask a question regarding floor clearance in the (XS) monowheel tunnel from the front of the tank back to the inboard bagage bay supports. How low does the flap drive rod
Hi Craig, No, I hadn't considered it and after the interchange re Monowheel Flap Operation I think I will stick with the build manual. I will go ahead with expecting 4 cm clearance as nobody on the l
Thank you Craig, Minimum clearance of bend in the cross tube noted, drive rod most likely better - I should be ok. Front rudder cable height noted - I'm thinking of doing Ian Rickard's rudder pedal p
Hi Rowland, In 2008 I found a German language forum discussion concerning the Ducati regulator. Writer "Arrow" seemed to know what he was talking about. I reported - http://www.sarangan.org/www/mhona
I should have said, actually: when average input voltage (G's) gets above some level, which requires C powered (which by itself only provides a bias current). Jan
Having a bad cold, can't sleep, so here. Fiddling with the cockpit module - before bonding in - I found that the rudder cable pulleys should really be oriented about 4 degrees (1 in 15) --From vertic
I can think of relative humidity and storage temperature as variables to which Ampreg 21 may be more sensitive than Ampreg 20. I have no experience with it. After trial and error I now use SP106 for
Hi Malcolm, I studied the drawings a while ago and compared to Rotax. I also visited the Ulpower stand at Aero Friedrichshafen. Items: 1. - used as is with standard exhaust and standard muffler with
Not that I know anything about the subject, but several Cherry builders in NL have been flying with BMW boxer engines for quite a few years. http://spang-air.de/e/html/bmw_-_engine.html http://www.ta
From your description I would still suspect the return line. Is there a 1-way valve in there? A way to test it would be to connect the forward line (from the pumps) directly to the return line using
There is information in the total flow from the pump(s). Jos O. once mentioned that one of his pre-flight checks was a total forward flow of 120 l/h or so (Rotax 914). Anything less would be an early
This is still in the future for me, but I think my plan is: - from wing conduit outlet behind the spar over the spar (under fairing) to in front of spar - connections in front of spar - into fuselage
Introduction of fluorination was in April 1997: http://www.sarangan.org/www/mhonarc/mharc/html//europa-list/1997-08/msg00096.html I have assumed that my tank from the year 2000 was treated and did no