Return-Path: Received: from mail4.mgfairfax.rr.com ([24.93.67.51]) by ns1.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-64832U3500L350S0V35) with ESMTP id com for ; Sun, 2 Apr 2000 20:01:00 -0400 Received: from helms.mgfairfax.rr.com ([24.28.196.113]) by mail4.mgfairfax.rr.com with Microsoft SMTPSVC(5.5.1877.357.35); Sun, 2 Apr 2000 19:57:55 -0400 Reply-To: From: "richard helms" To: Subject: First flight, test pilot, builder tips Date: Sun, 2 Apr 2000 19:57:43 -0400 Return-Path: rhelms@mgfairfax.rr.com Message-ID: <085e45557230240FE4@mail4.mgfairfax.rr.com> X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> After 2 years 7 months N360RH made its first flight under the expert hands of Mike DeHate on 28 March. Since then it has accumulated about 10 uneventful hours. Performance is the impressive nominal for an IO360 powered LNC2. The experience of the first flight and those since has been very rewarding but almost overshadowing the first flight was what I learned during the final days leading up to it. I'd like to pass along some of that now. Recommendation: Definitely use an experienced test pilot but go with one who has had experience building the airplane and if possible find one who is an A&P. I found several pilots who were definitely capable and willing to test fly my airplane. Mike said he had no doubt that I could have safely flown the plane, if nothing abnormal had taken place. Mike has test flown about 50 Lancairs and has been doing that sort of thing for Piper for the last couple of years. Perhaps more importantly, you also want someone who has built them. In addition to the two place, Mike has also built a IV and a number of less stimulating airplanes in the pre composite ear of aviation. (This of course begs the question of why is he now flying an old radial engine Cessna and all I can say is it must be some age thing with him.) All of this made it so Mike brought the risks of the first flight down considerably. When everything was examined and tweaked he was ready for the first flight. On the following flights we slowly expanded the envelop, verifying performance and building overall confidence after each post flight examination. He was not in and out the same day. He was not a wing walker. He did not roll my investment on the first flight during a high speed low pass. What I got was an education from someone who worked with me to go through and fix a few things and improve many others over several days leading up to the flight and for a day or so after. I would strongly recommend that all builders find just that sort of building and flying attention to detail person to get your planes safely into the air. In the process, I learned a few builder/A&P tricks from Mike...several of which I would like to pass along now. 1. Rudder pedal springs - you can cut and re bend the end of springs purchased at your local hardware store. The key is getting springs with the proper tension to hold the pedals up and not become a resistance problem when pushing the other pedal or so wimpy that after a few pulls they look like wet spagetti. The length should be a little shorter than the distance at the neutral pedal position. So go for the right tension and then cut them down to length, bending a loop at the end to attach to whatever you have set up for it to attach to on the firewall. Also, don't add a rudder trim tab, fixed or adjustable until into flight test. You may not need it. If you have a slightly displaced ball you can to put a slightly stronger spring on one side to pull the rudder over as needed. I don't think I will need to do either but I will opt for the sping over the trim tab. 2. Getting way up the tail end of your airplane. I had run out to get something and came back to the hanger to see Mike waaaay back into the tail section of my plane. His whole body was in the baggage compartment. I normally crawl across the back seat, push both my arms forward through the aft hole and rest my chest on the "hatshelf" while cutting off circulation to my brain and arms. Here is how he did it. Sit facing the rear of the aircraft on the center glove box. Carefully raise each leg, extend it rearward and over the seat back. Put each foot on the bottom of the fuselage behind the seat backs while pulling yourself over the seat back, putting head in chest to clear the rear arch. (You may have to exhale and contort yourself to do this (I'm 5'11" and Mike is a little lower.) It gets really tight here but stick with it you might make it after all. Once past this pass-out-from-lack-of-oxygen-phase you lean forward placing one knee on each side of the tunnel as close as you can to the rear bulkhead. Once you are in it is definitely more comfortable than laying across the seat back and onto the "hatshelf". On the otherhand, you may have several days of a sore neck/back. Shorter builders will have less of a problem. 3. Less grunts from hinge pin removal/insertion: I used hinges for the lower cowl attachments to the fuselage and for attaching the foward deck to the fuselage sides. An easy way to grip the wire which does not mark up the wire with plyer grip marks and is less stressful on the hands and likely to bend the wire is to use the plyers but the opposite side you would normally grip. Some plyers cut on that side so be careful. The needle nose plyers I have are perfect. Mine have flat surfaces which make griping the wire and pushing it in without bending it a piece of cake. Take your time, a couple of inches at a shove and they are in in no time with a lot less effort. I don't have the numbers on my CG range with me now but a pilot of proper weight brings it .2 inch into the forward end of the revised CG range. This will now be my excuse for not needing to go on a diet ever again. The good news is that I don't think my wife owns anything with sufficient density to move the CG aft of the rear most safe position. Thankfully the baggage compartment was not made any larger. (I have the long mount.) Final recommendation: Don't use the single strand control cable for anything important. It will break or come off whatever it is attached to at the end. I replaced those that I had with threaded ends, except the non critical RAM air and the cabin heat valves. When rigging the RAM air valve I knew I only had about an inch of pull to get a full 90 degree throw on the valve. So when I pulled it at about 6500 feet and got a whopping 1.5 inches of additional manifold pressure I just knew deep down inside that I could get MORE RAM pressure out of the bugger if I just pulled it a little more. When I stopped pulling and held up about 24 inches of cable to take a look at Mike said, "well, what are you going to do with it now." Saying nothing I immediately shoved it back in the panel which of course drew the comment about it not working again until we are on the ground and pleadings to not do that with any of the other controls. It is at such moments that Mike will utter a phrase I have heard no one else use but all probably understand...."Oh Hockey Puck!" In addition to a very tolerate family and Mike I would like to thank Orin, Doug and Mark at Lancair for all their help and advice during the buying and building process. I am one who thinks the manuals for the 320 left a great deal to the wrong imaginations but the one thing that made up for it was the truly outstanding technical support. They were always there and always helpful. Let us do hope however, that the Legacy sets a higher standard for builder manuals/revisions. I should also thank Marv and all of you who have contributed to the builder discussion Marv started. The building process was much more productive because of it. Richard Helms N360RH >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html Builders' Bookstore: http://www.buildersbooks.com/lancair Please send your photos and drawings to marvkaye@olsusa.com. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>