X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Sat, 12 Jan 2013 13:17:48 -0500 Message-ID: X-Original-Return-Path: Received: from snt0-omc3-s10.snt0.hotmail.com ([65.55.90.149] verified) by logan.com (CommuniGate Pro SMTP 6.0.1) with ESMTP id 6008956 for lml@lancaironline.net; Sat, 12 Jan 2013 11:34:06 -0500 Received-SPF: pass receiver=logan.com; client-ip=65.55.90.149; envelope-from=n320g@hotmail.com Received: from SNT145-DS9 ([65.55.90.135]) by snt0-omc3-s10.snt0.hotmail.com with Microsoft SMTPSVC(6.0.3790.4675); Sat, 12 Jan 2013 08:33:30 -0800 X-EIP: [nsTdpIZ1bHRqzbd8ajkuKH0fDlbraxDD] X-Originating-Email: [n320g@hotmail.com] X-Original-Message-ID: X-Original-Return-Path: n320g@hotmail.com From: "Airplane buddies" X-Original-To: "Lancair Mailing List" References: In-Reply-To: Subject: Re: [LML] Re: here's an original 235 builder/flyer responding X-Original-Date: Sat, 12 Jan 2013 08:33:19 -0800 MIME-Version: 1.0 Content-Type: text/plain; format=flowed; charset="iso-8859-1"; reply-type=response Content-Transfer-Encoding: 7bit X-Priority: 3 X-MSMail-Priority: Normal Importance: Normal X-Mailer: Microsoft Windows Live Mail 15.4.3555.308 X-MimeOLE: Produced By Microsoft MimeOLE V15.4.3555.308 X-OriginalArrivalTime: 12 Jan 2013 16:33:30.0280 (UTC) FILETIME=[8E362280:01CDF0E2] Dan, I have met you a few times up in Oregon and around California. I remember your 235 and thought you had done a great job with it. It was nice to read the whole story with the history. Like you I built mine before the internet was in wide use, the only help you got was on the telephone with the factory, flyins or project visits. My flight in the red 320 was with Goetz, Linda Neibauer wrote up the sale of my kit, they were still in Santa Paula in 1989. After some training in Redmond, Goetz took me for a check-out flight and recommended I get another 10 hours. Goetz flew the company LIV down to Chino in 1999, checked out my airplane, gave me a couple of trips around the pattern, stated I still need at least another 10 hours of training. Luckily I met Chuck Moon at Chino who let me fly with him in his beautiful L360 and then coached me through several flights when mine was first flying. I have managed to fly mine over 1300 hours, made it to OSH a half dozen times, Sun-N-Fun once, all over the mid-west and and West coast. All of those trips were around 200 mph and under 9GPH. Most of my maintenance has been dealing with the landing gear and hydraulic systems. For me the journey has been a very pleasurable one, I am so thankful that Lance and Don spent all of those years designing, developing and refining an airplane that I could afford to build and fly, that is still in my humble opinion the prettiest airplanes around. ("wee airplane" to quote Grayhawk) It is nice to hear from one of early guys who mostly just reads the posts on LML and smiles at the comments being made. Gary N320GG L320 1300 hours -----Original Message----- From: Dan Schaefer Ok, listers, here's an original 235 builder/flyer responding to the suggestion that maybe we ought chime in re: Our 235 lawn darts - so here goes. I built mine starting in about '86 - '87 (I think) when Lance was still in LA, before the company moved to Santa Paula and before Don Goetz started trying to squeeze a 320 into the airframe. This was in the days when the build manual was still partly in draft and corrections were arriving in the mail every week. First flight was in '93 done utilizing the then factory service of having an experienced factory pilot (Mike DeHate) do the first flight, explore the envelope and check me out. I'm still flying N235SP and have over 1000 hours on it. (That doesn't sound like a lot since '93 but work kept me out of country a bunch and after retirement to the north country, I don't fly much in the winters up here). I have used the airplane for simply boring holes, learning to fly formation with an ex-Navy carrier fighter pilot, and many of the requisite "$100 dollar hamburger runs". But also on quite a few reasonably long trips such as: Coeur d'Alene, ID (the town to which I retired) to LA, LA to Yellowstone, LA to Redmond, Or, etc. I run a Lyc. O-235-L2C with the Lycoming "helicopter" pistons (moderatly high-compression yielding maybe 120 to 125 HP) and run a two bladed electric MT C/S prop. On long trips, the airplane likes about 9,500 to 10,500 ft and for years I have averaged 164 knots in cruise. On the trips to Jellystone from LA I always carried a passenger (who ran to about 200 lbs), fishing gear and baggage for two guys for the week (limiting the baggage to a total of 50 lbs for structural reasons in the baggage bay). Of course, with that loading, takeoffs took more runway but once on cruise, there is very little difference in the speed or the handling. When I built the airplane, I had a partner who was 6' 1" and weighed about 205 lbs. to accomodate his size, we cut some of the passenger bottom seat-pan away (a factory suggestion), lowering his head by about two inches. His only comment was that he always had to be sure that he put on his headset with the mic towards the inside or it would hit the canopy side. My partner couldn't get his medical so we left the pilot's seat pan alone and I have to do the same too, but it's not a big deal. Like Grayhawk, after flying for a year or so, I arbitrarily moved my preferred cg range slightly forward - reason? - back in the mid '90's, there was also much talk about the airplane's probable spin recovery problems and I wanted as much rudder arm as plssible, just in case. I doubt if that reduces my cruise speed much due to elevator down-force as the airplane requires nose-down trim when going into reflex anyway, so the forward cg abets that requirement. To be factual, I did need to install slightly stronger pitch trim springs to have full trim authority at the flare for landing. My fuel tanks in the wings (11 gal each - header 11 gal as well) are located between the front and rear spars and between the inboard close-out rib and the second rib, which was moved a couple of inches outboard (with blessings from the factory). This was done for several reasons: First and foremost, I didn't like the idea of the inertia of the fuel all the way out to the wingtips as was designed. In a spin, centrifugal force would likely force all the wing fuel toward the tips exacerbating recovery difficulty - hopefully, it can only help inadvertent spin recovery - though I'm fully aware that a pattern stall/spin would be fatal. And not only in a Lancair. Second, with the fuel between the spars, burning off the fuel in the wings has little effect on cg travel. And third, I thought that trying to seal those bloody leading edges would be really tough. Whatever Lancair you are looking at to buy, I certainly recommend picking one that has the oleo nose strut. The original type required a lot of fiddling to keep it from going ape - s**t on landing and tearing up your engine mount. In my opinion they should all have been retrofitted by now. While I'm at it I'll add my 2c worth regarding the Stall, spin thread that's been going on - again! I do practice approach to stall recognition to remind myself what it feels like (my 235 gives a fairly good warning - even if one ignores the mushy controls). Though my Lancair doesn't seem to have a tendency to drop a wing at the stall, I know the envelope and don't push it. I've also always put in a bit of nose-down pitch trim in the pattern, just enough to require a noticable amount of back pressure on the stick, so the nose to drop enough to get my attention if I am distracted. I started doing this while flying in LA where it was common to be number six for landing - and four guys ahead were flying Cessna 150's! Dan Schaefer LNC2 N235SP 78 and still flying! -- For archives and unsub http://mail.lancaironline.net:81/lists/lml/List.html