Return-Path: Received: from anna.ana.com ([207.44.232.227]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Sat, 21 Aug 1999 02:00:59 -0400 Received: from gjpc (ppp138.creative.net [208.225.99.138]) by anna.ana.com (8.9.3/8.9.3) with SMTP id XAA29918 for ; Fri, 20 Aug 1999 23:04:22 -0700 (PDT) Message-ID: <004501beeb9b$774e21e0$06b8b6c6@gjpc> From: "Gerard J. Cerchio" To: Subject: The efficacy of Taxi Tests Date: Fri, 20 Aug 1999 23:06:01 -0700 X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Hello all, I have spent the last few days thinking about Dr Michael A Fopp's sad experience with his 320 and after having reported my very successful taxi tests I must say something here in our forum about his comments on high speed taxi testing. No one can accuse me of rushing head long into my project. Indeed, I have been constructing my aircraft for ten years. I still have not flown N333EX due to testing and detail after detail. I may be ready to flight test my project next week, given no more details show up. CJ Stephens, a professional test pilot will perform the flight test, not yours truly. Every flight test book I have read extols the virtues of high speed taxi tests. To me, they just make great sense. I am testing a vehicle. That vehicle has very specific phases of operation. Phase one, it must sit on its wheels and not collapse. Phase two, it must turn its propeller and not catch fire. Phase three, it must taxi to a place where it is safe to perform phase four. Phase four, it must turn its propeller with sufficient force and consistency to hurl said vehicle into the air. Phase five, it must hurl itself down a runway with sufficient speed for the airfoil to perform said task of hurling said vehicle into the air. Phase 6, it must enter the air. Now, I have spent some time getting to phase five. I personally believe that if Dr. Fopp had spent more time in Phase four, his calamity may have been prevented. When I decided to it was time to taxi test 3EX I was bent on seeing if the aircraft would perform at speeds I had not ventured to during phase three taxi. My first desire was to see the airspeed gage ride above the peg. I did this on the way to the runway. I did not notice any vibration or loss of control so I requested the tower for permission to use the runway for the test. My second goal was to reach 40 knots with the throttle full to the fire wall. Given how much testing that it took to get that throttle to the firewall, see earlier posts, I was quite happy to be traveling at freeway speed down a runway. I believe that if I was hell bent in flight testing the aircraft at that time that I may have well been unable to counter an uncontrolled shimmy in the gear given how quickly the aircraft reached 40 knots. But being that my only objective was to reach a comfortably fatal speed that I would have been ready to pull throttle and apply breaks, My second taxi run was to achieve speed that would be the projected stall for the aircraft. I chose 60 knots, reached the speed, maintained it for a while and then backed off. Still not a problem detected, I planed for a greater then a rotation velocity taxi with flaps in a cruise configuration giving me a margin of safety for saying on the ground. Again, success. I have to add that before I even taxied, that I had sent my strut to Nieco for a full overhaul and update. I did this because A) I had one of the older struts in the word and B) I bled all the nitrogen out of the strut earlier to keep the plane level for setup and testing. SOOO, I recommend everyone rebuild their struts immediately, and by all means taxi, taxi, taxi. (I did one more for good measure). Gerard Cerchio >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML homepage: http://www.olsusa.com/Users/Mkaye/maillist.html