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![]() Ron, do you judge from this that the Velocity (or the pusher/canards in general) have basic design issues (such as the Lancair's low speed regime history)? On Fri, 31 Oct 2008 17:58:28 -0700, Ron Wanttaja wrote: It's funny you should ask, because that was one of the questions I was hoping to answer when I got into homebuilt accident analysis about five years ago. Still haven't answered it. There are so many factors involved that I could spend years of full-time work trying to dig them out. The fleet size of the Velocity is still relatively low, for example, and as well all know, one or two extra accidents can cause a disproportionate change. I dug a bit deeper into my database, and extracted the accident-cause data for about 20 homebuilt types. As I mentioned on my last post, the Velocity has an accident rate generally higher than most. Yet, the Velocity had nearly the LOWEST "stick and rudder error" rate. About 43% of RV-6 accidents involved the pilot's handling of the aircraft, vs. only 29% of the Velocities. HOWEVER (geeze, there's ALWAYS a "however" when you analyze accident statistics), the pilots in the Velocity accidents had about 25% more flight hours than those involved in RV accidents, and *four times* the hours than the average homebuilder involved in an accident. Lower rates because they're easier to fly...or because more-experienced pilots are flying them? My analysis method is a bit different from the NTSB's, too. I look for the first major event of the accident string, which means that if the engine quits, I attribute the accident to the engine quitting. The NTSB works a bit differently. If the investigator thinks the pilot should have been able to safely land the aircraft despite the engine failure, the cause of the accident is listed as pilot error. So my "pilot failure" category does NOT take into account the difficulty of handling the aircraft in an emergency situation. While my stats may show the pilot error rate for the Velocity to be lower, the NTSB's may not. Ron Wanttaja Great work and thanks! |
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