RE: CERMARK F-18 HORNET, BUILT IT BETTER, STRONGER, AN... - 12/2/2007 5:29:06 PM
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TXKflier
Posts: 64
Joined: 1/24/2006 From: Texarkana,
TX, USA Status: offline
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You might find this interesting. I just did an Internet search for the words "Cherokee horizontal stablizer balance". One of the pages I found was about a lawsuit concerning the fatal crash of a recently serviced Piper Cherokee. If you read through it, you'll see where the stabilator was supposed to be balanced between 0 and minus 40 inch-pounds, which is nose heavy. But, the mechanic entered +20.125 inch-pounds on the worksheet, which would be tail-heavy. Read the expert's analysis of the evidence, their description of the sequence of events, and how rapidly things went wrong once the flutter started. http://caselaw.lp.findlaw.com/cgi-bin/getcase.pl?court=6th&navby=case&no=00a0279p The article was especially interesting to me for the following reasons: 1. My dad owned a 1972 Cherokee Arrow and I flew it for about 150 hours from 1974 to 1978. 2. Someone on RCU who didn't think R/C stabilators needed to be balanced wrote that the stab on a Cherokee would sit trailing edge low. If it did, I suspect a spring pulled it that way. Of course, when the plane's control lock is installed, the trailing edge will be low. In that position: (1) It keeps the plane from taking off if the pilot forgets to remove it. (2) It might help prevent high winds from flipping the plane over. (3) It gets the yoke out of the way for entry and exit. 3. The mechanic used an uncalibrated scale to measure the CG of the stab. 4. I'm a calibration technician in a US Army calibration lab. We calibrate scales, torque wrenches, etc. And finally, the quote that really hit home... "The airplane . . . flew a long time before [Plane Perfection] touched it, and it didn't last very long after . . . " And, unfortunately, three people died..
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