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Union Thug wrote in news:1191867568.240364.167630
@o80g2000hse.googlegroups.com: On Oct 8, 8:16 am, Jay Honeck wrote: The tripping point in this discussion has been the absolute refusal by some participants to accept your last statement (and the point I've been making) as true and correct. The tripping point of Monty's post was that he seemed to feel that by boasting about your qualifications it would somehow discredit other posters (odd that he didnt mention his own qualifications ). You are pretty well endowed, aviation wise (I for one admire your passion and comitment to GA) , but Montie failed to explain how this makes your posts any more relevant than anyone elses. The gist of the thread *was* whether or not engine out practice was worth the expense (and risk) of this added engine wear. Unfortunately, that debate was lost in the muddle over whether the wear was actually occurring. The gist ought to be maintaining proficency with minimal wear and tear on your plane. Lycoming recomends no more than 100 degrees per minute temp decline in CHT. Those of you who fly with an engine analizer will find that this not difficult to acomplish and still get the benefit of practice. Take a look at glider tow operations. These guys do low speed high power climbs and then dive back to the pattern to do it again 4 to 5 times an hour all day long and most of them regularly make it to recomended TBO (The careful ones). Ask them how it is done sometime. I did it once upon a time and we were restricted to a min of 1500 revs (IIRC) during the initial descent. Before that we cracked a lot of jugs. OTOH, we had a lot of aerobatic airplanes and most of them went well beyond recommended TBO Not to mention one extraordinary J-3 that just went on forever. I think it did over 4,000 hours without even a top end and it lived in the pattern. bertie |
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