Return-Path: Received: from www05.netaddress.usa.net ([204.68.24.25]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with SMTP id com for ; Thu, 14 Jan 1999 02:43:10 -0500 Received: (qmail 11349 invoked by uid 60001); 14 Jan 1999 07:41:54 -0000 Message-ID: <19990114074154.11348.qmail@www05.netaddress.usa.net> Date: Thu, 14 Jan 1999 07:41:54 From: Dan Schaefer To: lancair.list@olsusa.com Subject: Props, CS vs fixed pitch X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> A comment in response to Sven (SE-XOP) regarding props. I'm not sure what kind of terrain and environment you are accustomed to flying from, Sven, but here in the Western US, it's quite common to find yourself stopping for gas at an airport sitting at an altitude up at 5000 to 6000 ft. and often in the summer (when one is likely to be out and about going somewhere) where the temperatures can easily be 90 degrees (F) and higher. I've had my share of rejected takeoffs back when I was flying behind a fixed pitch prop and my plane's seats have the marks to prove it! Since I changed to a CS unit (MT two-blade), the problem went away. I may not go any faster in cruise (though I actually do, a bit - reflected in about a 10% higher fuel burn, indicating that I'm making, and using, more power) but I'll take the extra performance on takeoff any day!! Just for reference, with a wooden, fixed pitch prop, I could get no more than about 2350 RPM for a sealevel takeoff and takeoff was a bit on the anemic side, to say the least. With the CS unit, I always get 2650-2700 RPM and the takeoffs are now quite sprightly affairs. Do the numbers; that's better than a 10% increase in takeoff horsepower (HP = T x RPM / K [K is a constant around 5200 for these regimes]). Nearly all of it is "excess power" needed to climb, which relates to better takeoff performance. Cheers, Dan Schaefer