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		tigerrick(at)mindspring.c Guest
 
 
 
 
 
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				 Posted: Mon Apr 17, 2006 1:25 pm    Post subject: prop pitch question | 
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				Hi, Thomas!
 
 I also have a '76 that is now equipped with a 63" pitch Sensenich, and 
 it does just fine high and hot when flown right.  Dave Fletcher 
 maintains that the 62" is the ideal for most applications, and I don't 
 doubt him at all.  I don't have the PF exhaust either, but I'm a nut 
 about engine maintenance, leaning, and a third flap on take off, so I've 
 been happy with the 63" while getting all out of the O-360 that it has 
 to offer.
 
 The 64" can be repitched down to 63", but it sounds like you'd be better 
 off with the 62" - fly it awhile, and if you want a couple more knots at 
 cruise and a bit less climb, you could pitch it up an inch.
 
 Just my opinion, obviously.
 
 Rick Lindstrom
 N74613
 N4526B
 N9738U
 
 airman(at)appledumplings.com wrote:
 
  	  | Quote: | 	 		  
 
 Originally sent this to the grumman-gang list with an "unacceptable  
 subject line" and got bounced by the gg-list nazi. figured I would  
 try here.
 
   
 
 >I bought a 76 tiger and am getting a new sensenich prop. The  
 >problem is that the only pitch that they have is the 64" pitch prop  
 >available ... i was looking at 62"  or  63" pitch but they say 6-12  
 >weeks. Repitching is extra So either I go with the 64   or i go  
 >pick it up and  do the prop later.
 >It doesnt have any performance mods like the power flow or anything  
 >so I am unsure what the max pitch I  should consider.
 >I have no experience in tigers so recommendations would be  
 >helpful.   I plan to use it for my ifr training and flights back  
 >and forth to in-laws  about 4-500 miles. I also will be going to a  
 >sea level airport of 2300' long on and off.
 >Thanks in advance,
 >Thomas
 >N74225
 >    
 >
 
  
  
  
 
 
   
 
 
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		flyv35b(at)ashcreekwirele Guest
 
 
 
 
 
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				 Posted: Tue Apr 18, 2006 6:09 am    Post subject: prop pitch question | 
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				With your longer x-country flights I'd go with the 64" and see how it works. 
 You can always repitch it later on or add the PF exhaust and then you 
 wouldn't want to.  I doubt if a 2300 ft. strip will be a problem with a 64" 
 pitch prop unless there are tall obstructions right off the end.  I have 
 flown a Tiger in an out of a 1500 ft. strip in the past with a 63" pitch.
 
 Cliff  A&P/IA
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		GrummanDude
 
 
  Joined: 15 Jan 2006 Posts: 926 Location: Auburn, CA
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				 Posted: Tue Apr 18, 2006 10:52 pm    Post subject: prop pitch question | 
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				Most Tigers won't do very well with a 64" pitch.   The original blank, if I'm 
 not mistaken, is made with a 62" pitch, so, it's already been twisted 2 
 inches.   If you twist it back 2 inches, that's 4 inches it's been twisted already. 
   It can only be twisted a total of 8 inches ........    So, with that said, 
 
 Depending on how strong your engine is, I'd see if I could get a custom twist 
 with the twist at 64-62-60.   The average is 62 which is a legal pitch for 
 the Tiger.   But, you get back about 75 to 100 rpm and you don't give up much in 
 cruise.   maybe 2 knots.
 
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		bruce.smith(at)york.com Guest
 
 
 
 
 
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				 Posted: Wed Apr 19, 2006 4:07 am    Post subject: prop pitch question | 
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				Gary,
 
 What is the position of the measurements you have listed below for 
 pitch. I'm guessing that the 62 is midpoint on the blade. Correct?
 
 Bruce
 
 Depending on how strong your engine is, I'd see if I could get a custom 
 twist
 with the twist at 64-62-60.
 
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		GrummanDude
 
 
  Joined: 15 Jan 2006 Posts: 926 Location: Auburn, CA
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				 Posted: Wed Apr 19, 2006 10:59 am    Post subject: prop pitch question | 
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				In a message dated 4/19/06 5:08:00 AM, bruce.smith(at)york.com writes:
  	  | Quote: | 	 		   64 (first third, near the hub) - 62 (middle) - 60 (tip).
  
  
 
 | 	  
 And, I should have said you'll get back about 150 rpm for climb.   
 
 A certain someone I know had one of the new Cheetah Sensenich props pitched 
 63-62-61, gained 200 fpm rate of climb AND gained 2 knots.   But, he was able 
 to run WAY over redline at 7500 feet.     Now, he can turn redline at 9000 
 feet.
 
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		bruce.smith(at)york.com Guest
 
 
 
 
 
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				 Posted: Wed Apr 19, 2006 11:37 am    Post subject: prop pitch question | 
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				I would imagine that this is in a Cheetah with the HC mod that's been 
 further massaged by the folks at Lycon. I wonder what that kind of an 
 engine might produce on a dyno...
 
 Bruce
 
 TeamGrumman(at)aol.com said the following on 4/19/2006 2:57 PM:
  	  | Quote: | 	 		   
  In a message dated 4/19/06 5:08:00 AM, bruce.smith(at)york.com writes:
    
 > 64 (first third, near the hub) - 62 (middle) - 60 (tip).
 >     
 
  And, I should have said you'll get back about 150 rpm for climb.   
 
  A certain someone I know had one of the new Cheetah Sensenich props pitched 
  63-62-61, gained 200 fpm rate of climb AND gained 2 knots.   But, he was able 
  to run WAY over redline at 7500 feet.     Now, he can turn redline at 9000 
  feet.  
 
   
   
   
 
    
 
 | 	 
 
 
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		GrummanDude
 
 
  Joined: 15 Jan 2006 Posts: 926 Location: Auburn, CA
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				 Posted: Wed Apr 19, 2006 8:38 pm    Post subject: prop pitch question | 
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				In a message dated 4/19/06 12:37:54 PM, bruce.smith(at)york.com writes:
  	  | Quote: | 	 		   I would imagine that this is in a Cheetah with the HC mod that's been
  further massaged by the folks at Lycon. I wonder what that kind of an
  engine might produce on a dyno...
  
  Bruce
  
 
 | 	  
 actually, no.   This engine has 1500+ SMOH.   77 Cheetah.   Nothing trick on 
 this plane except a red rudder cap.   Trues at 132 knots.
 
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AuCountry Aviation
 
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		aa1bflyboy(at)msn.com Guest
 
 
 
 
 
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				 Posted: Wed Apr 19, 2006 8:53 pm    Post subject: prop pitch question | 
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				Has anyone evr done this with a prop for an AA1x model?
 
 Steve Roberts - AA-1B N9664L (at) ILG
 
  In a message dated 4/19/06 5:08:00 AM, bruce.smith(at)york.com writes:
  > 64 (first third, near the hub) - 62 (middle) - 60 (tip).
  >
  >
 
 And, I should have said you'll get back about 150 rpm for climb.
 
 A certain someone I know had one of the new Cheetah Sensenich props pitched
 63-62-61, gained 200 fpm rate of climb AND gained 2 knots.   But, he was 
 able
 to run WAY over redline at 7500 feet.     Now, he can turn redline at 9000
 feet.
 
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		FLYaDIVE(at)AOL.COM Guest
 
 
 
 
 
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				 Posted: Thu Apr 20, 2006 3:15 am    Post subject: prop pitch question | 
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				Steve:
 
 ALL PROPS have different pitches at different stations along their length.  
 This is not a speed mod or a magic dust trick.
 
 The only trick in picking a pitch is to go has high as you can without 
 failing the ground static check.
 
 Barry
 "Chop'd Liver"
 ============================
 
 In a message dated 4/20/06 12:54:23 AM Eastern Daylight Time, 
 aa1bflyboy(at)msn.com writes:
 
  	  | Quote: | 	 		   
   
   Has anyone evr done this with a prop for an AA1x model?
   
   Steve Roberts - AA-1B N9664L (at) ILG
   
   
   
   
   In a message dated 4/19/06 5:08:00 AM, bruce.smith(at)york.com writes:
   
   
    > 64 (first third, near the hub) - 62 (middle) - 60 (tip).  
   And, I should have said you'll get back about 150 rpm for climb.
   
   A certain someone I know had one of the new Cheetah Sensenich props 
 pitched  63-62-61, gained 200 fpm rate of climb AND gained 2 knots.   But, he was 
 | 	  
  	  | Quote: | 	 		    able to run WAY over redline at 7500 feet.     Now, he can turn redline at 
 9000
 | 	  
 
 
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		bruce.smith(at)york.com Guest
 
 
 
 
 
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				 Posted: Thu Apr 20, 2006 3:38 am    Post subject: prop pitch question | 
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				Barry,
 
 I thought this was the case, but had never heard it expressed in this 
 manner. It was always that this Tiger has X pitch or this Cessna has Y 
 pitch.
 
 Thanks.
 
 Bruce
 
 FLYaDIVE(at)aol.com said the following on 4/20/2006 7:15 AM:
  	  | Quote: | 	 		   
 
  Steve:
 
  ALL PROPS have different pitches at different stations along their length.  
  This is not a speed mod or a magic dust trick.
 
  The only trick in picking a pitch is to go has high as you can without 
  failing the ground static check.
 
  Barry
  "Chop'd Liver"
  ============================
 
  In a message dated 4/20/06 12:54:23 AM Eastern Daylight Time, 
  aa1bflyboy(at)msn.com writes:
 
    
 > 
 >  
 >  Has anyone evr done this with a prop for an AA1x model?
 >  
 >  Steve Roberts - AA-1B N9664L (at) ILG
 >  
 >  
 >  
 >  
 >  In a message dated 4/19/06 5:08:00 AM, bruce.smith(at)york.com writes:
 >  
 >  
 >   > 64 (first third, near the hub) - 62 (middle) - 60 (tip).  
 >  And, I should have said you'll get back about 150 rpm for climb.
 >  
 >  A certain someone I know had one of the new Cheetah Sensenich props 
 >     
  pitched  63-62-61, gained 200 fpm rate of climb AND gained 2 knots.   But, he was 
    
 >  able to run WAY over redline at 7500 feet.     Now, he can turn redline at 
 >     
  9000
    
 >  feet.
 >     
   
   
   
 
    
 
 | 	 
 
 
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		flyv35b(at)ashcreekwirele Guest
 
 
 
 
 
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				 Posted: Thu Apr 20, 2006 5:20 am    Post subject: prop pitch question | 
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				Yes there are different blade ANGLES specified for a PARTICULAR pitch at 
 ever station.  What Gary is saying that these specific angles are deviated 
 from to essentially achieve what would be the angle for a 64" pitch at the 
 inner third and changing to what would be a 60" pitch angle at the tip. 
 This is not common and some prop shops simply won't do it, saying they can 
 legally deviate from the specified angles for a particular pitch.
 
 Cliff
 ---
 
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		flyv35b(at)ashcreekwirele Guest
 
 
 
 
 
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				 Posted: Thu Apr 20, 2006 5:56 am    Post subject: prop pitch question | 
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				Should have said "they can't legally deviated"
 ---
 
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		aa1bflyboy(at)msn.com Guest
 
 
 
 
 
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				 Posted: Thu Apr 20, 2006 8:20 am    Post subject: prop pitch question | 
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				Yeah that's what I though too..
 
 Do a lot, get a little;
 Do a little, get a lot;
 Do nothing, get it all.
 Steve Roberts - AA-1B N9664L (at) ILG
 
 ----Original Message Follows----
 From: Bruce Smith <bruce.smith(at)york.com>
 Reply-To: teamgrumman-list(at)matronics.com
 To: teamgrumman-list(at)matronics.com
 Subject: Re: prop pitch question
 Date: Thu, 20 Apr 2006 07:37:58 -0400
 
  
 Barry,
 
 I thought this was the case, but had never heard it expressed in this
 manner. It was always that this Tiger has X pitch or this Cessna has Y
 pitch.
 
 Thanks.
 
 Bruce
 
 FLYaDIVE(at)aol.com said the following on 4/20/2006 7:15 AM:
  > 
  >
  > Steve:
  >
  > ALL PROPS have different pitches at different stations along their 
 length.
  > This is not a speed mod or a magic dust trick.
  >
  > The only trick in picking a pitch is to go has high as you can without
  > failing the ground static check.
  >
  > Barry
  > "Chop'd Liver"
  > ============================
  >
  > In a message dated 4/20/06 12:54:23 AM Eastern Daylight Time,
  > aa1bflyboy(at)msn.com writes:
  >
  >
  >> 
 <aa1bflyboy(at)msn.com>
  >>
  >>  Has anyone evr done this with a prop for an AA1x model?
  >>
  >>  Steve Roberts - AA-1B N9664L (at) ILG
  >>
  >>  
  >>
  >>
  >>  In a message dated 4/19/06 5:08:00 AM, bruce.smith(at)york.com writes:
  >>
  >>
  >>   > 64 (first third, near the hub) - 62 (middle) - 60 (tip).
  >>  And, I should have said you'll get back about 150 rpm for climb.
  >>
  >>  A certain someone I know had one of the new Cheetah Sensenich props
  >>
  > pitched  63-62-61, gained 200 fpm rate of climb AND gained 2 knots.   
 But, he was
  >
  >>  able to run WAY over redline at 7500 feet.     Now, he can turn redline 
 at
  >>
  > 9000
  >
  >>  feet.
  >>
  >
  >
  >
  >
  >
  >
  >
  >
  >
  >
  >
  >
  >
  >
  >
 
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		GrummanDude
 
 
  Joined: 15 Jan 2006 Posts: 926 Location: Auburn, CA
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				 Posted: Thu Apr 20, 2006 10:16 am    Post subject: prop pitch question | 
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				In a message dated 4/20/06 4:16:30 AM, FLYaDIVE(at)AOL.COM writes:
  	  | Quote: | 	 		   ALL PROPS have different pitches at different stations along their length.=A0
  This is not a speed mod or a magic dust trick.
 
 | 	  
 true, and not true.
 
 for a 64" pitch, there are specific angles, in degrees, for each station.  
 For a 62" pitch likewise.   Making an airfoil that conforms to the different
 primary pitches, really changes the way the prop performs.  
 
 It's used in racing at Reno all the time.
 
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AuCountry Aviation
 
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		FLYaDIVE(at)aol.com Guest
 
 
 
 
 
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				 Posted: Thu Apr 20, 2006 6:12 pm    Post subject: prop pitch question | 
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				In a message dated 4/20/06 2:17:10 PM Eastern Daylight Time, 
 TeamGrumman(at)aol.com writes:
 
  	  | Quote: | 	 		   
   
   > ALL PROPS have different pitches at different stations along their 
 length.> A0
 | 	  
  	  | Quote: | 	 		    > This is not a speed mod or a magic dust trick.
   >
   >
   
   true, and not true.
   
   for a 64" pitch, there are specific angles, in degrees, for each station.  
   For a 62" pitch likewise.   Making an airfoil that conforms to the 
 different
 | 	  
  	  | Quote: | 	 		    primary pitches, really changes the way the prop performs.  
   
   It's used in racing at Reno all the time.
 ===============================
 | 	  
 So ... Isn't that what I said?
 
 Chop'd Liver rides again!
 
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		GrummanDude
 
 
  Joined: 15 Jan 2006 Posts: 926 Location: Auburn, CA
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				 Posted: Thu Apr 20, 2006 9:31 pm    Post subject: prop pitch question | 
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				In a message dated 4/20/06 7:12:51 PM, FLYaDIVE(at)aol.com writes:
 
  	  | Quote: | 	 		   So ... Isn't that what I said?
  
 Oh, hell, I guess.   From your understanding of what I said, that is what you 
 | 	  
 said.   Yes,  "ALL PROPS have different pitches at different stations along 
 their length."  I don't think you understand the concept of variable twist 
 along the blade as used by racers with fixed pitch props. That is what I was 
 talking about.   And that is what Cliff was referring to.   It really isn't worth 
 trying to explain.   
 
 Let's just say a stock Cheetah Sensenich prop Model 74DM7S10-1.5-61P (61 inch 
 pitch) on a Cheetah that trues at 128 knots (at 5500 feet and 2650 rpm) and 
 has trouble pulling over 2700 rpm at 10,000 feet, when given a custom twist 
 with an average 62 inch pitch across the blade, GAINED 200 fpm rate of climb at 
 an airport at 2000 AGL, Trues at 132 knots (at 5500 feet and 2650 rpm) and can 
 still turn 2700 rpm at 10,000 feet, well.....   
 
 Anytime something can be done to increase climb rate, increase true airspeed, 
 and not give up horsepower (RPM) at altitude by over loading the prop, I'd 
 say that's a magic dust trick.
 
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