---------------------------------------------------------- TeamGrumman-List Digest Archive --- Total Messages Posted Thu 04/29/10: 10 ---------------------------------------------------------- Today's Message Index: ---------------------- 1. 04:18 AM - N119ST Jaguar (brian sandberg) 2. 06:09 AM - Re: Re: AG5B Jaguar (Hosler, John) 3. 06:24 AM - Re: Re: AG5B Jaguar (923te) 4. 03:00 PM - Re: TeamGrumman-List Digest: 5 Msgs - 04/28/10 (Davesbox1@AOL.COM) 5. 04:09 PM - Re: Re: AG5B Jaguar (teamgrumman@AOL.COM) 6. 04:48 PM - Re: Re: AG5B Jaguar (Kevin Lancaster) 7. 06:10 PM - Re: Re: TeamGrumman-List Digest: 5 Msgs - 04/28/10 (923te) 8. 09:06 PM - Re: Re: TeamGrumman-List Digest: 5 Msgs - 04/28/10 (teamgrumman@AOL.COM) 9. 09:14 PM - Re: Re: AG5B Jaguar (teamgrumman@AOL.COM) 10. 10:01 PM - Re: Re: AG5B Jaguar (Kevin Lancaster) ________________________________ Message 1 _____________________________________ Time: 04:18:05 AM PST US From: brian sandberg Subject: TeamGrumman-List: N119ST Jaguar Sounds great. I'm reading through 7 months worth of teamgrumman digests an d eagerly awaiting my first flight in more than 8 months=2C the longest str etch I've gone since 1998. -Brian Subject: N119ST Jaguar From: teamgrumman@aol.com I've been working on installing the Jaguar cowling on 119ST for a week now. Other than the owner=2C no one else knows that 119ST was the plane I used for all of my original company testing. 119ST has had 6 different prototy pe cowlings=2C 3 different kinds of exit ramps=2C and 2 different versions of air intakes tested on it. I used 119ST for a year way-back-when to test a bunch of ideas. Check out pict 030.jpg. I also had the cowling that is now on N1976T on 119ST about 3 years ago. Maybe it's my familiarity with the plane or maybe that after installing 3 c owlings in as many months=2C but=2C this one is going really smooth. The t rim lines on this cowling are very close to the planes mounting flange. Th is plane has one shim (I got two responses from you guys on shims and dista nces to the spinner=2C thanks) on each of the top mounts and the distance t o the spinner is just a shade under 40 inches. It's got to be differences in bushings and mounts . . . . but=2C I digress. The cowling should be all trimmed up by tomorrow. The missing baffles shou ld be here this week also. Then=2C all the rest of the details. _________________________________________________________________ Hotmail is redefining busy with tools for the New Busy. Get more from your inbox. http://www.windowslive.com/campaign/thenewbusy?ocid=PID28326::T:WLMTAGL:O N:WL:en-US:WM_HMP:042010_2 ________________________________ Message 2 _____________________________________ Time: 06:09:48 AM PST US Subject: RE: TeamGrumman-List: Re: AG5B Jaguar From: "Hosler, John" You guys have any pictures with the Jaguar cowl and MT prop combo? John ________________________________ From: owner-teamgrumman-list-server@matronics.com [mailto:owner-teamgrumman-list-server@matronics.com] On Behalf Of teamgrumman@aol.com Sent: Wednesday, April 28, 2010 2:49 PM Subject: Re: TeamGrumman-List: Re: AG5B Jaguar I guess that IS the question isn't it. Straight and level at 4000 feet, we were truing out at 152 knots. He was running 2700 rpm, I was running 2830. I could climb with him, but just barely. Project X plane is next. I have a torque tube I'm stripping and getting ready for paint. It'll be Red. I've also ordered a windshield for Project X plane. The one that is in it is too bastardized to make fit right. As soon as 119ST is finished, I'll get started on it. -----Original Message----- From: Lawrence Massaro Sent: Wed, Apr 28, 2010 8:46 am Subject: TeamGrumman-List: Re: AG5B Jaguar So I gather from your response, the Project X plane will be using this prop? What were you seeing (numbers please!) on cruise and fuel burn as compared to your AA-5 rocket? Larry Massaro 9186M 1992 AG-5B KRNM From: teamgrumman@AOL.COM Sent: Sat, Apr 24, 2010 8:56 pm Subject: TeamGrumman-List: AG5B Jaguar Ned picked up his plane today. We flew for about 30 minutes side-by-side. The CS MT PRop makes a big difference on cruise and fuel burn. I want one. Gary ator?TeamGrumman-List">http://www.matronics.com/Navigator?TeamGrumman-Li st ttp://forums.matronics.com ibution">http://www.matronics.com/contribution ________________________________ Message 3 _____________________________________ Time: 06:24:39 AM PST US From: "923te" <923te@att.net> Subject: Re: TeamGrumman-List: Re: AG5B Jaguar Yeah, Me too. I could climb with Gary but just barely... That is I had to put the nose way down and climb 20kts faster than best climb rate;) More info (numbers) soon as I finish flight testing. Regards, Ned ________________________________ Message 4 _____________________________________ Time: 03:00:41 PM PST US From: Davesbox1@AOL.COM Subject: TeamGrumman-List: Re: TeamGrumman-List Digest: 5 Msgs - 04/28/10 what's the difference exactly between the MT prop and the sensenich? weight? twist? what's the pitch on this thing anyway...its not constant speed is it? dave N-74356 In a message dated 4/29/2010 2:07:45 A.M. Central Daylight Time, teamgrumman-list@matronics.com writes: * ================================================= Online Versions of Today's List Digest Archive ================================================= Today's complete TeamGrumman-List Digest can also be found in either of the two Web Links listed below. The .html file includes the Digest formatted in HTML for viewing with a web browser and features Hyperlinked Indexes and Message Navigation. The .txt file includes the plain ASCII version of the TeamGrumman-List Digest and can be viewed with a generic text editor such as Notepad or with a web browser. HTML Version: http://www.matronics.com/digest/digestview.php?Style=82701&View=html&Chapter 10-04-28&Archive=TeamGrumman Text Version: http://www.matronics.com/digest/digestview.php?Style=82701&View=txt&Chapter 2010-04-28&Archive=TeamGrumman =============================================== EMail Version of Today's List Digest Archive =============================================== ---------------------------------------------------------- TeamGrumman-List Digest Archive --- Total Messages Posted Wed 04/28/10: 5 ---------------------------------------------------------- Today's Message Index: ---------------------- 1. 08:44 AM - Re: Aileron Trim (Lawrence Massaro) 2. 08:46 AM - Re: AG5B Jaguar (Lawrence Massaro) 3. 03:25 PM - N119ST Jaguar (brian sandberg) 4. 03:45 PM - Re: Re: AG5B Jaguar (teamgrumman@AOL.COM) 5. 04:39 PM - N119ST Jaguar (brian sandberg) ________________________________ Message 1 _____________________________________ Time: 08:44:53 AM PST US From: Lawrence Massaro Subject: TeamGrumman-List: Re: Aileron Trim Thanks to all for the responses. And re: rain, the plane is hangered. The thing that gets me is that I dont recall it ever being a problem until recently (over the last year maybe). I am going to do a few test flights and apply Gary's check and move the flaps small increments to see if that has an effect. Larry Massaro 9186M '92 AG-5B KRNM ________________________________ Message 2 _____________________________________ Time: 08:46:42 AM PST US From: Lawrence Massaro Subject: TeamGrumman-List: Re: AG5B Jaguar So I gather from your response, the Project X plane will be using this prop? What were you seeing (numbers please!) on cruise and fuel burn as compared to your AA-5 rocket? Larry Massaro 9186M 1992 AG-5B KRNM ** From:teamgrumman@AOL.COM Sent: Sat, Apr 24, 2010 8:56 pm Subject: TeamGrumman-List: AG5B Jaguar Ned picked up his plane today. We flew for about 30 minutes side-by-side. The CS MT PRop makes a big difference on cruise and fuel burn. I want one. Gary ** ________________________________ Message 3 _____________________________________ Time: 03:25:03 PM PST US From: brian sandberg Subject: TeamGrumman-List: N119ST Jaguar Sounds great. I'm reading through 7 months worth of teamgrumman digests an d eagerly awaiting my first flight in more than 8 months=2C the longest str etch I've gone since 1998. -Brian Subject: N119ST Jaguar From: teamgrumman@aol.com I've been working on installing the Jaguar cowling on 119ST for a week now. Other than the owner=2C no one else knows that 119ST was the plane I used for all of my original company testing. 119ST has had 6 different prototy pe cowlings=2C 3 different kinds of exit ramps=2C and 2 different versions of air intakes tested on it. I used 119ST for a year way-back-when to test a bunch of ideas. Check out pict 030.jpg. I also had the cowling that is now on N1976T on 119ST about 3 years ago. Maybe it's my familiarity with the plane or maybe that after installing 3 c owlings in as many months=2C but=2C this one is going really smooth. The t rim lines on this cowling are very close to the planes mounting flange. Th is plane has one shim (I got two responses from you guys on shims and dista nces to the spinner=2C thanks) on each of the top mounts and the distance t o the spinner is just a shade under 40 inches. It's got to be differences in bushings and mounts . . . . but=2C I digress. The cowling should be all trimmed up by tomorrow. The missing baffles shou ld be here this week also. Then=2C all the rest of the details. _________________________________________________________________ Hotmail is redefining busy with tools for the New Busy. Get more from your inbox. http://www.windowslive.com/campaign/thenewbusy?ocid=PID28326::T:WLMTAGL:O N:WL:en-US:WM_HMP:042010_2 ________________________________ Message 4 _____________________________________ Time: 03:45:12 PM PST US Subject: Re: TeamGrumman-List: Re: AG5B Jaguar From: teamgrumman@AOL.COM I guess that IS the question isn't it. Straight and level at 4000 feet, we were truing out at 152 knots. He was running 2700 rpm, I was running 2830. I could climb with him, but just barely. Project X plane is next. I have a torque tube I'm stripping and getting ready for paint. It'll be Red. I've also ordered a windshield for Project X plane. The one that is in it is too bastardized to make fit right. As soon as 119ST is finished, I'll get started on it. -----Original Message----- From: Lawrence Massaro Sent: Wed, Apr 28, 2010 8:46 am Subject: TeamGrumman-List: Re: AG5B Jaguar So I gather from your response, the Project X plane will be using this pro p? What were you seeing (numbers please!) on cruise and fuel burn as compared to your AA-5 rocket? Larry Massaro 9186M 1992 AG-5B KRNM From: teamgrumman@AOL.COM Sent: Sat, Apr 24, 2010 8:56 pm Subject: TeamGrumman-List: AG5B Jaguar Ned picked up his plane today. We flew for about 30 minutes side-by -side. The CS MT PRop makes a big difference on cruise and fuel burn. I want one. Gary ======================= ========== ======================= ========== ======================= ========== ======================= ========== ________________________________ Message 5 _____________________________________ Time: 04:39:44 PM PST US From: brian sandberg Subject: TeamGrumman-List: N119ST Jaguar Sounds great. I'm reading through 7 months worth of teamgrumman digests an d eagerly awaiting my first flight in more than 8 months=2C the longest str etch I've gone since 1998. -Brian Subject: N119ST Jaguar From: teamgrumman@aol.com I've been working on installing the Jaguar cowling on 119ST for a week now. Other than the owner=2C no one else knows that 119ST was the plane I used for all of my original company testing. 119ST has had 6 different prototy pe cowlings=2C 3 different kinds of exit ramps=2C and 2 different versions of air intakes tested on it. I used 119ST for a year way-back-when to test a bunch of ideas. Check out pict 030.jpg. I also had the cowling that is now on N1976T on 119ST about 3 years ago. Maybe it's my familiarity with the plane or maybe that after installing 3 c owlings in as many months=2C but=2C this one is going really smooth. The t rim lines on this cowling are very close to the planes mounting flange. Th is plane has one shim (I got two responses from you guys on shims and dista nces to the spinner=2C thanks) on each of the top mounts and the distance t o the spinner is just a shade under 40 inches. It's got to be differences in bushings and mounts . . . . but=2C I digress. The cowling should be all trimmed up by tomorrow. The missing baffles shou ld be here this week also. Then=2C all the rest of the details. _________________________________________________________________ Hotmail is redefining busy with tools for the New Busy. Get more from your inbox. http://www.windowslive.com/campaign/thenewbusy?ocid=PID28326::T:WLMTAGL:O N:WL:en-US:WM_HMP:042010_2 ________________________________ Message 5 _____________________________________ Time: 04:09:15 PM PST US Subject: Re: TeamGrumman-List: Re: AG5B Jaguar From: teamgrumman@AOL.COM -----Original Message----- From: Hosler, John Sent: Wed, Apr 28, 2010 7:03 pm Subject: RE: TeamGrumman-List: Re: AG5B Jaguar You guys have any pictures with the Jaguarcowl and MT prop combo? John From: owner-teamgrumman-list-server@matronics.com[mailto:owner-teamgrumman -list-server@matronics.com] On Behalf Of teamgrumman@aol.com Sent: Wednesday, April 28, 20102:49 PM Subject: Re: TeamGrumman-List: Re:AG5B Jaguar I guess that IS the question isn't it. Straight and level at 4000 feet, we weretruing out at 152 knots. He was running 2700 rpm, I was running 2830. I could climb with him, but just barely. Project X plane is next. I have atorque tube I'm stripping and getting re ady for paint. It'll be Red. I've also ordered a windshield forProject X plane. The one that is in it is too bastardized to make fitright. As soonas 119ST is finished, I'll get started on it. -----OriginalMessage----- From: Lawrence Massaro Sent: Wed, Apr 28, 2010 8:46 am Subject: TeamGrumman-List: Re: AG5B Jaguar So I gather from your response, the Project X plane will be using this pro p? What were you seeing (numbers please!) on cruise and fuel burn as compared to your AA-5 rocket? Larry Massaro 9186M 1992 AG-5B KRNM From: teamgrumman@AOL.COM Sent: Sat, Apr 24, 2010 8:56 pm Subject: TeamGrumman-List: AG5B Jaguar Ned picked up his plane today. We flew for about 30 minutes side-by -side. The CS MT PRop makes a big difference on cruise and fuel burn. I want one. Gary ======================== =========== ator?TeamGrumman-List">http://www.matronics.com/Navigator?TeamGrumman-List ======================== =========== ttp://forums.matronics.com ======================== =========== ibution">http://www.matronics.com/contribution ======================== =========== ======================== =========== ======================== =========== ======================== =========== ======================== =========== ________________________________ Message 6 _____________________________________ Time: 04:48:32 PM PST US From: "Kevin Lancaster" Subject: Re: TeamGrumman-List: Re: AG5B Jaguar I'm eager to see some numbers too! We (True Flight) are set up to distribute and install these and will be offering them on the new Tigers too. As they say the proof is in the puddin' so how's the puddin' Ned? Kevin ----- Original Message ----- From: 923te To: teamgrumman-list@matronics.com Sent: Wednesday, April 28, 2010 7:25 PM Subject: Re: TeamGrumman-List: Re: AG5B Jaguar Yeah, Me too. I could climb with Gary but just barely... That is I had to put the nose way down and climb 20kts faster than best climb rate;) More info (numbers) soon as I finish flight testing. Regards, Ned ________________________________ Message 7 _____________________________________ Time: 06:10:24 PM PST US From: "923te" <923te@att.net> Subject: Re: TeamGrumman-List: Re: TeamGrumman-List Digest: 5 Msgs - 04/28/10 Constant speed it is Pitch is from 11 - 35 deg Scimitar shaped design Weight with spinner 54.7 pounds Difference between MT and other 2 fixed pitch is that it provides more thrust on less fuel. Numbers will come after the turbulance and wind dies down and a good flight test can be conducted. A thorough flight test comparison was done on the earlier MT STC that had the -17 blades and is available here: http://docs.google.com/Doc?docid=0Ad6U0DSgjX1QZGRwd3IybjZfMGhwMnJzbWQ4& hl=enest Regards, All for now..... Well I did fly 1240 miles to return home yesterday from the prop shop in California. I flew at 11,500msl burning 7.9gph. First part of trip here: http://flightaware.com/live/flight/N923TE/history/20100427/2233Z/KPMD/KSJ N/tracklog Your Fellow Grumman Enthusiast, Ned ________________________________ Message 8 _____________________________________ Time: 09:06:17 PM PST US Subject: Re: TeamGrumman-List: Re: TeamGrumman-List Digest: 5 Msgs - 04/28/10 From: teamgrumman@AOL.COM Yes, the MT prop is a constant speed prop. -----Original Message----- From: Davesbox1@AOL.COM Sent: Thu, Apr 29, 2010 6:08 am Subject: TeamGrumman-List: Re: TeamGrumman-List Digest: 5 Msgs - 04/28/10 what's the difference exactly between the MT prop and the sensenich? weig ht? twist? what's the pitch on this thing anyway...its not constant speed is it? dave N-74356 In a message dated 4/29/2010 2:07:45 A.M. Central Daylight Time, teamgrumm an-list@matronics.com writes: * ======================== ======================== = Online Versions of Today's List Digest Archive ======================== ======================== = Today's complete TeamGrumman-List Digest can also be found in either of the two Web Links listed below. The .html file includes the Digest formatte d in HTML for viewing with a web browser and features Hyperlinked Indexes and Message Navigation. The .txt file includes the plain ASCII version of the TeamGrumman-List Digest and can be viewed with a generic text edi tor such as Notepad or with a web browser. HTML Version: http://www.matronics.com/digest/digestview.php?Style=82701&View= html&Chapter 10-04-28&Archive=TeamGrumman Text Version: http://www.matronics.com/digest/digestview.php?Style=82701&View= txt&Chapter 10-04-28&Archive=TeamGrumman ======================== ======================= EMail Version of Today's List Digest Archive ======================== ======================= ---------------------------------------------------------- TeamGrumman-List Digest Archive --- Total Messages Posted Wed 04/28/10: 5 ---------------------------------------------------------- Today's Message Index: ---------------------- 1. 08:44 AM - Re: Aileron Trim (Lawrence Massaro) 2. 08:46 AM - Re: AG5B Jaguar (Lawrence Massaro) 3. 03:25 PM - N119ST Jaguar (brian sandberg) 4. 03:45 PM - Re: Re: AG5B Jaguar (teamgrumman@AOL.COM) 5. 04:39 PM - N119ST Jaguar (brian sandberg) ________________________________ Message 1 ___________________________ __________ Time: 08:44:53 AM PST US From: Lawrence Massaro Subject: TeamGrumman-List: Re: Aileron Trim Thanks to all for the responses. And re: rain, the plane is hangered. The thing that gets me is that I dont recall it ever being a problem until recently (over the last year maybe). I am going to do a few test flights and apply Gary's check and move the flaps small increments to see if that has an effect. Larry Massaro 9186M '92 AG-5B KRNM ________________________________ Message 2 ___________________________ __________ Time: 08:46:42 AM PST US From: Lawrence Massaro Subject: TeamGrumman-List: Re: AG5B Jaguar So I gather from your response, the Project X plane will be using this prop? What were you seeing (numbers please!) on cruise and fuel burn as compar ed to your AA-5 rocket? Larry Massaro 9186M 1992 AG-5B KRNM ** From:teamgrumman@AOL.COM ; Sent: Sat, Apr 24, 2010 8:56 pm Subject: TeamGrumman-List: AG5B Jaguar Ned picked up his plane today. We flew for about 30 minutes si de-by-side. The CS MT PRop makes a big difference on cruise and fuel burn. I want one. Gary ** ________________________________ Message 3 ___________________________ __________ Time: 03:25:03 PM PST US From: brian sandberg Subject: TeamGrumman-List: N119ST Jaguar Sounds great. I'm reading through 7 months worth of teamgrumman digests an d eagerly awaiting my first flight in more than 8 months=2C the longes t str etch I've gone since 1998. -Brian Subject: N119ST Jaguar From: teamgrumman@aol.com I've been working on installing the Jaguar cowling on 119ST for a week now. Other than the owner=2C no one else knows that 119ST was the plane I used for all of my original company testing. 119ST has had 6 different proto ty pe cowlings=2C 3 different kinds of exit ramps=2C and 2 different ve rsions of air intakes tested on it. I used 119ST for a year way-back-when to test a bunch of ideas. Check out pict 030.jpg. I also had the cowling that is now on N1976T on 119ST about 3 years ago. Maybe it's my familiarity with the plane or maybe that after installing 3 c owlings in as many months=2C but=2C this one is going really smooth. The t rim lines on this cowling are very close to the planes mounting flange. Th is plane has one shim (I got two responses from you guys on shims and di sta nces to the spinner=2C thanks) on each of the top mounts and the dista nce t o the spinner is just a shade under 40 inches. It's got to be differenc es in bushings and mounts . . . . but=2C I digress. The cowling should be all trimmed up by tomorrow. The missing baffles shou ld be here this week also. Then=2C all the rest of the details. _________________________________________________________________ Hotmail is redefining busy with tools for the New Busy. Get more from yo ur inbox. http://www.windowslive.com/campaign/thenewbusy?ocid=PID28326::T:WLMTAGL: O N:WL:en-US:WM_HMP:042010_2 ________________________________ Message 4 ___________________________ __________ Time: 03:45:12 PM PST US Subject: Re: TeamGrumman-List: Re: AG5B Jaguar From: teamgrumman@AOL.COM I guess that IS the question isn't it. Straight and level at 4000 feet, we were truing out at 152 knots. He wa s running 2700 rpm, I was running 2830. I could climb with him, but just barely. Project X plane is next. I have a torque tube I'm stripping and getting ready for paint. It'll be Red. I've also ordered a windshield for Project X plane. The one that is in it is too bastardized to make fit right. As soon as 119ST is finished, I'll get started on it. -----Original Message----- From: Lawrence Massaro Sent: Wed, Apr 28, 2010 8:46 am Subject: TeamGrumman-List: Re: AG5B Jaguar So I gather from your response, the Project X plane will be using this pro p? What were you seeing (numbers please!) on cruise and fuel burn as compar ed to your AA-5 rocket? Larry Massaro 9186M 1992 AG-5B KRNM From: teamgrumman@AOL.COM Sent: Sat, Apr 24, 2010 8:56 pm Subject: TeamGrumman-List: AG5B Jaguar Ned picked up his plane today. We flew for about 30 minutes sid e-by -side. The CS MT PRop makes a big difference on cruise and fuel burn. I want one. Gary ======================= ======================= ======================= ======================= ________________________________ Message 5 ___________________________ __________ Time: 04:39:44 PM PST US From: brian sandberg Subject: TeamGrumman-List: N119ST Jaguar Sounds great. I'm reading through 7 months worth of teamgrumman digests an d eagerly awaiting my first flight in more than 8 months=2C the longes t str etch I've gone since 1998. -Brian Subject: N119ST Jaguar From: teamgrumman@aol.com I've been working on installing the Jaguar cowling on 119ST for a week now. Other than the owner=2C no one else knows that 119ST was the plane I used for all of my original company testing. 119ST has had 6 different proto ty pe cowlings=2C 3 different kinds of exit ramps=2C and 2 different ve rsions of air intakes tested on it. I used 119ST for a year way-back-when to test a bunch of ideas. Check out pict 030.jpg. I also had the cowling that is now on N1976T on 119ST about 3 years ago. Maybe it's my familiarity with the plane or maybe that after installing 3 c owlings in as many months=2C but=2C this one is going really smooth. The t rim lines on this cowling are very close to the planes mounting flange. Th is plane has one shim (I got two responses from you guys on shims and di sta nces to the spinner=2C thanks) on each of the top mounts and the dista nce t o the spinner is just a shade under 40 inches. It's got to be differenc es in bushings and mounts . . . . but=2C I digress. The cowling should be all trimmed up by tomorrow. The missing baffles shou ld be here this week also. Then=2C all the rest of the details. _________________________________________________________________ Hotmail is redefining busy with tools for the New Busy. Get more from yo ur inbox. http://www.windowslive.com/campaign/thenewbusy?ocid=PID2===== ======================== ==================== Use utilitie s Day ====================== ======================== == - MATRONICS WEB FORUMS ========== ======================== ============== - List Contribution Web Site sp; =========== ======================== =============== ======================== =========== ======================== =========== ======================== =========== ======================== =========== ________________________________ Message 9 _____________________________________ Time: 09:14:03 PM PST US Subject: Re: TeamGrumman-List: Re: AG5B Jaguar From: teamgrumman@AOL.COM Kevin, For what-it's-worth, Ken Tunnell (LyCon Engine Rebuilders) and I have a 10 :1 fuel injected engine in the works that is rated at 180 hp at 2550 rpm. With the MT prop, it should climb like a homesick angel and get awesome fuel mileage. The MT prop will take advantage of the extra torque and st ill improve cruise speeds. Gary -----Original Message----- From: Kevin Lancaster Sent: Thu, Apr 29, 2010 3:05 pm Subject: Re: TeamGrumman-List: Re: AG5B Jaguar I'm eager to see some numbers too! We (True Flight) are set up to distrib ute and install these and will be offering them on the new Tigers too. As they say the proof is in the puddin' so how's the puddin' Ned? Kevin ----- Original Message ----- From: 923te Sent: Wednesday, April 28, 2010 7:25 PM Subject: Re: TeamGrumman-List: Re: AG5B Jaguar Yeah, Me too. I could climb with Gary but just barely... That is I had to put the nose way down and climb 20kts faster than best climb rate;) More info (numbers) soon as I finish flight testing. Regards, Ned href="http://www.matronics.com/Navigator?TeamGrumman-List">http://www.ma tronics.com/Navigator?TeamGrumman-List href="http://forums.matronics.com">http://forums.matronics.com href="http://www.matronics.com/contribution">http://www.matronics.com/c ======================== =========== ======================== =========== ======================== =========== ======================== =========== ________________________________ Message 10 ____________________________________ Time: 10:01:22 PM PST US From: "Kevin Lancaster" Subject: Re: TeamGrumman-List: Re: AG5B Jaguar Hi Gary, I like fast! Wonder how much power it would make at........say......let's pull a random number out of the air here.........2700 rpm? COOOL! (note the BIG smile) ;-) And while Ned was making great time flying East with fantastic tail winds I flew almost 1400 miles in a 150hp AA1A in the opposite direction into the wind - often at only 80-90 knots. Long trip - still fun! Some guys have all the luck. Kevin ----- Original Message ----- From: teamgrumman@AOL.COM To: teamgrumman-list@matronics.com Sent: Friday, April 30, 2010 12:13 AM Subject: Re: TeamGrumman-List: Re: AG5B Jaguar Kevin, For what-it's-worth, Ken Tunnell (LyCon Engine Rebuilders) and I have a 10:1 fuel injected engine in the works that is rated at 180 hp at 2550 rpm. With the MT prop, it should climb like a homesick angel and get awesome fuel mileage. The MT prop will take advantage of the extra torque and still improve cruise speeds. Gary -----Original Message----- From: Kevin Lancaster To: teamgrumman-list@matronics.com Sent: Thu, Apr 29, 2010 3:05 pm Subject: Re: TeamGrumman-List: Re: AG5B Jaguar I'm eager to see some numbers too! We (True Flight) are set up to distribute and install these and will be offering them on the new Tigers too. As they say the proof is in the puddin' so how's the puddin' Ned? Kevin ----- Original Message ----- From: 923te To: teamgrumman-list@matronics.com Sent: Wednesday, April 28, 2010 7:25 PM Subject: Re: TeamGrumman-List: Re: AG5B Jaguar Yeah, Me too. I could climb with Gary but just barely... That is I had to put the nose way down and climb 20kts faster than best climb rate;) More info (numbers) soon as I finish flight testing. Regards, Ned href="http://www.matronics.com/Navigator?TeamGrumman-List">http://www.m atronics.com/Navigator?TeamGrumman-List href="http://forums.matronics.com">http://forums.matronics.com href="http://www.matronics.com/contribution">http://www.matronics.com/c ator?TeamGrumman-List">http://www.matronics.com/Navigator?TeamGrumman-Lis t ttp://forums.matronics.com ibution">http://www.matronics.com/contribution ------------------------------------------------------------------------------------- Other Matronics Email List Services ------------------------------------------------------------------------------------- Post A New Message teamgrumman-list@matronics.com UN/SUBSCRIBE http://www.matronics.com/subscription List FAQ http://www.matronics.com/FAQ/TeamGrumman-List.htm Web Forum Interface To Lists http://forums.matronics.com Matronics List Wiki http://wiki.matronics.com Full Archive Search Engine http://www.matronics.com/search 7-Day List Browse http://www.matronics.com/browse/teamgrumman-list Browse Digests http://www.matronics.com/digest/teamgrumman-list Browse Other Lists http://www.matronics.com/browse Live Online Chat! http://www.matronics.com/chat Archive Downloading http://www.matronics.com/archives Photo Share http://www.matronics.com/photoshare Other Email Lists http://www.matronics.com/emaillists Contributions http://www.matronics.com/contribution ------------------------------------------------------------------------------------- These Email List Services are sponsored solely by Matronics and through the generous Contributions of its members.