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
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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.
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N:WL:en-US:WM_HMP:042010_2
Message 2
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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 <lmassaro@tac-eng.com>
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
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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
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| Subject: | 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 <lmassaro@tac-eng.com>
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 <lmassaro@tac-eng.com>
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 <mailto: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 <sandbag23@msn.com>
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 <lmassaro@tac-eng.com>
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 <sandbag23@msn.com>
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
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-----Original Message-----
From: Hosler, John <JHOSLER@epri.com>
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 <lmassaro@tac-eng.com>
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
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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
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| Subject: | 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
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| Subject: | Re: TeamGrumman-List Digest: 5 Msgs - 04/28/10 |
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 <lmassaro@tac-eng.com>
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 <lmassaro@tac-eng.com>
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 <mailto: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 <sandbag23@msn.com>
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 <lmassaro@tac-eng.com>
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 <sandbag23@msn.com>
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
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Message 9
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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 <jkevinl@bellsouth.net>
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
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Message 10
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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 <jkevinl@bellsouth.net>
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
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