TeamGrumman-List Digest Archive

Sat 10/23/10


Total Messages Posted: 8



Today's Message Index:
----------------------
 
     1. 07:03 AM - Re: Re: IO-360 B1E (180 hp) (flyv35b)
     2. 07:04 AM - Re: Project X plane (flyv35b)
     3. 07:28 AM - Re: Project X plane (lmassaro)
     4. 11:25 AM - Re: Re: IO-360 B1E (180 hp) (Gary Vogt)
     5. 11:26 AM - Re: Project X plane (Gary Vogt)
     6. 11:32 AM - Re: Re: Project X plane (Gary Vogt)
     7. 01:03 PM - Re: Pro-seal (cwleach)
     8. 01:07 PM - Re: lost key (cwleach)
 
 
 


Message 1


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    Time: 07:03:02 AM PST US
    From: "flyv35b" <flyv35b@minetfiber.com>
    Subject: Re: IO-360 B1E (180 hp)
    Are you sure it was only 100LL? They sell 130 octane at Reno. ----- Original Message ----- From: Gary Vogt To: teamgrumman-list@matronics.com Sent: Friday, October 22, 2010 6:07 PM Subject: Re: TeamGrumman-List: Re: IO-360 B1E (180 hp) The angle valve engine is actually more prone to detonation due to the large valve pockets cut into the piston crown. Parallel valve engines with 14.7:1 have been run at Reno on 100LL. ------------------------------------------------------------------------- ----- From: flyv35b <flyv35b@minetfiber.com> To: teamgrumman-list@matronics.com Sent: Fri, October 22, 2010 1:40:16 PM Subject: Re: TeamGrumman-List: Re: IO-360 B1E (180 hp) <flyv35b@minetfiber.com> Ned, I didn't know that. Any restrictions on that STC? I think I recall reading that the angle valve engine might be slightly less prone to detonation because of the combustion chamber shaft. But it's probably not more than 0.2 CR difference. Heck, I'm going to be running about 9.7 CR on my 356 Porsche on 92 octane auto gas. Cliff ----- Original Message ----- From: "discover" <923te@att.net> To: <teamgrumman-list@matronics.com> Sent: Friday, October 22, 2010 12:07 PM Subject: TeamGrumman-List: Re: IO-360 B1E (180 hp) > > Hey Cliff, > > Are you aware of Firewall Forwards STC's for 10:1 pistons for Mooneys and Cessna Cardinals? Yes, they had to demonstrate he detonation margins to get the STC approved. And it is the angle valve engine.. > > Ned > > I don't know if the FAA will issue a multiple STC for an engine with 10:1 CR without a lot of "detonation margin" testing. You obviously have a fair amount of experience with 10:1 CR with apparently no problems with 100LL fuel at least and that will not only increase HP and BSFC and be especially beneficial at high altitude where the engine would not be derated by limiting MP. A 9.0:1 CR might be much easier to get approved. The only real practical solution to the replacement of 100LL will be with


    Message 2


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    Time: 07:04:08 AM PST US
    From: "flyv35b" <flyv35b@minetfiber.com>
    Subject: Re: Project X plane
    Are the side air ducts made out of aluminum? Or fiberglass? ----- Original Message ----- From: Gary Vogt To: Teamgrumman List Sent: Friday, October 22, 2010 6:36 PM Subject: TeamGrumman-List: Project X plane Here are some pics of the plane's interior. It's all back together now. Without a side-by-side comparison it's hard to comprehend the difference. I used a handheld florescent drop cord for the lighting. The colors are off a bit. I capped off the rear seat heat and installed the plastic console panels. Gained 2 inched of foot room on each side; saved about 8 lbs in weight. Plus, they are easy to remove for maintenance. I wish the trim wheel and flap switch were in their correct places. I'd put in a cup holder. The modified cowling (with a new inlet design and K&N air filter from a Tiger) is nearing it's final fabrication steps. Initially Dave thought it would take a week. Two weeks later he's still making parts/molds/tooling. He promises me it will be soon. I can't wait to fly it. Gary


    Message 3


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    Time: 07:28:39 AM PST US
    Subject: Re: Project X plane
    From: "lmassaro" <lmassaro@tac-eng.com>
    Nice pics... Plane is looking real good. Cant wait to see the new cowling... Read this topic online here: http://forums.matronics.com/viewtopic.php?p=316757#316757


    Message 4


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    Time: 11:25:48 AM PST US
    From: Gary Vogt <teamgrumman@YAHOO.COM>
    Subject: Re: IO-360 B1E (180 hp)
    that's what Ken Tunnell told me. ________________________________ From: flyv35b <flyv35b@minetfiber.com> Sent: Sat, October 23, 2010 7:00:25 AM Subject: Re: TeamGrumman-List: Re: IO-360 B1E (180 hp) Are you sure it was only 100LL? They sell 130 octane at Reno. ----- Original Message ----- >From: Gary Vogt >To: teamgrumman-list@matronics.com >Sent: Friday, October 22, 2010 6:07 PM >Subject: Re: TeamGrumman-List: Re: IO-360 B1E (180 hp) > > >The angle valve engine is actually more prone to detonation due to the large >valve pockets cut into the piston crown. Parallel valve engines with 14.7:1 >have been run at Reno on 100LL. > > ________________________________ From: flyv35b <flyv35b@minetfiber.com> >To: teamgrumman-list@matronics.com >Sent: Fri, October 22, 2010 1:40:16 PM >Subject: Re: TeamGrumman-List: Re: IO-360 B1E (180 hp) > >--> TeamGrumman-List message posted by: "flyv35b" <flyv35b@minetfiber.com> > >Ned, > >I didn't know that. Any restrictions on that STC? I think I recall >reading that the angle valve engine might be slightly less prone to detonation >because of the combustion chamber shaft. But it's probably not more than 0.2 >CR difference. > >Heck, I'm going to be running about 9.7 CR on my 356 Porsche on 92 octane >auto gas. > >Cliff >----- Original Message ----- From: "discover" <923te@att.net> >To: <teamgrumman-list@matronics.com> >Sent: Friday, October 22, 2010 12:07 PM >Subject: TeamGrumman-List: Re: IO-360 B1E (180 hp) > > >> >> Hey Cliff, >> >> Are you aware of Firewall Forwards STC's for 10:1 pistons for Mooneys and >>Cessna Cardinals? Yes, they had to demonstrate he detonation margins to get >>the STC approved. And it is the angle valve engine.. >> >> Ned >> >> I don't know if the FAA will issue a multiple STC for an engine with 10:1 >>CR without a lot of "detonation margin" testing. You obviously have a fair >>amount of experience with 10:1 CR with apparently no problems with 100LL >>fuel at least and that will not only increase HP and BSFC and be especially >>beneficial at high altitude where the engine would not be derated by >>limiting MP. A 9.0:1 CR might be much easier to get approved. The only >>real practical solution to the replacement of 100LL will be with >> > > >href="http://www.matronics.com/Navigator?TeamGrumman-List">http://www.matronics.com/Navigator?TeamGrumman-Listhref="http://forums.matronics.com">http://forums.matronics.com > href="http://www.matronics.com/contribution">http://www.matronics.com/c >


    Message 5


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    Time: 11:26:44 AM PST US
    From: Gary Vogt <teamgrumman@YAHOO.COM>
    Subject: Re: Project X plane
    not sure what you're talking about. ________________________________ From: flyv35b <flyv35b@minetfiber.com> Sent: Sat, October 23, 2010 7:01:58 AM Subject: Re: TeamGrumman-List: Project X plane Are the side air ducts made out of aluminum? Or fiberglass? ----- Original Message ----- >From: Gary Vogt >To: Teamgrumman List >Sent: Friday, October 22, 2010 6:36 PM >Subject: TeamGrumman-List: Project X plane > > >Here are some pics of the plane's interior. It's all back together now. > Without a side-by-side comparison it's hard to comprehend the difference. I >used a handheld florescent drop cord for the lighting. The colors are off a >bit. > > >I capped off the rear seat heat and installed the plastic console panels. > Gained 2 inched of foot room on each side; saved about 8 lbs in weight. > Plus, they are easy to remove for maintenance. > > >I wish the trim wheel and flap switch were in their correct places. I'd put >in a cup holder. > > >The modified cowling (with a new inlet design and K&N air filter from a >Tiger) is nearing it's final fabrication steps. Initially Dave thought it >would take a week. Two weeks later he's still making parts/molds/tooling. > He promises me it will be soon. I can't wait to fly it. > > >Gary >


    Message 6


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    Time: 11:32:40 AM PST US
    From: Gary Vogt <teamgrumman@YAHOO.COM>
    Subject: Re: Project X plane
    I can't wait to fly it. Dave closed out the opening on the bottom of the cowling where the old inlet was. The housing for the air filter is the last to be finished. I will send pics when I get some. ________________________________ From: lmassaro <lmassaro@tac-eng.com> Sent: Sat, October 23, 2010 7:26:26 AM Subject: TeamGrumman-List: Re: Project X plane Nice pics... Plane is looking real good. Cant wait to see the new cowling... Read this topic online here: http://forums.matronics.com/viewtopic.php?p=316757#316757


    Message 7


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    Time: 01:03:33 PM PST US
    Subject: Re: Pro-seal
    From: "cwleach" <cwleach@earthlink.net>
    I think your gutter will work fine as long as it only rains 100LL! Read this topic online here: http://forums.matronics.com/viewtopic.php?p=316782#316782


    Message 8


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    Time: 01:07:18 PM PST US
    Subject: Re: lost key
    From: "cwleach" <cwleach@earthlink.net>
    teamgrumman(at)YAHOO.COM wrote: "I had a key made from the baggage door lock. After I put the baggage door back together, I tried the canopy; it worked. Then I tried the ignition. Wouldn't ya know. It worked too. There isn't a lot of good things I can say about the AG5B. However, using the same key for all three locks was an awesome idea." Don't let the TSA know that the same key works all three places. Their recent "security" practices suggest* different keys for doors and ignition. *suggest = we recommend it only until we're able to mandate it! Read this topic online here: http://forums.matronics.com/viewtopic.php?p=316784#316784




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