X-Virus-Scanned: clean according to Sophos on Logan.com From: "Steven W. Boese" Received: from [157.56.111.116] (HELO na01-bn1-obe.outbound.protection.outlook.com) by logan.com (CommuniGate Pro SMTP 6.1.8) with ESMTPS id 8354270 for flyrotary@lancaironline.net; Mon, 25 Jan 2016 12:18:13 -0500 Received-SPF: none receiver=logan.com; client-ip=157.56.111.116; envelope-from=SBoese@uwyo.edu DKIM-Signature: v=1; a=rsa-sha256; c=relaxed/relaxed; d=uwy.onmicrosoft.com; s=selector1-uwyo-edu; h=From:To:Date:Subject:Message-ID:Content-Type:MIME-Version; bh=69f+5d5ni3iVxqagnDyt2qJwqlNKmBJEHFYgq9lP1Cw=; b=g6DWSI8atD79sEbWNC0oUBNKq0tzyKV4Y0p5JVlW8FrnKpvisgRy+6ZKL2gppW9IY+S2Z914AXLmc/P/gBcPcBl7KyZwmxcZ1c6qY2xh1myAw8xq9tWZ8ZTXgmG0Ky5iDwMmJ1s7lhgHOMIgsIHI9zEeC7E+H7bGgNgkxtRyO1g= Received: from BLUPR0501MB2148.namprd05.prod.outlook.com (10.164.23.154) by BLUPR0501MB2147.namprd05.prod.outlook.com (10.164.23.153) with Microsoft SMTP Server (TLS) id 15.1.390.13; Mon, 25 Jan 2016 17:17:53 +0000 Received: from BLUPR0501MB2148.namprd05.prod.outlook.com ([10.164.23.154]) by BLUPR0501MB2148.namprd05.prod.outlook.com ([10.164.23.154]) with mapi id 15.01.0390.013; Mon, 25 Jan 2016 17:17:53 +0000 To: Rotary motors in aircraft Subject: Re: [FlyRotary] Re: parts upgrade; was: What do you think may be happening? Thread-Topic: [FlyRotary] Re: parts upgrade; was: What do you think may be happening? Thread-Index: AQHRV4+iqUiR/WMjdkWCsB4H2ST53J8MeYes Date: Mon, 25 Jan 2016 17:17:53 +0000 Message-ID: <57B092B7-C728-4395-B461-1332FD402004@uwyo.edu> References: In-Reply-To: Accept-Language: en-US Content-Language: en-US X-MS-Has-Attach: yes X-MS-TNEF-Correlator: authentication-results: spf=none (sender IP is ) smtp.mailfrom=SBoese@uwyo.edu; x-originating-ip: [69.146.103.188] x-microsoft-exchange-diagnostics: 1;BLUPR0501MB2147;5:2Ogb4x8Gep7SWg0xqyKSGDF52qOWMoj8/HA7D++otwow3r5MZGOzOJtY9JUBsa0zSSr9mWd8/117ysKaxTd3+6kF12l5i8DpzYl/ycXpP0H8sUjGaW60pInP2LZTfCTq1uB+qt9KCcnVKhMWslDNwA==;24:EnB0TT7LKUKVdlUiDhZgul/dYarlzs+5BnXaZILRLecaxTI7483H8OKrw079SGwKjDM5cPFbhblYhcMy0pI4KwBbQt86a1wD+D+wwTQuCTw= x-microsoft-antispam: UriScan:;BCL:0;PCL:0;RULEID:;SRVR:BLUPR0501MB2147; x-ms-office365-filtering-correlation-id: 796156e9-5e1e-44d9-0d93-08d325ab75cf x-microsoft-antispam-prvs: x-exchange-antispam-report-test: UriScan:; x-exchange-antispam-report-cfa-test: BCL:0;PCL:0;RULEID:(123027)(102615245)(601004)(2401047)(5005006)(520078)(8121501046)(3002001)(10201501046);SRVR:BLUPR0501MB2147;BCL:0;PCL:0;RULEID:;SRVR:BLUPR0501MB2147; x-forefront-prvs: 083289FD26 x-forefront-antispam-report: SFV:NSPM;SFS:(10019020)(279900001)(504954002)(85664002)(479174004)(76104003)(52034003)(24454002)(377454003)(189002)(199003)(3905003)(5001960100002)(54356999)(19625305001)(15975445007)(99936001)(3846002)(2950100001)(77096005)(1096002)(102836003)(110136002)(1220700001)(2900100001)(107886002)(11100500001)(50986999)(105586002)(106356001)(76176999)(5002640100001)(5008740100001)(586003)(106116001)(33656002)(16236675004)(82746002)(6116002)(19617315012)(97736004)(81156007)(89122001)(83716003)(66066001)(99286002)(80792005)(189998001)(19580395003)(101416001)(2906002)(19580405001)(122556002)(87936001)(90282001)(10400500002)(790700001)(36756003)(450100001)(88552002)(5004730100002)(40100003)(86362001)(92566002)(75432002)(5890100001)(15395725005)(3280700002)(104396002);DIR:OUT;SFP:1102;SCL:1;SRVR:BLUPR0501MB2147;H:BLUPR0501MB2148.namprd05.prod.outlook.com;FPR:;SPF:None;PTR:InfoNoRecords;MX:1;A:1;LANG:en; received-spf: None (protection.outlook.com: uwyo.edu does not designate permitted sender hosts) spamdiagnosticoutput: 1:23 spamdiagnosticmetadata: NSPM Content-Type: multipart/related; boundary="_005_57B092B7C7284395B4611332FD402004uwyoedu_"; type="multipart/alternative" MIME-Version: 1.0 X-OriginatorOrg: uwyo.edu X-MS-Exchange-CrossTenant-originalarrivaltime: 25 Jan 2016 17:17:53.4104 (UTC) X-MS-Exchange-CrossTenant-fromentityheader: Hosted X-MS-Exchange-CrossTenant-id: f9cdd7ad-825d-4601-8e9c-a325e02d52da X-MS-Exchange-Transport-CrossTenantHeadersStamped: BLUPR0501MB2147 --_005_57B092B7C7284395B4611332FD402004uwyoedu_ Content-Type: multipart/alternative; boundary="_000_57B092B7C7284395B4611332FD402004uwyoedu_" --_000_57B092B7C7284395B4611332FD402004uwyoedu_ Content-Type: text/plain; charset="Windows-1252" Content-Transfer-Encoding: quoted-printable Bill, If turning both disables on removes power to all the injectors as intended,= then the engine should quit no matter what the controller tries to do or w= hat position the cold switch is in. With a fixed pitch prop, SAG is similar to throttling back significantly. = It's probably somewhat different with a constant speed prop. If SAG is all= owed to persist, the EGT's will decrease and the temperatures of the oil an= d coolant will increase. Steve Boese On Jan 25, 2016, at 9:44 AM, Bill Bradburry > wrote: Jeff, With the engine at idle, mixture at 14.7, disabling the secondary brings th= e mixture to about 13.0. If I turn both disables on, and then turn cold st= art on, the mixture goes really rich around 10. In your third line scenario: At 1400 rpm with both INJ ON and CS OFF, disabling the PRI should cause the= engine to quit =96 if you quickly set the CS to ON the engine should recov= er using the SEC injectors. This assumes that the cold start switch will turn both injectors on even th= ough the EC-2 is staging. My EC-2 does not seem to be doing that at this t= ime. I suppose there is something in the system that is broken. I think t= his has been going on for quite some time and hasn=92t been much of a probl= em unless I find myself in need of shutting down the primary. Currently in= order to do that, I would have to land with the engine at at least 20 inch= es=85.or dead stick it in. Which is something that Ed Anderson would not t= hink a problem at all! :>) By the way, I am ordering the BR10EIX plugs. I think I may be experiencing= SAG. Can someone give me a pretty good description of what that feels lik= e?? Bill ________________________________ From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] Sent: Monday, January 25, 2016 10:21 AM To: Rotary motors in aircraft Subject: [FlyRotary] Re: parts upgrade; was: What do you think may be happe= ning? Bill, something you may want to try (if only temporary) is to separate the = Cold Start function from the Injector Disable functions; I believe this mak= es it is easier to tell what is going on. Wire the Cold Start switch independently to pin 30. Use one toggle switch to power the PRI and another to power the SEC injecto= rs. At 1400 rpm with both INJ ON and CS OFF, disabling the SEC injectors should= do nothing. At 1400 rpm with both INJ ON and CS ON, the engine will run very rough due = to fuel-doubling to PRI injectors =96 this is a handy feature for true COLD= starting. At 1400 rpm with both INJ ON and CS OFF, disabling the PRI should cause the= engine to quit =96 if you quickly set the CS to ON the engine should recov= er using the SEC injectors. At >4000 rpm and above staging: disabling either INJ should cause the engin= e to stumble =96 if you now set the CS to ON the engine should recover usin= g the other injectors. My engine is wired this way permanently =85 Jeff From: Bill Bradburry > Subject: RE: [FlyRotary] Re: parts upgrade; was: What do you think may be happening? Date: Mon, 25 Jan 2016 08:44:19 -0600 To: 'Rotary motors in aircraft' > Steve and Tracy, The injectors are all four the yellow injectors, 450 CC, I think. The EC-2= was in Mode 0 when I tested it yesterday. No, unfortunately, I have not gotten the signal recording setup going. Good Luck with the slicing and dicing, Tracy. Is this a second hip or a re= do of the first? Bill On 1/20/2016 12:55 PM, Tracy Crook wrote: Steve=92s description of how the EC2/3 works was correct. Many get this bit confused but The intention with the disable switch was t= o use a DPDT switch for the disables. When in the disable position, the o= ther pole of the switch is used to activate (switch to ground) the Cold Sta= rt input to the EC2/3 at the same time. This eliminates having to turn off= the CS switch when disabling a set of injectors and enables the EC2 to ope= rate on either set over the full range of manifold pressures. The EC2/3 is= able to see when you have disabled the primaries and operate the secondary= =92s even though engine is operating below stage point. I=92ve been out of touch lately and will be for awhile. Need to have my hi= p replaced (again). Tracy Sent from Mail for Windows= 10 From: Bill Bradburry Sent: Wednesday, January 20, 2016 1:44 PM To: Rotary motors in aircraft Subject: [FlyRotary] Re: What do you think may be happening? Steve, I think my engine dies and has little effect when I turn off the primary an= d secondary respectively. I will have to investigate this when I get the s= witches replaced (I plan to replace both) I may have something miswired?? It is cold, maybe Tracy is back in Florida and will chime in. Bill From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] Sent: Wednesday, January 20, 2016 12:32 PM To: Rotary motors in aircraft Subject: [FlyRotary] Re: What do you think may be happening? Bill, I have tested the injector disable function with my EC2's. With the power = interrupted to the primary injectors and the cold switch on, the engine run= s on the secondary injectors at MAP below the staging threshold. I don't k= now the details of how the controller treats the cold switch, but it is pos= sible that with the cold switch on, the controller increases the fuel flow = by using both the primary and secondary injectors at MAP below the staging = threshold, and doubles the injector pulse width at MAP above the staging th= reshold. I remember investigating this when first using the controllers bu= t don't remember the exact details. My backup system does work at low MAP. Steve From: Rotary motors in aircraft on behalf of Bill Bradburry Sent: Wednesday, January 20, 2016 11:15 AM To: Rotary motors in aircraft Subject: [FlyRotary] Re: What do you think may be happening? Bobby, I am sorry I was not clear and the reason was that I was not clear myself. The injector disable switches are for in case you lose an injector in fligh= t and the engine starts to run on only one rotor. You can disable either o= f the primary or secondary injectors which will take the failed injector ou= t of the circuit. Tracy says you should test this to make sure that it works. That is where = my question came from. You can only test the disable switches when the eng= ine is not staged. If the engine is staged, and you turn off the primary i= njectors, the engine will die because the secondary injectors are not runni= ng, and if you turn off the secondary injectors, the engine will run rich b= ecause you turned on the cold start but the secondaries were not running an= yway. I am not sure what would happen if you lost a primary injector in flight, d= isabled the primary injectors, then reduced power to the staging point in o= rder to land??? I suspect all would get quiet! :>( Bill From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] Sent: Wednesday, January 20, 2016 11:35 AM To: Rotary motors in aircraft Subject: [FlyRotary] Re: What do you think may be happening? Bill, I=92m not sure I understand the question. If your referring to my =93cente= r off switch position=94 it=92s not used in flight. Intentionally anyway :)= It=92s used to shut down the engine. Primary injector switch of course. Sa= me switch used for both primary and secondary injectors. Bobby From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] Sent: Wednesday, January 20, 2016 10:55 AM To: Rotary motors in aircraft Subject: [FlyRotary] Re: What do you think may be happening? Changing the subject a minute=85How do you disable the secondary=92s when t= he engine is staged?? They are not running anyway??? Bill -- Homepage: http://www.flyrotary.com/ Archive and UnSub: http://mail.lancaironline.net:81/lists/flyrotary/List.= html This message, and the documents attached hereto, is intended only for the a= ddressee and may contain privileged or confidential information. Any unauth= orized disclosure is strictly prohibited. If you have received this message= in error, please notify us immediately so that we may correct our internal= records. Please then delete the original message. Thank you. --_000_57B092B7C7284395B4611332FD402004uwyoedu_ Content-Type: text/html; charset="Windows-1252" Content-Transfer-Encoding: quoted-printable
Bill,
If turning both disables on removes power to= all the injectors as intended, then the engine should quit no matter what = the controller tries to do or what position the cold switch is in.

With a fixed pitch prop, SAG is similar to t= hrottling back significantly.  It's probably somewhat different with a= constant speed prop.  If SAG is allowed to persist, the EGT's will de= crease and the temperatures of the oil and coolant will increase.

Steve Boese

On Jan 25, 2016, at 9:44 AM, Bill Bradburry <flyrotary@lancaironline.net> wrote:

Jeff,

 

With the engine at idle, mixture at 14= .7, disabling the secondary brings the mixture to about 13.0.  If I tu= rn both disables on, and then turn cold start on, the mixture goes really rich around 10.

 

In your third line scenario:

= At 1400 rpm with both INJ ON= and CS OFF, disabling the PRI should cause the engine to quit =96 if you q= uickly set the CS to ON the engine should recover using the SEC injectors.

=  

This assumes that the cold start switc= h will turn both injectors on even though the EC-2 is staging.  My EC-= 2 does not seem to be doing that at this time.  I suppose there is something in the system that i= s broken.  I think this has been going on for quite some time and hasn= =92t been much of a problem unless I find myself in need of shutting down t= he primary.  Currently in order to do that, I would have to land with the engine at at least 20 inches=85.or dead stic= k it in.  Which is something that Ed Anderson would not think a proble= m at all!   :>)

 

By the way, I am ordering the BR10EIX = plugs.  I think I may be experiencing SAG.  Can someone give me a= pretty good description of what that feels like??

 

Bill

 


= From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.= net]
Sent: Monday, January 25, 20= 16 10:21 AM
To: Rotary motors in aircraft
Subject: [FlyRotary] Re: par= ts upgrade; was: What do you think may be happening?

 

= Bill, something you may want= to try (if only temporary) is to separate the Cold Start function from the= Injector Disable functions; I believe this makes it is easier to tell what is going on.

= Wire the Cold Start switch i= ndependently to pin 30.

= Use one toggle switch to pow= er the PRI and another to power the SEC injectors.=

= At 1400 rpm with both INJ ON= and CS OFF, disabling the SEC injectors should do nothing.

= At 1400 rpm with both INJ ON= and CS ON, the engine will run very rough due to f= uel-doubling to PRI injectors =96 this is a handy feature for true COLD sta= rting.

= At 1400 rpm with both INJ ON= and CS OFF, disabling the PRI should cause the engine to quit =96 if you q= uickly set the CS to ON the engine should recover using the SEC injectors.

=  

= At >4000 rpm and above st= aging: disabling either INJ should cause the engine to stumble =96 if you n= ow set the CS to ON the engine should recover using the other injectors.

=  

= My engine is wired this way = permanently =85

= Jeff

=  

From:

Bill Bradburry <flyrotary@lancaironline.net>

Subject:

RE: [FlyRotary] Re: parts upgrade; was: What do you th= ink may be happening?

Date:

Mon, 25 Jan 2016 08:44:19 -0600

To:

'Rotary motors in aircraft= ' <flyro= tary@lancaironline.net>

&l= t;image001.gif>

&l= t;image002.gif>

Steve and Tracy,

 

The injectors are all four the yellow injectors, 450 CC, I th= ink.  The EC-2 was in Mode 0 when I tested it yesterday.

No, unfortunately, I have not gotten the signal recording set= up going.

 

Good Luck with the slicing and dicing, Tracy.&= nbsp; Is this a second hip or a redo of the first?<= /span>

 

Bill

=  


On 1/20/2016 12:55 PM, Tracy Crook wrote:

Steve=92s description of how the EC2/3 works= was correct.

 

Many get this bit confused but The intention= with  the disable switch was to use a DPDT switch for the disables.&n= bsp;  When in the disable position, the other pole of the switch is used to activate (switch to ground) the Cold Start input to = the EC2/3 at the same time.  This eliminates having to turn off the CS= switch when disabling a set of injectors and enables the EC2 to operate on= either set over the full range of manifold pressures.  The EC2/3 is able to see when you have disabled the prima= ries and operate the secondary=92s  even though engine is operating be= low stage point.

 

I=92ve been out of touch lately and will be = for awhile.  Need to have my hip replaced (again).

 

Tracy

 

Sent from Mail for Wi= ndows 10

 


From: Bill Bradburry
Sent: Wednesday, January 20,= 2016 1:44 PM
To: Rotary motors in aircraft
Subject: [FlyRotary] Re: Wha= t do you think may be happening?

 

Steve,

I think my engine dies and has little = effect when I turn off the primary and secondary respectively.  I will= have to investigate this when I get the switches replaced (I plan to replace both)  I may have= something miswired??

It is cold, maybe Tracy is back in Florida and will chime in.

 

Bill

 

 

= From:<= /span> Rotary motors in aircraft [mailto:flyrotary@lancaironline.= net]
Sent: Wednesday, January 20,= 2016 12:32 PM
To: Rotary motors in aircraft
Subject: [FlyRotary] Re: Wha= t do you think may be happening?

 

Bill,

 

I have tested the= injector disable function with my EC2's.  With the power interrupted = to the primary injectors and the cold switch on, the engine runs on the secondary injectors at MAP below the staging thresh= old.  I don't know the details of how the controller treats the cold s= witch, but it is possible that with the cold switch on, the controller incr= eases the fuel flow by using both the primary and secondary injectors at MAP below the staging threshold, and do= ubles the injector pulse width at MAP above the staging threshold.  I = remember investigating this when first using the controllers but don't reme= mber the exact details.  My backup system does work at low MAP.

 

Steve

 

 

From: Rotary motors in aircraft <flyrotary@lancaironline.net> on behalf of Bill Bradburry <flyrotary@lancaironline.net>
Sent: Wednesday, January 20,= 2016 11:15 AM
To: Rotary motors in aircraft
Subject: [FlyRotary] Re: Wha= t do you think may be happening?

 

Bobby,

I am sorry = I was not clear and the reason was that I was not clear myself.

 

The injecto= r disable switches are for in case you lose an injector in flight and the e= ngine starts to run on only one rotor.  You can disable either of the primary or secondary injectors which will take t= he failed injector out of the circuit.

= Tracy says you should test this to make sure that it works.  That is where = my question came from.  You can only test the disable switches when th= e engine is not staged.  If the engine is staged, and you turn off the= primary injectors, the engine will die because the secondary injectors are not running, and if you turn off the secondary= injectors, the engine will run rich because you turned on the cold start b= ut the secondaries were not running anyway.

 

I am not su= re what would happen if you lost a primary injector in flight, disabled the= primary injectors, then reduced power to the staging point in order to land???  I suspect all would get quiet!=   :>(

 

Bill

 

 

From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.= net]
Sent: Wednesday, January 20,= 2016 11:35 AM
To: Rotary motors in aircraft
Subject: [FlyRotary] Re: Wha= t do you think may be happening?

 

B= ill,

&= nbsp;

I= =92m not sure I understand the question.  If your referring to my =93c= enter off switch position=94 it=92s not used in flight. Intentionally anyway J It=92s used to shut down the engine. Primary injector switch of course. Sa= me switch used for both primary and secondary injectors.

&= nbsp;

B= obby

&= nbsp;

From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.= net]
Sent: Wednesday, January 20,= 2016 10:55 AM
To: Rotary motors in aircraft
Subject: [FlyRotary] Re: Wha= t do you think may be happening?

 

 = ;

&= nbsp;

Changing th= e subject a minute=85How do you disable the secondary=92s when the engine i= s staged??  They are not running anyway???

 

Bill

 

 



--
Homepage:  http=
://www.flyrotary.com/
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