X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from [64.129.170.194] (HELO VIRCOM1.fcdata.private) by logan.com (CommuniGate Pro SMTP 5.4.1) with ESMTP id 5091231 for flyrotary@lancaironline.net; Sat, 13 Aug 2011 19:30:51 -0400 Received-SPF: none receiver=logan.com; client-ip=64.129.170.194; envelope-from=cbarber@texasattorney.net Received: from FCD-MAIL06.FCDATA.PRIVATE ([fe80::697f:d6aa:b87:78d8]) by FCD-MAIL05.FCDATA.PRIVATE ([fe80::809d:a06e:5913:452e%13]) with mapi id 14.01.0289.001; Sat, 13 Aug 2011 18:29:18 -0500 From: Chris Barber To: Rotary motors in aircraft Subject: Re: [FlyRotary] Re: Rotary Roster Spreadsheet Updated Thread-Topic: [FlyRotary] Re: Rotary Roster Spreadsheet Updated Thread-Index: AQHMWf1t5LcHlv3B2EqEZ4/B77LsC5UbbexU Date: Sat, 13 Aug 2011 23:29:41 +0000 Message-ID: <5607E604-3B7C-42D1-B95F-45EAD19D45B2@texasattorney.net> References: In-Reply-To: Accept-Language: en-US Content-Language: en-US X-MS-Has-Attach: X-MS-TNEF-Correlator: Content-Type: multipart/alternative; boundary="_000_5607E6043B7C42D1B95F45EAD19D45B2texasattorneynet_" MIME-Version: 1.0 --_000_5607E6043B7C42D1B95F45EAD19D45B2texasattorneynet_ Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: quoted-printable Chris Barber - Velocity SE N17010 (pusher) - 2nd gen 13b turbo block w/ medium street port (by Mazdatrix) - Mistral intake - "Comp" T-4 turbo w/ "Performance" 46mm wastegate. - EM2 by RWS - EC2 by RWS - RD-B by RWS - A/C by Seamech Enviromental - Dynon Skyview EFIS - duel battery/alternator per AeroElectric Z-14 drawing - Conversion Concepts engine mount - IVO 3 blade in flight adjustable prop (45" - 105" pitch range/ 68" prop) Sent from my iPhone 4 On Aug 13, 2011, at 4:10 PM, "Mark Steitle" > wrote: OK, thanks for the updates. Anyone else have any updates/corrections, plea= se let me know. Mark On Tue, Aug 9, 2011 at 8:23 PM, Steven W. Boese <SB= oese@uwyo.edu> wrote: Mark: Please include any of the additions/corrections you think are appropriate. Steve (last name spelled) Boese Prop: Warp drive 3 blade 68 x 17* Ignition: LS1 coils Modifications: dual alternators, Floscan and pulse width based (with injec= tor dead time correction) fuel flow indicators and totalizers. Engine and = flight parameter data logging. Injector dead time correction added to EC2= controller A. Retained oil metering system but with separate oil supply = and steel lines. 0.020" dia fuel bypass. Fuel pressure regulator with ret= urn co-located with fuel pumps allowing single fuel line to fuel rails. Significant events: SAG and abnormally short spark plug life probably due = to over-advanced ignition timing. RD1A prop shaft developed end play requi= ring shim installation and replacement of ball bearing and seal, partially = attributed to Performance Propeller tip flutter. --_000_5607E6043B7C42D1B95F45EAD19D45B2texasattorneynet_ Content-Type: text/html; charset="us-ascii" Content-Transfer-Encoding: quoted-printable

Chris Barber

- Velocity SE N17010 (pusher)

- 2nd gen 13b turbo block w/ medium street port (by Mazdatrix)

- Mistral intake

- "Comp" T-4 turbo w/ "Performance" 46mm wastegate.

- EM2 by RWS

- EC2 by RWS

- RD-B by RWS

- A/C by Seamech Enviromental
- Dynon Skyview EFIS

- duel battery/alternator per AeroElectric Z-14 drawing

- Conversion Concepts engine mount

- IVO 3 blade in flight adjustable prop (45" - 105" pitch ra= nge/ 68" prop)

Sent from my iPhone 4

On Aug 13, 2011, at 4:10 PM, "Mark Steitle" <msteitle@gmail.com> wrote:

OK, thanks for the updates. Anyone else have any updates/correct= ions, please let me know.

Mark

On Tue, Aug 9, 2011 at 8:23 PM, Steven W. Boese = <SBoese@uwyo.edu> wrote:

Mark:

Please include any of the addi= tions/corrections you think are appropriate.

Steve (last name spelled) Boes= e

Prop: Warp drive 3 blade 68 x = 17*

Ignition: LS1 coils

Modifications: dual alte= rnators, Floscan and pulse width based (with injector dead time correction)= fuel flow indicators and totalizers. Engine and flight paramete= r data logging. Injector dead time correction added to EC2 controller A. Retained oil metering system but wit= h separate oil supply and steel lines. 0.020" dia fuel bypass.&n= bsp; Fuel pressure regulator with return co-located with fuel pum= ps allowing single fuel line to fuel rails.
Significant events: SAG = and abnormally short spark plug life probably due to over-advanced ignition= timing. RD1A prop shaft developed end play requiring shim installati= on and replacement of ball bearing and seal, partially attributed to Performance Propeller tip flutter. <= br>

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