X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from mail.fdic.gov ([167.176.6.5] verified) by logan.com (CommuniGate Pro SMTP 5.1c.2) with ESMTPS id 1226477 for flyrotary@lancaironline.net; Thu, 06 Jul 2006 16:53:59 -0400 Received-SPF: pass receiver=logan.com; client-ip=167.176.6.5; envelope-from=brogers@fdic.gov DKIM-Signature: a=rsa-sha1; d=fdic.gov; s=fdic; c=simple; q=dns; t=1152219184; x=1152305584; h=from:date:subject:message-id:content-class:content-type; b=mbYh1ECxo9ngxGpEb+6sl2Pk6j0xU4OK4jBnU7ZBOn9TPBOXYREaKgSNR3h4IEjLFy7Tvcm1RQxtK7fMxtJNMg== Content-class: urn:content-classes:message MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="----_=_NextPart_001_01C6A13E.20B72424" X-MimeOLE: Produced By Microsoft Exchange V6.5.7226.0 Subject: RE: [FlyRotary] Re: Rotary configuration list. Date: Thu, 6 Jul 2006 15:52:43 -0500 Message-ID: <15839C662A43B844B6E393DBFEAA90BF0494DC5B@dalexc101p.prod.fdic.gov> X-MS-Has-Attach: X-MS-TNEF-Correlator: Thread-Topic: [FlyRotary] Re: Rotary configuration list. Thread-Index: AcaeW+qB0LuuNrbGSuiCZ+l9jaoa5QC3JIOg From: "Rogers, Bob J." To: "Rotary motors in aircraft" Return-Path: BRogers@FDIC.gov X-OriginalArrivalTime: 06 Jul 2006 20:52:44.0029 (UTC) FILETIME=[20FF62D0:01C6A13E] This is a multi-part message in MIME format. ------_=_NextPart_001_01C6A13E.20B72424 Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: quoted-printable Here is my input. =20 ________________________________ From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of Dale Rogers Sent: Sunday, July 02, 2006 11:46 PM To: Rotary motors in aircraft Subject: [FlyRotary] Re: Rotary configuration list. =20 Hi All, Well, already I've had to change the form. One line=20 item added ("Fuel Control"). Tail Number: N62BT Builder: Bob J. Rogers, Plano, TX Engine/Model/Year: 1987 13B Turbo Source/Condition: Rebuilt by Bob J. Rogers from used (100K miles) Mazda RX-7 Modifications: New rotor housings, 1 new end housing, new seals and bearings. Intake: Custom short intake with Turbonetics 60-1 Turbo & stock intercooler Exhaust: Custom Exhaust headers for Turbo (3" down pipe, no muffler). PSRU/Re-Drive: RWS RD-1B 2.175/1=20 Engine Control: RWS EC-2 EFI & Ignition Controller =20 Fuel control: Fuel Injected with four 550 cc injectors on TWM Throttle Body=20 Fuel pumps: Dual EFI fuel pumps from RWS Prop: Prince P-tip composite fixed-pitch 68x84 Cooling System: Summit Race Radiator, approx dimensions 27x19x3 Oil System: Stock Mazda Oil Cooler, aftermarket ADC Oil filter system =20 Installation: Conventional =20 Power: Estimated 200 hp - turbo normalized up to 17,000 feet First Flown: Expected yr 2007 Total Time: 10 hours ground run (not yet flying) Platform: Bushby Mustang II kitplane Best regards, Dale R. -- Homepage: http://www.flyrotary.com/ Archive and UnSub: http://mail.lancaironline.net/lists/flyrotary/ ------_=_NextPart_001_01C6A13E.20B72424 Content-Type: text/html; charset="us-ascii" Content-Transfer-Encoding: quoted-printable

Here is my input.

From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of Dale Rogers
Sent: Sunday, July 02, = 2006 11:46 PM
To: Rotary motors in = aircraft
Subject: [FlyRotary] Re: = Rotary configuration list.

Hi All,

Well, already I've had to = change the form. One line
item added ("Fuel = Control").

Tail = Number: = N62BT

&nbs= p; Builder: Bob = J. Rogers, Plano, TX
Engine/Model/Year: = 1987 13B Turbo

Source/Condition: =Rebuilt = by Bob J. Rogers from used (100K miles) Mazda RX-7

    Modifications: =    New rotor housings, 1 new end housing, new seals and = bearings.
           Intake:     Custom short intake with Turbonetics 60-1 Turbo & stock = intercooler
          Exhaust:     Custom Exhaust headers for Turbo (3” down pipe, no = muffler).
    PSRU/Re-Drive: =    RWS RD-1B 2.175/1

Engine = Control: RWS EC-2 EFI & Ignition Controller =

=Fuel control: =Fuel = Injected with four 550 cc injectors on TWM Throttle Body

       Fuel = pumps:     Dual EFI fuel = pumps from RWS
             Prop: =    Prince P-tip composite fixed-pitch 68x84
   Cooling System: =    Summit Race = Radiator, approx dimensions 27x19x3
       Oil System:     Stock Mazda Oil Cooler, aftermarket ADC Oil filter system   =
   = Installation:      = Conventional

= ; = Power: =Estimated = 200 hp – turbo normalized up to 17,000 feet

      First = Flown:     Expected yr 2007
       = Total Time:     10 hours ground run (not yet flying)
         Platform:     Bushby Mustang II kitplane

Best regards,
Dale R.

--

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