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Steve, I want to do a high speed run with the prop at full cruise pitch tue. eve., will send you those also, temps are in the response to Ed. David From: "Steven W. Boese" <SBoese@uwyo.edu> To: "Rotary motors in aircraft" <flyrotary@lancaironline.net> Sent: Sunday, August 18, 2013 11:29:34 PM Subject: [FlyRotary] Re: Update RV6A Rotary in MI.
David,
Let me echo Ed's congratulations. I'm also interested in temperature data.
Steve Boese
RV6A, 1986 13B NA, RD1A, EC2
From: Rotary motors in aircraft <flyrotary@lancaironline.net> on behalf of Ed Anderson <eanderson@carolina.rr.com>
Sent: Sunday, August 18, 2013 3:35 PM
To: Rotary motors in aircraft
Subject: [FlyRotary] Re: Update RV6A Rotary in MI.
Congratulations, David!!
Sounds like everything is going A – OK!!
How are temps?
Ed
Sent: Sunday, August 18, 2013 4:33 PM
Subject: [FlyRotary] Update RV6A Rotary in MI.
3000' , 74deg. F, 6700rpm, 26.5 MAP, high rpm takeoff pitch set on prop, 165 MPH ind. ( circling over airport ) RV6A, 1120#, Bruce Turrantine 13B, 20" intake runners, 3.5" throttlebody
( from 2001 Cadillac Northstar eng. ), 22" 1-7/8 ID" .60" wall 304 SS exhaust headers into 3" X16" pipe into Hushpower Res. under fus., Conversion Concepts bed eng. mount, Mazda oil cooler under RWS 2.17 psru, GM evap. core x 2 rads., GM 580 coils x
4, Ivoprop 68" Magnum 65-105 pitch elect. inflight adjust with custom faired transition from spinner to prop blades, 23 hrs. ground testing, 12 hrs. airtime over Mason Jewett Field, will now remove cowl one more time for inspection, then start to do long
distance flights, 100 mile rad. from Mason with a crew member for computer tuning made available by FAA ( ask & you will receive ), need 40 hrs. David R. Cook
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