Hi Tracy, thanks for the trip report!.

The rotary is hard to get cabin heat.  The exhaust is bigger diameter than most aircraft exhaust, so off the shelf heat muffs are hard to come by, not to mention difficult to fit (finding space) and potentially dangerous.  I have had poor success at getting sufficient heat off the oil or water cooler.  So besides sealing up cabin leaks, I found the soulution, heated seats. 

Got these on Amazon for $45 for TWO seats.  Installed in a couple of hours.  Work great.  My tush can only take the high setting for 20 min or so.  Makes all the difference.

http://www.amazon.com/gp/product/B005PJ334G

Dave Leonard

Turbo Rotary RV-6 N4VY

On Wed, Aug 6, 2014 at 11:38 AM, Tracy <flyrotary@lancaironline.net> wrote:

Here's some trip data from a flight from Florida to Colorado in the 20B powered RV-8.    It's the first long trip where I was able to fly at or near the altitudes it was optimized for.   It didn't do as well as I had hoped in terms of fuel economy but the numbers were as good or slightly better than the typical Lycoming powered RV numbers I hear.   It is only slightly faster than my Renesis powered RV-4 at cruise conditions and reasonable fuel flow.  But what I like about it is the effortlessness with which it does the job.  There is always a handful of throttle left for reserve in any normal flight situation.

Full throttle is reserved for those few seconds between rudder effectiveness at 30mph and lift off speed at 60.  As soon as the wheels break ground I typically reduce manifold pressure to 24".   Cruise climb is done at between 18 and 19" depending on takeoff weight at around 700 FPM.  Cruise altitude was limited to 15,000 this trip by temperature.  I wasn't thinking and wore only a thin jacket and I don't have cabin heat.   All three legs were flown at 14,500 in a very unusual high pressure system the whole way with almost zero wind.  Here are the raw numbers:

Altitude       14,500
OAT              35 -  43F
TAS              174  -   182 MPH  *
Fuel Flow     8 GPH
Engine RPM  5250 - 5450
Manifold Pressure    14.3"
% Power       30%   (As calculated by EM3)
EGT              1450F
Water temp   145 - 150
Oil Temp       160        (Cowl flap would help temps and airspeed)
Total flight hours on trip  9.2

*  Fuel flow was held constant, TAS varied with fuel batch.  Low number was with Florida gas with about 8% ethanol.   Refueled at Charlie England's place (Thanks for the hospitality and fuel service Charlie!).  Not sure wether it had ethanol or not but TAS was a few MPH better.   After refueling at 47K in Kansas with no ethanol mogas, the TAS reached the highest number.

Tracy

Sent from my iPad
--
Homepage:  http://www.flyrotary.com/
Archive and UnSub:   http://mail.lancaironline.net:81/lists/flyrotary/List.html