Mailing List flyrotary@lancaironline.net Message #30884
From: Ernest Christley <echristley@nc.rr.com>
Subject: Re: [FlyRotary] Re: Rotary installed weight comparison
Date: Fri, 24 Mar 2006 10:42:20 -0500
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Al Gietzen wrote:

The first column includes EVERYTHING (including coolant) back to the prop flange.  The right hand column is the number that is a reasonable comparison to what Lyc publishes for an IO 540.

 

*Engine/Ancilliaries*



 



 



 

 



 



 



 

Engine



260.0



 



260

Water Pump (inc. )



 



 



 

Alternator (inc.)



 



 



 

Air Pump



0.0



 



 

Oil pan



4.5



 



4.5

Induction Sys (comp)



10.0



 



10

Exhaust Man/Muff



12.5



 



12

Sec muff/Exit pipe



3.5



 



 

Mount brackets



3.5



 



 

Coils w/bracket



4.5



 



 

Starter



7



 



 

Re-drive



43



 



43

Main mount



15.0



 



 

Radiator 1



4.5



 



4.5

Radiator 2



6.0



 



6

Aux cooling fan



0.0



(none)



 

Oil cooler



10.0



 



 

Expansion tank



0.6



 



2.5

Fuel pumps/filter



3



 



 

Lines/fittings



4.5



(Est)



 

Coolant



18.0



(Est)



18

Exhaust baffle



2.5



 



 

Misc



3



 



 

 



 



 



 

Total Powerplant



415.6



 



355.5

 

Did something go awry with the cut'n'paste?

--
        ,|"|"|,               Ernest Christley     |
----===<{{(oQo)}}>===----     Dyke Delta Builder    |
       o|  d  |o          www.ernest.isa-geek.org  |
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