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FAA Part 91.205

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tonybabb(at)alejandra.net
Guest

Posted: Mon Oct 09, 2006 3:33 pm Post subject: FAA Part 91.205

Hello OC,



I'd appreciate a copy of the table you mentioned



<SNIP>

Because this subject is a bit convoluted I have put together a table that 

lays the information out in fairly compact reference form. I will send you a



copy of this table attached to a separate email. If anyone else would like a



copy just email me. This table was also published on page 50 of the June 

2006 issue of Kitplanes magazine.

<SNIP>



Thanks,



Tony Babb

Velocity SEFG 62% done, 78% to go

www.alejandra.net/velocity

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khorton01(at)rogers.com
Guest

Posted: Mon Oct 09, 2006 4:27 pm Post subject: FAA Part 91.205

 	  Quote: 	
		  

 I was wondering if you could clearify FAA Part 91.205 for me.  As I

 understand this FAR it applies to  powered civil aircraft with a  

 standard

 category U.S. airworthiness certificate.  Is our experimental  

 airworthiness

 certificate under this catagory?  It requires a manifold pressure  

 gauge for

 each altitude engine.  It does not require a CHT or EGT.  This does  

 not

 seem right for experimental aircraft.  I would much rather have a  

 CHT and

 EGT than a manifold pressure gauge although I have all three on my  

 KIS.  I

 was also wondering if my VFR day only plane needs to have a strobe  

 and nav

 lights?


	


The reference to an "altitude engine" requires a study of FAR 1.1 to  

see that it means "a reciprocating aircraft engine having a rated  

takeoff power that is producible from sea level to an established  

higher altitude."  I.e. it means a turbo-charged or super-charged  

engine.  Anyone who has such an engine really should have a MP gauge,  

whether FAR  91.205 applies to them or not.



Kevin Horton

Ottawa, Canada

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