At 01:36 PM 9/19/2015, you wrote:
>My understanding is that the intent of a (wet) compass requirement 
>is as a last resort/emergency/always available navigation tool - 
>with the fluid serving as a dampening influence compared to a dry 
>compass with no dampening.  In order for any other type to qualify, 
>there must be no external power needed to make it operational. 
>Therefore, unless one of the magnetometers you have researched will 
>always operate reliably without externally supplied power, then no, 
>I can't agree.
>George
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I think you're reading too much "intent" in to item 3 below.  These 
types of instruments weren't available when the reg's were written. 
What part of "magnetic direction indicator"  does the new instrument 
not meet?  It says nothing about requiring it to be a wet compass or 
requiring some level of reliability.  The only requirement I've ever 
seen is a compass correction card.  If this instrument is accurate to 
within one or two degrees I doubt if even that is needed.  If the FAA 
disagrees they need to come back with a description of exactly what 
they require.  Don't impose any self inflicting restrictions. The 
reg's say "magnetic direction indicator".  Go with that and make the 
FAA justify a "no" answer.

A friend of mine had a restriction on the 40 hour test phase on his 
RV10 of operation from a single named airport.  I told him that's not 
in the reg's and was simply a restriction put in by the designated 
inspector.  When he went to the FSDO to get his mechanic's license 
for the 10, he questioned the FSDO rep and she said , yes, is in the 
regs.  He asked her to look it up.  She did and came back and removed 
the restriction.  He then asked her  about a second pilot during 
flight testing (40 hours) and she said "no, that's only for multi 
engine aircraft".  Some of these people don't know what they are 
talking about.  AC no. 90-116 has been out for one year now and she 
apparently has no knowledge of it.  Really?  Maybe a government shut 
down is in order.

Larry



FAA requirements as listed in the regs (part 91).

(1) Airspeed indicator.

(2) Altimeter.

(3) Magnetic direction indicator.

(4) Tachometer for each engine.

(5) Oil pressure gauge for each engine using pressure system.

(6) Temperature gauge for each liquid-cooled engine.

(7) Oil temperature gauge for each air-cooled engine.

(8) Manifold pressure gauge for each altitude engine.

(9) Fuel gauge indicating the quantity of fuel in each tank.

(10) Landing gear position indicator, if the aircraft has a 
retractable landing gear.




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