On Thu, 20 Jan 2005 20:06:13 +0000, Dave Martin
<[EMAIL PROTECTED]> wrote:

> Is there any way to get a compensated 'TAS' output to drive the ASI because I
> *think* the B1900D's ASI is compensated (but I must check)

I'd be pretty incredibly surprised to see an ASI doing that.  Some
ASIs do have a circular sliderule (or similar) around the edge to
calculate true airspeed, but all ASIs necessarily show indicated
airspeed because that's what has the most aerodynamic significance for
the plane (i.e. it's going to rotate, climb, approach, stall, etc. at
the same indicated airspeeds at 10,000 ft density altitude and at sea
level, even though the true airspeeds are significantly different).

What is the density altitude is the TAS for the Beech 1900 specified
at?  25,000 ft?  If so, then divide by about 1.5 to find out what
number you should see on the ASI.


All the best,


David

-- 
http://www.megginson.com/

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