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#18
December 9th 03, 08:16 PM
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From DG website DG1000 flight manual:
http://www.dg-flugzeugbau.de/index-e.html ========== Warning: At higher altitudes the true airspeed is higher than the indicated airspeed, so VNE is reduced with altitude according to the table below, see also section 4.5.5. Altitude in [m] 0-3000 4000 5000 6000 7000 8000 VNE indicated km/h 270 256 243 230 217 205 Altitude in [ft] 0-10000 13000 16000 20000 23000 26000 VNE indicated kts. 146 138 131 124 117 111 ------- Simon. 19:54 09 December 2003, Arnold Pieper wrote: This seems to me to be some arbitrary way of staying conservative. Look at the manual of some gliders, that do have the limitation on IAS with Altitude. You will see that the table of IAS is not correcting the VNE as a TAS value. Nowhere in aviation VNE is considered a TAS value. 
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