Aircraft Publia~tions
Piper Con~;inclic
250
(E:uly Model)
Section
-
5
Perfornmnce
ALTITUDE CONVERSION CHART
**
NOTE
* *
THIS CHART SHOULD BE USED TO DETERMINE DENSITY ALTITUDE FROM
EXISTING TEMPERATURE AND PRESSURE ALTITUDE CONDITIONS.
FOR USE WITH THE ACCOMPANYING PERFORMANCE CHARTS
Copyright: 1993
I
I
I
I
I
I
I
I
I
.40
-3 0
-20
-I0
0
10
20
3 0
3 8
TEMPERATURE - DEGREES C.
FIGURE
5-03
Page
5-7