Cirrus SR20 - Page 279

Cirrus Design Section 7
SR20 Airplane and Systems Description
P/N 21399-004 7-95P/N 21399-004 7-95
Figure 7-20
Baro-VNAV Vertical Deviation Indicator
SR20_FM02_3685
19 00
17 00
16 00
15 00
14 00
29.92 IN
35 00
18 00
V
16
60
40
LEGEND
1.Excessive Deviation
Indicator
2.Glidepath Indicator
1
2
1
1
NOTE
While Baro-VNAV is being utilized,
the Glidepath Indicator appears as
a magenta pentagon.
1
Revision A1