190-00820-08 Rev. A
Cirrus Perspective
™
by Garmin – Pilot’s Guide for the SR20/SR22/SR22T
577
ADDITIONAL FEATURES
SY
STEM
O
VER
VIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO P
ANEL
& CNS
FLIGHT
MANA
GEMENT
HAZARD
AV
OID
ANCE
AFCS
ADDITIONAL
FEA
TURES
APPENDICES
INDEX
Once engaged, ESP
™
force will be applied between 30
°
and 75
°
, as illustrated in Figure 8-112. The force
increases as roll attitude increases and decreases as roll attitude decreases. The applied force is intended to
encourage pilot input that returns the airplane to a more normal roll attitude. As roll attitude decreases, ESP
™
will disengage at 30°.
Figure 8-112 ESP Roll Operating Range When Engaged
(Force Increases as Roll Increases & Decreases as Roll Decreases)
0º
10º
10º
20º
20º
30º
30º
45º
45º
60º
60º
75º
75º
90º
90º
ESP
™
is automatically disengaged if the aircraft reaches the autopilot roll engagement attitude limit of 75
°
(Figure 8-113).
Figure 8-113 Roll Attitude Autopilot Engagement Limit (ESP Engaged)
ESP Upper Disengage Limit (75°)
Aircraft Roll Attitude = 74°
PITCH ENGAGEMENT
ESP
™
engages at 17.5
°
nose-up and 15.5
°
nose-down. Once ESP
™
is engaged, it will apply opposing force
between 17.5
°
and 50
°
nose-up and between 15.5
°
and 50
°
nose-down, as indicated in Figure 8-114. Maximum
opposing force is applied between 22.5
°
and 50
°
nose-up and between 20.5
°
and 50
°
nose-down.
Summary of Contents for Cirrus Perspective SR20
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