Garmin GFC 600 Pilot's Manual page 63

Automatic flight control system
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ESP Engage (45°) Aircraft
BC
141
7
6
5
175
°
149
Once engaged, ESP force will be applied between bank angles of 30° and 75°. The
HDG
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°.
Minimum
ESP Torque
(30º)
7°c
OAT
Configured
Bank Limit
(45º)
Maximum
ESP Torque
(60º)
190-01488-00 Rev. B
Roll Attitude = 44°
AP
YD
Before ESP Engage
Roll Increasing to ESP Engagement
123
°
LOC2
CDI
ESP Roll Operating Range When Engaged
(Force Increases as Roll Increases & Decreases as Roll Decreases)
ESP Disengage (30°) Aircraft
Roll Attitude = 46°
BC
PIT
ALTS
2
141
400
GS
170
2
500
160
2
400
40
7
150
20
6
14
2
3
2300
00
5
140
80
2
200
130
2
100
120
175
°
149
30.19
TAS
IN
HDG
KNOTS
2
N
1
O
G
0
P
1
H
D
7°c
G
OAT
2
0
1-2
PFD
Garmin GFC 600 Pilot's Guide
AP
YD
After ESP Engage
123
°
LOC2
2
CDI
AFCS
PIT
ALTS
2
40
2
500
2
400
4
2
2
3
2300
0
8
2
200
2
100
30.19
IN
2
N
1
O
G
0
P
Minimum
ESP Torque
1
(30º)
2
Configured
0
Bank Limit
(45º)
1-2
PFD
Maximum
ESP Torque
(60º)
55

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