Normal operation, Pitch roll yaw, Man cw auto ccw – BendixKing KFC 500 User Manual
Page 14: 1dire ctio n of fl ight, Dire ctio n of fl ight, Vs alt 1000 ft/min, Up dn in hg hpa den alt sel vs, Alert, Display system, Navigation receivers
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18
006-18081-0000
March 27, 1998
19
Normal Operation
006-18081-0000
March 27, 1998
RADIO
ICS
FOOT
SW
RADIO
ICS
FOOT
SW
FORCE
TRIM 1
OFF
AP ON
SCAS ON
FORCE
TRIM 2
OFF
AP
1 2
PIC
R
ı
APR
HDG
ALT
BL
IAS
AP
FD
NAV
VS
SCAS
1
KDC 481
KCP 520
ı
KCP 520
ı
Primary KRG 333
Rate/Acceleration Sensor
Primary
KCP 520
Flight
Computer
KMS 541
Mode Selector
KCS 305 Compass
Trim Actuator
Primary Pitch
Linear Actuator
Control Position
Synchro
Cyclic
Switches
PITCH
ROLL
YAW
Collective
Switches
Primary KVG 350
Vertical Gyro
IIDS
Control Position
Synchro
Control Position
Synchro
Collective Control
Position Synchro
Trim Actuator
Primary Roll
Linear Actuator
Trim Actuator
Linear Actuator
SCAS/AP Remote
Switches/Annunciators
MAN
CW
AUTO
CCW
-
+
KSG 105
1
DIRE
CTIO
N
OF FL
IGHT
Secondary
KCP 520
Flight
Computer
Secondary KRG 333
Rate/Acceleration Sensor
DIRE
CTIO
N
OF FL
IGHT
Secondary KVG 350
Vertical Gyro
Secondary Pitch
Linear Actuator
Secondary Roll
Linear Actuator
SCAS &
AP PWR 2
OFF
EFIS PWR
PLT
OFF
EFIS PWR
COPLT
OFF
SCAS &
AP PWR 1
OFF
Display
System
KDC 481T Air Data
Computer
0
2
3
4
5
6
7
8
9
ALT
VS
ALT
1000 FT/MIN
VS
2
3
2
1
1
.5
.5
0
UP
DN
IN HG HPa
DEN ALT
SEL
VS
1,160
30.08 1,700
1
ENG
SEL
ı
BARO
U
P SH
E
T
S T
SEL
U
P LL
V S
3
ALT
ALERT
KAV 485
Altimeter/VSI
Navigation
Receivers
AFCS
GROUND
TEST
KFC 500 Dual SCAS/Autopilot/Single Flight Director System Block Diagram