89000004-200
KA 310 STC Installation Manual
Rev 0
Page 3-4
© Honeywell International Inc. Do not copy without express permission of Honeywell.
3.5.2.2
KA 310 Installation Considerations in KAP 150/KAP 200/KFC 150/KFC 200 Flight Control
System
When installing the KA310 with the KI 300 to provide intended functions of the KI 255/KI 256/KG 258
and KRG 331 (yaw rate gyro) in KAP 150/KAP 200/KFC 150/KFC 200 autopilot system, refer to Figure 3-1
for a system depiction of the wiring that will be required.
Refer to Figure B-4 and Figure B-6 for Interconnect diagrams.
AIRPLANE POWER
PRIMARY BUS
(28V OR 14V)
DECISION HEIGHT
ALERT
(OPTIONAL FOR
INSTALLATION WITH
RADAR ALTIMETER)
KC 192
(KFC 150 SYSTEM)
2 AMP
ELECTRONIC
ATTITUDE
INDICATOR
KA 310
KC 295
(KAP 200/KFC 200
SYSTEM)
KC 296
(YAW COMPUTER)
KC 191
(KAP 150 SYSTEM)
Figure 3-1 Installation of KA310 in KAP 150/KAP 200/KFC 150/KFC 200
Flight Control System
REF:
RELEASED FOR THE EXCLUSIVE USE BY: HONEYWELL EMPLOYEE AMERICAS
UP793797
