Honeywell BENDIX/KING KCS55 Installation Manual page 16

RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION
BENDIX/KING
SPECIFICATION
SIZE:
WEIGHT:
TSO:
POWER INPUTS:
SIGNAL INPUTS:
SIGNAL OUTPUTS:
1.3.7 KA 52
SPECIFICATION
SIZE:
WEIGHT:
MOUNTING:
MATING CONNECTOR:
POWER INPUTS:
SIGNAL INPUTS:
SIGNAL OUTPUTS:
1.3.8 KA 57
Page 1-6
©Honeywell International Inc. Do not print without express permission of Honeywell
CHARACTERISTIC
See Fig. 2-7
See Fig. 2-7
C6c, DO-138 Env. Cat. DANAAAXXXXXX
+5VDC from KG 102A or +12VDC from KSG 105
7.2VAC 400Hz from KG 102A or 26VAC 400Hz from KSG
105
+5VDC Lamp Supply (-03 version)
+14VDC Lamp Supply (-00/-05 version)
+28VDC Lamp Supply
(-01/-02/-04/-06 versions)
Slaving meter drive signal from the KG 102A/KSG 105.
Magnetic Azimuth Transmitter compensation outputs for
North/South and East/West correction.
Clockwise and counterclockwise manual slew signals to
the KG 102A/KSG 105.
Slave/free gyro mode logic signal to the KG 102A/KSG
105.
CHARACTERISTIC
See Fig. 2-8
See Fig. 2-8
Rigid mount with four #6 screws.
See paragraph 1.5 Installation Kits
±
15 volts DC from the KG 102/102A
Heading select DC input from the KI 525/525A
Course datum DC input from the KI 525/525A
AC reference input from the aircraft autopilot system at 5
volts R.M.S. minimum.
Heading select AC output transformer isolated and phase
locked to the reference input from the autopilot.
Course datum AC output transformer isolated and phase
locked to the reference input from the autopilot.
KCS 55/55A
Rev 11, Apr/2007