Honeywell BENDIX/KING KCS55A - KA 52 Technical Specifications; KA 57 Technical Specifications

BENDIX/KING KCS 55/55A
Page 1-6
©Honeywell International Inc. Do not print without express permission of Honeywell Rev 11, Apr/2007
1.3.7 KA 52
1.3.8 KA 57
SPECIFICATION CHARACTERISTIC
SIZE: See Fig. 2-7
WEIGHT: See Fig. 2-7
TSO: C6c, DO-138 Env. Cat. DANAAAXXXXXX
POWER INPUTS: +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)
SIGNAL INPUTS: Slaving meter drive signal from the KG 102A/KSG 105.
SIGNAL OUTPUTS: 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.
SPECIFICATION CHARACTERISTIC
SIZE: See Fig. 2-8
WEIGHT: See Fig. 2-8
MOUNTING: Rigid mount with four #6 screws.
MATING CONNECTOR: See paragraph 1.5 Installation Kits
POWER INPUTS:
±15 volts DC from the KG 102/102A
SIGNAL INPUTS: 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.
SIGNAL OUTPUTS: 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.
RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION
UP536434