Honeywell BENDIX/KING KCS55A - KG 102;102 A Technical Specifications; KMT 112 Technical Specifications

BENDIX/KING KCS 55/55A
Page 1-4
©Honeywell International Inc. Do not print without express permission of Honeywell Rev 11, Apr/2007
1.3.3 KG 102/102A
1.3.4 KMT 112
SPECIFICATION CHARACTERISTIC
SIGNAL OUTPUTS: Heading synchro transmitter:
Output equal to 206 millivolts per degree of heading rota-
tion. (066-3029-01 and 066-3046-01/03/05/07/08/10/11/
12 Indicators only)
Selected heading error output:
An internally excited transducer which supplies an error
output equal to 0.55 volts D.C. per degree of displace-
ment from the lubber line.
Selected course error output:
An internally excited transducer which supplies an error
output equal to .21 volts D.C. per degree of displacement
from the lubber line.
SIZE: See Fig. 2-3
WEIGHT: See Fig. 2-3
MOUNTING: Shock mounted (provided in installation kit)
MATING CONNECTOR: See Paragraph 1.5 Installation Kits
POWER INPUTS: 14VDC, 3.0 amperes or 28VDC, 1.5 amperes
SIGNAL INPUTS: Slaving error control transformer from the KI525/525A.
POWER OUTPUTS:
±15 and +5VDC reference voltages for the KI525/525A
and the KA 51/51A/51B.
A 7.2 VRMS, 400 Hz drive signal for the primary excitation
of the KMT 112 and for use in the KA 51/51A/51B.
A 5 VA maximum of 26 VAC, 400 Hz power is available
for all uses.
SIGNAL OUTPUTS: A drive signal for the heading loop drive motor in the KI
525/525A.
Slaving meter drive signal for the
KA 51/51A/51B.
(KG 102A Only) Pin a
supplies a ground when compass system is valid.
RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION
UP536434