Honeywell BENDIX/KING KCS55A - Ki 525;525 A

BENDIX/KING KCS 55/55A
Rev 11, Apr/2007
©Honeywell International Inc. Do not print without express permission of Honeywell Page 1-3
1.3.2 KI 525/525A (cont).
SPECIFICATION CHARACTERISTIC
SIZE: See Fig. 2-2
WEIGHT: See Fig. 2-2
MOUNTING: Flanged mounted through front of the instrument panel.
MATING CONNECTORS: See Paragraph 1.5 Installation Kits
POWER INPUTS: 14VDC, .36 amps or 28VDC, .27 amps (required for light-
ing and NAV flag power);
±15VDC, ±5VDC (provided by
the KG 102/102A)
Heading synchro transmitter: Requires a 26 volt, 400Hz
rotor excitation for a 3-wire stator output equal to 206 mil-
livolts per degree of heading rotation. (066-3029-01, 066-
3046-01/03/05/07/08/10/11/12 indicators only).
SIGNAL INPUTS: Slaving control transformer; 3-wire stator input from the
KMT 112.
VOR/LOC deviation meter: 150
± 20 microamperes
through a resistance of 1000
± 30 ohms for a full scale de-
flection of five dots.
To-From pointer 200
± 40 microamperes through a resis-
tance of 200
± 30 ohms for full deflection.
NAV warning flag: Disappears from view with an input of
225
± 15 microamperes through a resistance of 1000 ± 30
ohms.
Glideslope deviation pointers: 150
± 20 micro amperes
through a resistance of 1000
± 30 ohms for a full scale of
two dots.
Glideslope flag input: 230
± 50 microamperes through a
resistance of 1000
± 30 ohms. When glideslope is valid
and after a 2 to 12 second delay pointers will come into
view displaying deviation.
30Hz Course resolver: Omnirange zeroed at 300 de-
grees for 30Hz. Electrically equivalent to Clifton TWH-11-
F-08.
400Hz Course resolver: Electrically zeroed at 300 de-
grees for 400Hz. Electrically equivalent to Clifton TSH-
11-F-08. (066-3046-02/03/06/07/11/12 indicators only)
Drive signal for the heading loop drive motor from the KG
102/102A.
RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION
UP536434