Ki 525/525A - Honeywell BENDIX/KING KCS55 Installation Manual

RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION
BENDIX/KING
SPECIFICATION
SIZE:
WEIGHT:
MOUNTING:
MATING CONNECTORS:
POWER INPUTS:
SIGNAL INPUTS:
1.3.2 KI 525/525A (cont).
Rev 11, Apr/2007
©Honeywell International Inc. Do not print without express permission of Honeywell
CHARACTERISTIC
See Fig. 2-2
See Fig. 2-2
Flanged mounted through front of the instrument panel.
See Paragraph 1.5 Installation Kits
14VDC, .36 amps or 28VDC, .27 amps (required for light-
ing and NAV flag power);
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).
Slaving control transformer; 3-wire stator input from the
KMT 112.
VOR/LOC deviation meter: 150
through a resistance of 1000
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
ohms.
Glideslope deviation pointers: 150
through a resistance of 1000
two dots.
Glideslope flag input: 230
±
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.
KCS 55/55A
± ±
15VDC, 5VDC (provided by
±
20 microamperes
±
30 ohms for a full scale de-
±
20 micro amperes
±
30 ohms for a full scale of
±
50 microamperes through a
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±
30