Operation; Display Description; Ki 525/525A Indicator And Controls - Honeywell BENDIX/KING KCS55 Installation Manual

RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION
BENDIX/KING
3.1

DISPLAY DESCRIPTION

This section contains information pertaining to controls and indicators, operating procedures, and
emergency operation of the KCS 55/55A Pictorial Navigation System. Refer to Figures 3-1, 3-2
and 3-3 for additional information.
3.1.1

KI 525/525A INDICATOR AND CONTROLS

INDICATOR AND CONTROLS
Compass Card:
Heading Select Knob:
Symbolic Aircraft:
Reciprocal Course Pointer:
Course Select Knob:
Lateral Deviation Bar:
Glideslope Pointer:
Heading Select:
NAV Warning Flag:
Lubber Line:
Heading Warning Flag: (KI 525A only)
Power Flag (KI 525 only)
Selected Course Pointer:
To-From Indicator:
Slaving Meter:
Counterclockwise Manual
Heading Drive Pushbutton:
Rev 11, Apr/2007
©Honeywell International Inc. Do not print without express permission of Honeywell
SECTION III

OPERATION

FUNCTION
This rotating card displays gyro stabilized magnetic
compass in formation beneath the lubber line.
Positions the heading select marker relative to the
compass card.
Represents the relationship of the aircraft with respect
to the display.
Indicates the reciprocal of the selected course.
Positions the selected course pointer with respect to
the compass card.
Represents VOR radial or LOC course. When refer-
enced to the symbolic aircraft the position of the devi-
ation bar is the same as the position of the chosen
VOR radial or LOC Course to the air craft.
Represents the actual aircraft deviation from the
glideslope path. When unusable glideslope informa-
tion is present the glideslope pointer is biased out of
view. When a valid glideslope signal is received there
is a 2 to 12 second delay before the pointers come
into view.
Indicates the selected aircraft heading.
When unusable VOR/LOC information is present the
warning flag is in view.
Aircraft magnetic heading is read under this line.
Inadequate Power, manual slave, fast auto slave or
spin motor less than 50% normal speed.
Inadequate Power.
Indicates the selected VOR radial or LOC course.
Indicates the direction to the VOR station along the
selected radial.
Indicates the difference between the displayed head-
ing. Positive deflection indicates a clockwise error of
the compass card.
When the system is in the free gyro mode, engage-
ment of this pushbutton will cause the compass card
rotate counterclockwise at a constant rate of 360 de-
grees per minute.
KCS 55/55A
Page 3-1