BENDIXKing KI 300, Installation Manual

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89000004-101 KI 300 Installation Manual
Rev 1 Page 4-10
© Honeywell International Inc. Do not copy without express permission of Honeywell.
Setup Page Purpose
Min
Value Max
Value
Increment
Reference
Section
Slip/Skid Type
Used to set the slip/skid indicator type. (BALL,
POLYGON, BOTH)
n/a n/a n/a 4.7.3.10
Diagnostic
Mode Used for diagnostic purposes. Should remain
“No” unless requested by the factory.
No Yes n/a 4.7.3.11
AP Type
Used to select the autopilot interface when the
KI 300 is connected to the KA 310
(None, Analog, Analog w/FD, Digital)
n/a n/a n/a 4.7.3.12
Software Part
Numbers Used to verify the correct software part
numbers for the KI 300 and KA 310
n/a n/a n/a 4.7.3.13
AP Alignment
Used for autopilot alignment when the KA 310
is connected to a legacy (analog) autopilot.
(No, Yes)
n/a n/a n/a 4.7.3.14
AP Align Pitch
Used to set the Pitch output value for autopilot
alignment -60
degrees +60
degrees
1 degree 4.7.3.15
AP Align Roll
Used to set the Roll output value for autopilot
alignment -60
degrees +60
degrees
1 degree 4.7.3.15
Yaw Rate
Alignment This allows installation to manually check
rudder movement. +20
deg/sec -20
deg/sec 1
degree/sec
4.7.3.16
4.7.3.1 Pitch Trim and Roll Trim
The pitch trim and roll trim are used to make adjustments for various aircraft panel tilts and variations in
roll offsets. The aircraft should be leveled per the aircraft maintenance manual to determine the offset
values. After the aircraft is level, enter the appropriate pitch and roll trim values in the setup menu by
turning the rotary knob to the value that levels the ownship symbol on the KI 300 display and then
pressing in the knob to move to the next menu item.
4.7.3.2 Panel Type
If the aircraft panel is mounted on vibration absorbin g shock mounts, select “Float” as the Panel Type
within the setup pages, otherwise select “Hard”.
4.7.3.3 ADC Display
The air data displayed on the KI 300 has four options:

Display of both the indicated airspeed and baro corrected altitude

Display of only indicated airspeed

Display of only baro corrected altitude

No air data displayed.