Honeywell KLN 94 GPS Receiver User Manual


 
B KLN 94
Rev. 4, Jan/2003 10599I04.CDL Page 2-73
B. Configuring the KLN 94 to operate with KFC 225 (attitude-based flight control system):
1. Select MNT 8 page.
2. Push CRSR button. The cursor will appear over the second line.
3. Select “Bank Angle” and push CRSR again. The screen should look like:
C. Configuring the KLN 94to operate with KAP 140 (turn-rate-based flight control system):
1. Select MNT 8 page.
2. Push CRSR button. The cursor will appear over the second line.
3. Select “Turn Rate”. “Max Turn Rate” should appear on the fourth line.
4. Turn the outer knob once. The cursor should move to the bottom line.
5. Dial in the autopilot’s maximum turn rate. For KAP 140 as of 7/17/2002, it is 2.7
degrees per second.
6. Push the CRSR agin. The screen should look like:
2.4.2 POST INSTALLATION CHECKOUT PROCEDURE
This procedure is divided into two major sections. The first section deals with “Stand Alone”
installations in which none of the signal Input/Output capability of the unit is utilized, (except for
the RF input signal from the antenna). In this type of installation the only connections to the KLN
94 are the cable from the GPS antenna, the aircraft power and ground leads, and the lighting bus
wires.
NOTE
All output data is read from the unit front panel display and all input to the unit
is via the front panel controls.
The second part of this procedure deals with an installation in which some or all of the electrical
signal I/O have been utilized. This second section is divided in such a way that each input or
output signal is treated separately, and hence only those subsections that apply to a given
installation will be conducted.
Configuration
Module
DC Roll Steering
Bank Angle
MNT 8
Configuration
Module
DC Roll Steering
Turn Rate
MNT 8
Max Turn Rate
2.7 dps