Honeywell bendis king KLN 94, Maintenance Manual

Page: 57 / 172

BENDIX/KING KLN 94
Page 5-18 15599M00.JA Rev 0, Sept/2000
D. Two or more satellites should be acquired, an Sg of more than 4, and a HIT of GD
will be displayed after 5 minutes of run time.
E. Turn the right inner knob to the AUX +1 page. It should display the present state of
the GPS receiver as NAV D and an estimated position error of not more than
0.124nm.
F. If no failure is indicated, check “OK” on the Final Data Sheet.
5.2.4.21 HARDWARE FAILURE TEST
A. Press the MSG button on the unit.
B. Verify that no messages regarding hardware failures are displayed on the page.
C. If no failure is indicated, check “OK” on the Final Data Sheet.
5.2.4.22 POST TEST PROCEDURE
A. If the application software is updated, verify the SW REVISION by viewing the top
line of the AUX 14 page. SW REVISION 0X0X will be displayed, where 0X0X is the
last four digits of the of the KLN 94 Application Software 206-number.
A marking should be made in the Aircraft Log Book to indicate that the KLN 94 Ap-
plication Software has been updated.
The recommended wording in the log book is as follows:
“KLN 94 APPLICATION SOFTWARE IS AT SW REVISION 0X0X ON (current date).
B. Turn the unit power to OFF.
C. Disconnect the test harness and antenna cable.
D. Sign and date the Final Test Data Sheet.
__1_nm
-------
M>LEG
AUX +2
SV HIT Sg El Hz
11 GD 4 26 0