BendixKing CNI 5000 - Manual (Page 14)

13
FUNCTION SELECTOR
The Function Selector on the right side
of the transponder portion of the CNI 5000
is used to select the different modes of
operation of the Mode S transponder.
The different modes are as follows:
OFF- The unit is not energized. When the
unit is turned from “OFF” to some other
mode, the unit will display the installer-pro-
grammed aircraft address and maximum
airspeed according to the following
sequence: (Does not apply to the
ATCRBS-only Systems):
a.) The “FL” window will display “ xe
“AA1”AA1” and the ident window will dis-
play the first 4 digits of the unique aircraft
address for 2 (two) seconds.
b.) The “FL” window will display “ xe
“AA2”AA2” and the ident window will dis-
play the last 4 digits of the unique aircraft
address for 2 (two) seconds.
c.) The “FL” window will display the lower
limit and the ident window shall display the
upper limit of the preprogrammed maxi-
mum airspeed range for 2 (two) seconds.
The airspeed range displayed is one of the
following six: 0-75, 75-150, 150-300, 300-
600, 600-1200, and greater than 1200.
SBY- The unit is energized, but is inhibited
from replying to any interrogation. “SBY” is
annunciated on the display in this mode.
The altitude display is disabled.
TST- (Test) The unit will illuminate all seg-
ments of the display for at least four sec-
onds. A series of tests are performed inter-
nally that check the integrity of the Mode S
system.
When a squitter error occurs, the
transponder is considered inoperative and
message will be reported on the altitude
display.
Whenever an EEPROM error is detected,
the message “F02” signifying internal EEP-
ROM failure, or “F03” signifying external
EEPROM failure, is reported in the altitude
side of the display.
When the unit detects a hardware fail-
ure that prevents the unit from operating as
a transponder, “F04” is displayed in the alti-
tude window.
If the unit displays any of these failure
messages, it should be taken in for service.
If the unit has no errors, it remains in
the test mode.
All replies are disabled during TEST.
GND- (Ground) The unit inhibits ATCRBS
Mode A & C interrogations but will reply to
all valid Mode S interrogations. The ID
4096 code is displayed on the right side of
the display and the altitude on the left.
“GND” is annunciated on the display in this
mode.
Note: An optional remote “air/ground”
switch may be installed on a landing gear
strut that will keep the Mode S unit in the
GND mode until airborne. The unit can
XPDR 1
PUSH
VFR
SBY
OFF
GND TST ON
ALT
R
IDT
FL
XPDR 1
PUSH
VFR
SBY
OFF
GND TST ON
ALT
R
IDT
FL
XPDR 1
PUSH
VFR
SBY
OFF
GND TST ON
ALT
R IDT
FL
XPDR 1
PUSH
VFR
SBY
OFF
GND TST ON
ALT
R 300
IDT
XPDR 1
PUSH
VFR
SBY
OFF
GND TST ON
ALT IDT
XPDR 1
PUSH
VFR
SBY
OFF
GND TST ON
ALT
ALT ON
GND SBY R 8888
IDT
FL
XPDR 1
PUSH
VFR
SBY
OFF
GND TST ON
ALT
IDT