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CSP C--013--067
2. MODE S TRANSPONDER (FLIGHT ID) <1096>
Mode S also has the capability to display either a 4--digit squawk code or the flight
identification (FLT ID) on line 4 of the RTU Top Level Page. Selection of either the squawk
code or the FLT ID for display on the Top Level Page is made on the ATC Main Page.
To access the ATC Main Page from the Top Level Page, the ATC Line Select Key is pressed
twice. Once the Main Page is displayed, the DISPLAY Line Select Key is pressed to select
either the SQUAWK or FLT ID (the selected function will be displayed larger). The selected
function is then displayed on line 3 of the Main Page, line 4 of the Top Level Page and on
the FLT ID Page. To modify the squawk code or the FLT ID on the Top Level Page, the ATC
Line Select Key is pressed, which will cause a tune window to surround the left character.
The small Tuning Knob is then used to change the character displayed in the tune window.
The RTU then waits 2 seconds after knob rotation stops before locking in the new character.
Rotating the large tune knob cycles the tune window from character to character.
To access the FLIGHT ID Main Page from the ATC Main Page, the FLT ID key is pressed
twice. On the FLIGHT ID Main Page, the RTU displays an Active and Preset Flight ID. By
pressing the top right line--select key the ACTIVE and Preset FLT ID will swap when the tune
window is on a Preset Flight ID character.
The FMS can also display the FLIGHT ID on the ”RADIO TUNING PAGE” page 2 of 2,
adjacent to the top right line select key on the CDU. To input the FLIGHT ID data:
(a) Press the top right line select key on the CDU so that the selection box
highlights the FLIGHT ID information field.
(b) Input the FLT ID data, via the CDU keypad, where it will appear on the
bottom left corner of the page (in brackets).
(c) After the FLT ID has been inputted, press the top right line select key and
check that the proper FLT ID appears adjacent to the top right line select
key.
Vol. 1 18--60--4
NAVIGATION SYSTEMS
Air Traffic Control Transponder System REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
Air Traffic Control Transponder System --- Radio Tuning Unit
Figure 18---60---3
Radio Tuning Unit -- Top Level Page
Center Pedestal
IDENT
Pushed at ATC request; causes an
additional identification pattern on ATC
ground radar screen.
Transponder Code (green)
Turns white when selected to standby.
Tuning Window (white)
Tuning Knob
ATC Key
Push key once to tune frequency
with tuning knob. Push key twice to
select ATC main page.
Mode Messages (cyan)
STBY -- Both transponders are in
standby mode. Code turns white.
ALT OFF -- Mode C selected off.
ID -- Identification has been selected.
R -- Transponder is responding to an
interrogation.
Mode C, altitude reporting selection is made on the ATC main page of the radio tuning unit.
Air Traffic Control Transponder System ---
Radio Tuning Unit --- ATC Main Page
Figure 18---60---4
Radio Tuning Unit -- ATC Main Page
Center Pedestal
Altitude Reporting
Used to turn altitude reporting
feature on and off. Selected
setting is displayed in cyan.
Reported Altitude
Vol. 1 18--60--5
NAVIGATION SYSTEMS
Air Traffic Control Transponder System Sep 09/02
Flight Crew Operating Manual
CSP C--013--067
A. System Circuit Breakers
SYSTEM SUB--SYSTEM CB NAME BUS BAR CB
PANEL
CB
LOCATION
NOTES
Air Traffic
Control Transponder
XPDR 1 DC
ESSENTIAL 2
V5
XPDR 2 DC BUS 2
H8
Vol. 1 18--60--6
NAVIGATION SYSTEMS
Air Traffic Control Transponder System REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
THIS PAGE INTENTIONALLY LEFT BLANK
NAVIGATION SYSTEMS Vol. 1 18--70--1
Traffic Alert and Collision Avoidance
System REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
1. TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM
The traffic alert and collision avoidance system (TCAS) is an airborne system that
interrogates the air traffic control transponders of nearby aircraft to identify and display
potential and predicted collision threats. TCAS surveillance range is up to 40 nautical miles
and can detect and track up to 30 aircraft simultaneously. The system computes range,
bearing and closure rates of other transponder equipped aircraft.
A mode “S” Transponder is installed on the aircraft. The transponder provides air-to-air
communications for coordinating the resolution maneuvers between TCAS equipped aircraft.
　
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