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Indicates TCAS
system is in test.
Range Readout (white)
Indicates range selected at
the display control panel.
RADAR NOT AT TCAS RANGE (cyan)
Weather radar control has been
transferred and range disagrees with
TCAS range.
NOTES
2.
1.
TCAS can be overlaid on any map display mode.
Weather radar can be displayed on the MFD when in
TCAS mode (range: 5,10, 20 and 40 nm).
3. During an electrical transient, TCAS display range
may default to 10 nm.
NAVIGATION SYSTEMS Vol. 1 18--70--8
Traffic Alert and Collision Avoidance
System REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
C. Aural Warning
The system provides appropriate aural warnings to the flight crew when the TCAS
computer analysis of an aircraft signal predicts a penetration of TCAS protected
airspace. The voice warnings cannot be cancelled or reduced in volume.
TA voice warning is TRAFFIC -- TRAFFIC
RA voice warnings are:
S CLIMB, CLIMB, CLIMB
S DESCEND, DESCEND
S MONITOR VERTICAL SPEED
S CLIMB -- CROSSING CLIMB, CLIMB -- CROSSING CLIMB
S DESCEND -- CROSSING DESCEND, DESCEND -- CROSSING DESCEND
S INCREASE CLIMB, INCREASE CLIMB
S INCREASE DESCENT, INCREASE DESCENT
S CLIMB -- CLIMB NOW, CLIMB -- CLIMB NOW
S DESCEND -- DESCEND NOW, DESCEND -- DESCEND NOW
S MAINTAIN VERTICAL SPEED, MAINTAIN
S MAINTAIN VERTICAL SPEED, CROSSING MAINTAIN
S ADJUST VERTICAL SPEED, ADJUST
The clear advisory is CLEAR OF CONFLICT
Test voice messages are TCAS SYSTEM TEST OK or TCAS SYSTEM TEST FAIL.
NAVIGATION SYSTEMS Vol. 1 18--70--9
Traffic Alert and Collision Avoidance
System Sep 09/02
Flight Crew Operating Manual
CSP C--013--067
D. System Circuit Breakers
SYSTEM SUB--SYSTEM CB NAME BUS BAR CB
PANEL
CB
LOCATION
NOTES
Traffic Alert
and Collision
Avoidance
System
Transmitter /
Receiver TCAS AC
ESSENTIAL 1 V10
NAVIGATION SYSTEMS Vol. 1 18--70--10
Traffic Alert and Collision Avoidance
System Sep 09/02
Flight Crew Operating Manual
CSP C--013--067
THIS PAGE INTENTIONALLY LEFT BLANK
Vol. 1 18--80--1
NAVIGATION SYSTEMS
Ground Proximity Warning System REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
1. ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS) <2040>
The enhanced ground proximity warning system (EGPWS) is used to help prevent accidents
caused by unsafe flight maneuvers in proximity of terrain or severe windshear. The EGPWS
computer generates alerts and warnings by comparing the actual aircraft position
(programmed by the FMS) to terrain features and obstacles that are stored in the computer
database. The aural alerts, messages and visual annunciations are generated when the
boundaries of the following alerting envelopes are exceeded: <2040>
S Mode 1 Excessive descent rate
S Mode 2 Excessive terrain closure rate
S Mode 3 Altitude loss after take-off
S Mode 4 Unsafe terrain clearance
S Mode 5 Below glideslope alert
S Mode 6 Callouts (descent below minimums, altitude callouts and bank angle alert)
S Mode 7 Windshear detection and alerting
S Terrain clearance floor and terrain / obstacle awareness alerting and display
Radar or terrain information is displayed on the multifunctional displays by pressing the
RDR/TERR button on the display control panel.
NOTE
In the event of a momentary loss of AC electrical
power, the TERRAIN FAIL status message may be
displayed while the GPS satellites are reacquired
(approximately 75 seconds) and the FMS aircraft
position is re--entered.
Vol. 1 18--80--2
NAVIGATION SYSTEMS
Ground Proximity Warning System REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
Ground Proximity Warning System Interface Diagram <1015, 1025,2040>
Figure 18---80---1
GPWS
ADC 2
SPS
VHF NAVs
RAD ALTs
IRS 2
PSEU
SFECU
TAS/VS/ALT
GS DEV
ACC/ATT
TERRAIN INHIBIT
WINDSHEAR DISCRETES
WINDSHEAR
DISCRETES
LAT/LONG
GND TRK/SPEED
FLAP POS
AOA
WARNINGS
&
ALERTS
IAPS
(FMS/GPS)
PULL UP
GND
PROX
PULL UP
GND
PROX
TEST/GS CANCEL
AECU
EICAS
TCAS
STATUS
MESSAGES
AURAL
MESSAGES
AUDIO
PRIORITY
CB1--B14
AC BUS 1
GND PROX
WARN
Vol. 1 18--80--3
NAVIGATION SYSTEMS
Ground Proximity Warning System REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
　
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