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attitude inside PTZ and away from PAZ.
Aircraft flight path will cross intruder’s altitude
Maintain Vertical Speed
Maintain
SYS 17 TCAS − Monitor pitch attitude to keep pitch
attitude inside PTZ and away from PAZ
Minimums SYS 17 At minimum altitude selected on PFD
Monitor Vertical Speed −
Monitor Vertical Speed
SYS 17 TCAS − Monitor pitch attitude to keep pitch
attitude inside PTZ and away from PAZ
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
03−10−17
AURALS (CONT'D)
VOICE MESSAGE − ALPHABETICAL
W = Warning
SYS = System
Voice Message Type Chapter
Ref.
EICAS/ PFD INDICATION
NO TAKEOFF W 10
&
15
CONFIG AIL TRIM
CONFIG RUD TRIM
CONFIG SLATS/FLAPS
CONFIG SPOILERS
CONFIG STAB TRIM
PARK BRAKE ON
Obstacle, Obstacle SYS 17 EGPWS − Excessive obstacle closure
Pull Up SYS 17 EGPWS − Corrective action after excessive
descent rate during approach
RIGHT ENGINE FIRE W 9 R ENG FIRE
Selcal SYS 6 SELCAL HF, SELCAL VHF 1, SELCAL
VHF 2, SELCAL VHF 3
Sink Rate SYS 17 EGPWS − Excessive descent rate during
approach
SMOKE W 9 SMOKE BAGGAGE
SMOKE FWD LAV
SMOKE AFT LAV
SMOKE CLOSET
SMOKE AVIONICS BAY
Terrain, Terrain SYS 17 EGPWS − Excessive terrain closure
Too Low Flap SYS 17 EGPWS − Insufficient flap, low altitude
Too Low Gear SYS 17 EGPWS − Gear up, low altitude
Too Low Obstacle SYS 17 Obstacle closure low altitude
Too Low Terrain SYS 17 EGPWS − Terrain closure low altitude
Traffic, Traffic SYS 17 TCAS − Conduct visual search for intruder
Windshear, Windshear SYS 17 EGPWS − WINDSHR (decreasing
performance)
500, 100, 50, 30 SYS 17 EGPWS − Descending altitude callouts
AURAL AND VISUAL WARNINGS
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
03−10−18
AURAL WARNING TEST
Most aural alerts are exercised as part of their own system test. For all other aural alerts, an AURAL
WARN TEST can be initiated via the Electrical Management System (EMS) Display Unit (DU)
located on the pilot’s and copilot’s side panel. There are two warning test selections provided to test
Integrated Avionics Computer (IAC 1 and IAC 2).
GF0310_019
STAT SYS BUS PREV CNTL TEST
PAGE
NEXT
PAGE
EMER
CNTL
BUS
STBY
CIRCUIT BREAKER SYSTEM
CIRCUIT BREAKER − SYSTEM 1/2
FIRE TEST
STALL TEST
AURAL WARNING TEST 1
LAMP TEST 1
LAMP TEST 2
OFF
NOTE: TEST is initiated by pressing activation key and can
be terminated by pressing activation key again.
OFF
OFF
OFF
OFF
AURAL WARNING TEST 2 TEST
Activation Key
BRT
The test sequences through each tone and/or voice message in the following priority order:
· “AURAL WARNING TEST 1”or “AURAL WARNING TEST 2”.
· “STALL” (stall shaker active).
· Continuous Tone (overspeed).
· Triple Chime tone (any warning).
· “NO TAKEOFF”.
· “LEFT ENGINE FIRE”.
· “RIGHT ENGINE FIRE”.
· “APU FIRE”.
· “SMOKE”.
· “CABIN ALTITUDE”.
· “GEAR BAY OVERHEAT”.
· “LEFT REVERSER UNLOCKED”.
· “RIGHT REVERSER UNLOCKED”.
· “NORMAL BRAKE FAIL”l.
· Single Chime (any caution).
· “GEAR”.
· Single Cavalry Charge tone (autopilot disengage).
· “AUTOTHROTTLE”.
· “ALTITUDE” (altitude alert − departure).
· Cchord
tone (altitude alert − capture).
· Double Cchord
tone (vertical track alert).
· Single Chime.
· Trim clacker (trim in motion).
· “MINIMUMS, MINIMUMS” (DH and MDA).
· “SELCAL, SELCAL”.
AURAL AND VISUAL WARNINGS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
03−10−19
AURAL WARNING PANEL
The aural warning panel, located on the overhead panel, is used to disable the tone/aural generators,
located in IAC 1 and IAC 2.
GF0310_020
IAC1 and IAC2 PUSH TO MUTE Switches
Used to disable respective tone/aural generator
located in the respective IACs.
PUSH TO MUTE
　
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