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500, 100, 50, 30 SYS 17 EGPWS − Descending altitude callouts
AURAL AND VISUAL WARNINGS
Flight Crew Operating Manual Rev 2A, Apr 11, 2005
CSP 700−5000−6
Volume 2
03−10−16
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) Control Display Unit
(CDU) 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”.
· 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 2A, Apr 11, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
03−10−17
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. Aural for EGPWS and TCAS will not be inhibited by muting the IACs.
GF0310_020
IAC1 and IAC2 PUSH TO MUTE Switches
Used to disable respective tone/aural generator
located in the respective IACs.
PUSH TO MUTE
IAC 1 IAC 2
AURAL WARNING
MUTED MUTED
INHIBITS
During takeoff
and landing, the IAC fault warning computer, will process inhibit logic to minimize
spurious or distracting messages. Warnings and status messages are not inhibited except for
APU OVERTEMP (TO only), NORM BRAKE FAIL (TO only), CABIN ALT, CABIN DELTA P and
BRAKE OVHT (TO only).
During takeoff,
the caution and advisory messages are inhibited when:
· Weight On Wheels.
· Indicated airspeed transitions from less than 80 knots to greater than or equal to 80 knots.
The caution and advisory messages’ inhibit is removed 25 seconds after:
· Weight Off Wheels.
· Pressure Altitude is greater than or equal to takeoff
altitude +400 feet.
· Indicated airspeed is less than 50 knots.
· Takeoff
inhibit has been active for 60 consecutive seconds.
During landing, the caution and advisory messages are inhibited when:
· Landing gear down.
· Radio altitude transitions from 200 feet to less than or equal to 200 feet.
The caution and advisory messages’ inhibit is removed:
· 25 seconds after air to ground transition.
· Radio altitude greater than 200 feet.
· Indicated airspeed less than 50 knots.
AURAL AND VISUAL WARNINGS
Flight Crew Operating Manual Rev 2A, Apr 11, 2005
CSP 700−5000−6
Volume 2
03−10−18
INHIBITS (CONT'D)
The following caution and advisory messages are NOT inhibited during takeoff
and/or landing.
Airplane System Caution Messages Advisory Messages
AFCS AP MISTRIM NOSE UPDN
(Ldg only)
AP MISTRIM LWDRWD
(Ldg only)
YD 1−2 FAIL
YD OFF
YD NOT CENTERED (TO only)
　
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