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Too Low Terrain SYS 16 EGPWS - Terrain closure low altitude
Traffic, Traffic SYS 16 TCAS - Conduct visual search for intruder
Windshear, Windshear SYS 16 EGPWS - WINDSHR (decreasing performance)
500, 100, 50, 30 SYS 16 EGPWS - Descending altitude callouts
VOICE MESSAGE - ALPHABETICAL
W = WARNING
SYS = SYSTEM EICAS/PFD INDICATION
VOICE MESSAGE TYPE CH.REF
7-22 For Training Purposes Only
Sept 04
P I LOT T R A I N I N G GU I D E
ELECTRONIC DISPLAY SYSTEM
AURAL WARNING TEST
Most aural alerts are exercised as part of their own system test. For all other aural
alerts, an AURAL WARNING TEST can be initiated via the Electrical Management
System Control Display Unit (EMS CDU) located on the pilot’s and copilot’s side
panel. There are two warning test selections provided to test the Integrated Avionics
Computer (IAC 1 and IAC 2).
NOTE
TEST is initiated by pressing activation key and can be
terminated by pressing activation key again.
The test sequences through each tone and/or voice message in the following priority
order:
• AURAL WARNING TEST 1 aural 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)
M
BRT
CIRCUIT BREAKER SYSTEM
STAT SYS BUS
PREV
PAGE
NEXT
PAGE
CNTL TEST
BUS
EMER
CONT
TEST CONTROL 1/2
FIRE TEST
STALL TEST
AURAL WARNING TEST 2
LAMP TEST 1
LAMP TEST 2
AURAL WARNING TEST 1
OFF
OFF
OFF
OFF
OFF
OFF
M
BRT
CIRCUIT BREAKER SYSTEM
STAT SYS BUS
PREV
PAGE
NEXT
PAGE
CNTL TEST
BUS
EMER
CONT
TEST CONTROL 1/2
FIRE TEST
STALL TEST
AURAL WARNING TEST 1
AURAL WARNING TEST 2
LAMP TEST 1
LAMP TEST 2
TEST
OFF
OFF
OFF
OFF
OFF
NOTE: TEST is initiated by pressing activation key and
can be terminated by pressing activation key again.
Test duration is 60 seconds.
Activation Key
GX_07_022
For Training Purposes Only
Sept 04
7-23
P I LOT T R A I N I N G GU I D E
ELECTRONIC DISPLAY SYSTEM
• GEAR
• Single Cavalry Charge tone (autopilot disengage)
• AUTOTHROTTLE aural
• C-chord tone (altitude alert - capture)
• Double C-chord (vertical track alert)
• Trim clacker (trim in motion)
• MINIMUMS
• SELCAL
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. Aurals for EGPWS and TCAS will not
be inhibited by muting the IACs.
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 CABIN ALT and APU OVERTEMP (T/O only), NORMAL
BRAKE FAIL, BRAKE OVHT, CABIN DELTA-P.
During takeoff, the caution and advisory messages are inhibited when:
• Weight On Wheels; and
• 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; or
• Pressure Altitude is greater than or equal to takeoff altitude +400 feet; or
• Indicated airspeed is less than 50 knots; or
AURAL WARNING
PUSH TO MUTE
IAC 1 IAC 2
MUTED MUTED
IAC 1 and IAC 2 PUSH TO MUTE Switches
Used to disable respective tone/aural generator
located in respective IACs.
GX_07_023
7-24 For Training Purposes Only
Sept 04
P I LOT T R A I N I N G GU I D E
ELECTRONIC DISPLAY SYSTEM
• Takeoff inhibit has been active for 60 consecutive seconds
During landing, the caution and advisory messages are inhibited when:
• Landing gear down; and
• Radio altitude from 200 feet to less than or equal to 200 feet
The caution and advisory message inhibit is removed:
• 25 seconds after air to ground transition; or
• Radio altitude greater than 200 feet; or
• Indicated airspeed less than 50 knots
The following caution messages are NOT inhibited during takeoff and/or landing.
　
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