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automatically silence after two (2) seconds. Airplane overspeed cannot be
silenced as long as the overspeed condition exists. The landing gear unsafe
warning can be silenced, either manually or automatically, in all cases except
when the flaps are fully extended without the landing gear being down and locked.
The airplane has a radio altimeter-activated automatic horn silencing system that
will function above 1200 ft AGL except when the flaps are fully extended without
the landing gear being down and locked.
2. SPZ-8400 Tone Generator:
For SPZ-8400 equipped aircraft: A tone generator is incorporated into each fault
warning computer to provide audible sounds, calling the attention of the flight crew
to an associated message or condition. Tone volume is adjusted from the TONE
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prompt on the TEST page of the pilot’s display controller. The aural tones
provided by the tone generator are:
Type of Aural Tone: Condition:
Klaxon™ (Hi/Lo - Hi/Lo) Landing Gear Unsafe
Cricket Airplane Overspeed
Beep Altitude Alert
1 Chime CAS Advisory (1)
2 Chimes CAS Caution
3 Chimes CAS Warning
Lo/Lo/Lo A/T Disconnect
Lo/Hi/Lo Manual A/P Disconnect
NOTE(S):
(1) Only those messages not resulting from deliberate crew action.
CAS Warning and CAS Caution alerts can be silenced by pressing the respective
master capsule. CAS Advisory alerts cannot be manually silenced, but will
automatically silence after one cycle. Airplane overspeed cannot be silenced as
long as the overspeed condition exists. The landing gear unsafe warning can be
silenced, either manually or automatically, in all cases except when the flaps are
fully extended without the landing gear being down and locked. The airplane has
a radio altimeter-activated automatic horn silencing system that will function
above 1200 ft AGL except when the flaps are fully extended without the landing
gear being down and locked.
The following CAS Advisory messages do not generate a tone when activated:
AC EXT POWER FUEL XFLOW OPEN
APU ALT OFF GND SPOILER UNARM
L-R COWL AI ON IRS 1-2 HI LAT ALN
DC EXT POWER ISOLATION VLV OPEN
EXT BATT SWITCH ON MAINT SWITCH ON
FGC NOT USING IRS 1 (2) SPD BRAKE EXTENDED
FMS 3 ACTIVE TONE GEN 1-2 FAIL
FUEL INT TANK OPEN L-R WING AI
3. Warning/Caution Tone/Indication Inhibit Feature:
With the landing gear extended and at least one radio altimeter valid, some
Warning/Caution aural tones and the corresponding Master Warning Light/Master
Caution Light can be inhibited by depressing the glareshield inhibit switch.
All CAS ADVISORY (blue) tones and CAS CAUTION (amber) tones (single chime
and double chime, respectively), can be inhibited with the SWLP in AUTO or
MAN. (Exception: CAS CAUTION tone associated with the amber CPL DATA
INVALID amber CAS message.)
In airplanes with the Standby Warning Lights Panel removed (SPZ-8400
equipped aircraft), neither the CAS WARNING (red) tone (triple chime) nor
the Master Warning Light can be inhibited.
A. For SPZ-8000 Equipped Aircraft:
The following Warning/Caution aural tones and the corresponding Master
Warning Light/Master Caution Light annunciations cannot be inhibited:
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(1) CAS WARNING (red) aural tone and corresponding Master Warning
Light:
L/R REV UNLOCK L/R PYLON HOT SMOKE DETECT
L/R FUEL FILTER L/R FUEL PRES LOW FLAME DETECT
L/R ENGINE HOT L/R OIL PRES LOW
AFT EQUIP HOT BAGGAGE DOOR
GND SPOILER ENG FIRE LOOP ALRT
CHECK PFD ACFT CONFIGURATION
(2) CAS CAUTION (amber) aural tone and corresponding Master
Caution Light:
• CPL DATA INVALID
B. For SPZ-8400 Equipped Aircraft:
With the SWLP in “MAN”, or with the SWLP removed:
(1) CAS WARNING (red) aural tone and corresponding Master Warning
Light:
L/R REV UNLOCK L/R PYLON HOT
L/R FUEL FILTER L/R FUEL PRES LOW
L/R ENGINE HOT L/R OIL PRES LOW
AFT EQUIP HOT BAGGAGE DOOR
GND SPOILER ENG FIRE LOOP ALRT
CHECK PFD ACFT CONFIGURATION
MAIN DOOR APU FIRE
CABIN PRESSURE LOW CABIN DIFF 9.8
DAU 1-2 MISCOMPARE SMOKE DETECT
FLAME DETECT
(2) CAS CAUTION (amber) aural tone and corresponding Master
Caution Light:
• CPL DATA INVALID
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04-01-00 MESSAGES AND ANNUNCIATIONS PROCEDURES
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湾流4操作手册 Gulfstream IV Operating Manual 3(47)
