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of the display and are preceded by ADV. The caution displays, in larger characters than the advisory
displays, appear immediately above the advisory displays. The caution lights, located on the caution
lights panel and the instrument panel, are yellow lights. The advisory lights, scattered throughout the
cockpit(s), are green. Lights that have been lit on the caution lights panel flash when overheated to
prevent light damage.
2.16.2.1 MASTER CAUTION Light. A yellow MASTER CAUTION light, on the upper left part of the
instrument panel, comes on when any of the caution lights or caution displays come on. The MASTER
CAUTION light goes out when it is pressed (reset). An audio tone is initiated whenever the MASTER
CAUTION light comes on. The tone is of 0.8 second duration and consists of a 0.25 second sound
followed by a 0.15 second sound of higher pitch, followed by one repetition of these sounds. The tone
does not repeat unless the original condition causing the tone clears and recurs 5 seconds after the first
tone, regardless of whether or not the MASTER CAUTION is reset. Additional cautions sound the
tone, regardless of whether or not the MASTER CAUTION is reset, providing about 5 seconds have
elapsed since the previous caution. Pressing the MASTER CAUTION when it is unlighted causes the
uncorrected caution and advisory displays to reposition to the left and to a lower level, provided there
is available space vacated by corrected caution and advisory displays. To restack the cautions and
advisories when the MASTER CAUTION is lighted, the MASTER CAUTION must be pressed twice:
first, to turn off the MASTER CAUTION light and second, to reposition the caution and advisory
displays. A reset MASTER CAUTION light (and tone) comes on if there is at least one uncorrected
caution present when weight is on the wheels and both throttles are moved beyond approximately 80%
rpm if both throttles were below 80% for at least 60 seconds.
2.16.2.2 MASTER CAUTION Light (F/A-18F). A yellow MASTER CAUTION light, on the upper
instrument panel comes on whenever the MASTER CAUTION light in the front cockpit comes on.
The rear cockpit MASTER CAUTION light goes out whenever the front cockpit MASTER CAUTION
is reset.
2.16.2.3 Dimming and Test Functions. There are no provisions for testing the caution and advisory
displays and each DDI contains its own display dimming controls. The warning/caution/advisory lights
are dimmed by the warning/caution lights knob and are tested by the lights test switch. The following
lights can be dimmed by the warning/caution lights knob, but once in the dimmed lighting range
cannot be varied in intensity: MASTER CAUTION light, landing gear handle warning, L BAR
A1-F18EA-NFM-000
I-2-119 ORIGINAL
warning, HOOK warning, L BLEED warning, R BLEED warning, APU FIRE warning, left and right
engine FIRE warning.
2.16.3 Voice Alert System. For certain critical warnings and cautions, voice alert transmissions are
sent to the aircrew's headset. The message is repeated twice; for example, ªAPU FIRE, APU FIREº.
The voice alert requires no reset action on the pilot's part and the alert is not repeated unless the
original condition ceases for 5 seconds or more and then recurs. For cautions with voice alert, the voice
alert replaces the master caution tone; however, the master caution tone backs up the voice alert
system and provides a tone if the voice alert system malfunctions. FIRE, APU FIRE, L BLEED, and
R BLEED warning lights are not backed up by the master caution tone. Voice alert is the only audio
warning for these problems. With dual generator failure, the following voice alert warnings operate
from battery power: APU FIRE, ENGINE FIRE LEFT (RIGHT), and BLEED AIR LEFT (RIGHT).
All voice alert cautions, and the master caution tone are inoperative on battery power during dual
generator failure.
The primary radar low altitude warning (WHOOP, WHOOP), is repeated at the lowest priority until
reset or disabled by the pilot.
NOTE
With an MC1 failure, the voice alert does not sound when the aircraft
descends below the altitude set by the primary low altitude warning
setting.
CAUTION VOICE ALERT
IFF 4
FCS
FCS HOT
L (R) OVRSPD
L (R) EGT HIGH
L (R) FLAMEOUT
L (R) OIL PR
L (R) STALL
L (R) ENG
L (R) ENG VIB
FUEL LO
BINGO
MODE 4 REPLY
FLIGHT CONTROLS
FLIGHT COMPUTER HOT
ENGINE LEFT (RIGHT)
FUEL LOW
BINGO
WARNING VOICE ALERT
ALTITUDE
L (R) BLEED AIR
L (R) FIRE
APU FIRE
ALTITUDE
BLEED AIR LEFT (RIGHT)
ENGINE FIRE LEFT (RIGHT)
APU FIRE
A1-F18EA-NFM-000
I-2-120 ORIGINAL
2.16.4 GPWS - Ground Proximity Warning System. GPWS is designed to backup the pilot by
　
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本文鏈接地址：NATOPS Flight Manual 飛行手冊 1(93)