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DCOY ON light also comes on during ALE-50 self
test. When self test is complete, the light goes out.
1. Refer to A1-F18EA-TAC-Series.
DISCH · Fire extinguisher bottle discharge initiated or
pressure drop detected.
GROUND
1. Do not takeoff.
DISP · ALE-47 dispense activated. 1. Refer to A1-F18EA-TAC-Series.
DPLY
· ALE-50 deployed.
When the JAMMER switch on the ECM panel is
placed to ON, the system initiates self test. The
DPLY light also comes on during ALE-50 self test.
When self test is complete, the light goes out.
1. Refer to A1-F18EA-TAC-Series.
FLAPS
(Amber)
· TEF(s) OFF, LEF(s) OFF, SPIN mode engaged,
GAIN ORIDE selected, or FLAPS HALF/FULL
over 240 KCAS (auto flap retract).
Information
FULL · FLAP switch in FULL. Information
HALF · FLAP switch in HALF. Information
L BAR
(Green)
· Launch bar extended. (Weight on the nose gear,
LAUNCH BAR switch in EXTEND, launch bar
not up (launch bar proximity switch not energized))
Information
LEFT
STEADY
· Left main landing gear down and locked.
--------------------------------------------------------------
FLASHING
· Left planing link failure detected with the
left main landing gear down and locked.
Information
--------------------------------------------------------------
1. Refer to Planing Link Failure Procedure.
LOCK/SHOOT · Radar in STT; ready to shoot. 1. Refer to A1-F18EA-TAC-Series.
A1-F18EA-NFM-000
Figure 12-1. Warning/Caution/Advisory Displays (Sheet 53 of 55)
V-12-55 CHANGE 1
Advisory Lights
INDICATOR · CAUSE / REMARKS CORRECTIVE ACTION
MASTER CAUTION · Warning or caution has been activated. 1. MASTER CAUTION light - RESET
NOSE · Nose landing gear down and locked. Information
RCDR ON
· CVRS mode switch in MAN or AUTO (in A/A or
A/G)
The light is not an indication that tape is actually
pulling.
Information
READY (APU) · APU online and ready to support engine start. Information
REC · ASPJ in receive mode. 1. Refer to A1-F18EA-TAC-Series.
RIGHT
STEADY
· Right main landing gear down and locked.
-------------------------------------------------------
FLASHING
· Right planing link failure detected with the
right main landing gear down and locked.
Information
-------------------------------------------------------
1. Refer to Planing Link Failure Procedure.
SAM · SAM threat detected. 1. Refer to A1-F18EA-TAC-Series.
SPD BRK · Speedbrake function surfaces not fully retracted. Information
STBY · ASPJ in standby mode. 1. Refer to A1-F18EA-TAC-Series.
XMT · ASPJ in transmit mode. 1. Refer to A1-F18EA-TAC-Series.
A1-F18EA-NFM-000
Figure 12-1. Warning/Caution/Advisory Displays (Sheet 54 of 55)
V-12-56 ORIGINAL
GPWS Voice Warnings
INDICATOR · CAUSE / REMARKS CORRECTIVE ACTION
CHECK GEAR
· Aircraft is <150 feet, <200 KCAS, more than 60
seconds after take-off/bolter or wave-off, descending
and landing gear is not down and locked for
0.3 seconds.
There is no visual cue.
1. Wave-off.
2. LDG GEAR handle - DN.
POWER
Approach Phase -
· Aircraft is <150 feet, <200 KCAS, more than 60
seconds after take-off/bolter or waveoff, and sink
rate ³ threshold for 0.3 seconds. (Threshold varies
linearly with a maximum sink rate of 2,040
fpm from 150 feet.)
Takeoff Phase -
· Aircraft is <150 feet, <250 KCAS, less than 60
seconds after take-off/bolter or waveoff, and a
sink rate³300 fpm for greater than 0.3 seconds.
1. Immediately add power (up to MAX may be
required) to reduce sink rate and pull up using
the direction-of-pull arrow on the HUD to
maintain 10 to 12° AOA.
Do not exceed 14° AOA (AOA tone).
PULL UP
· Aircraft is ³150 feet and MC1 calculates a dive
recovery is required.
· Aircraft is £90 feet for 0.3 seconds and airspeed
is either ³250 KCAS or or ³200 KCAS (when
more than 60 seconds after take-off/bolter or
wave-off).
1. Immediately pull-up using the direction-of-pull
arrow on the HUD.
ROLL LEFT/RIGHT
(MC OFP 18E)
· Aircraft is ³150 feet, angle of bank >45°, and
MC1 calculates a dive recovery is required. (May
be followed by PULL UP once bank angle is
£45°).
· Aircraft is <150 feet, <200 KCAS, more than 60
seconds after take-off/bolter or wave-off, and at a
　
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本文鏈接地址：NATOPS Flight Manual 飛行手冊 2(45)