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feed group (approximately 1,000 pounds remaining in individual fuel feed
ww).
Indicates insufficient discharge pressure (less than 9 psi) from respective
turbine driven boost pump.
L GEN
R GEN
(caution)
Indicates that corresponding generator is inoperative because of fault in
generator, control unit, or electrical distribution system.
HYD PRESS
(caution)
HZ TAIL
AUTH
(caution)
Indicates hydraulic pressure from either engine-driven pump is less than
2,100 psi.
Indicates failure of lateral tail authority actuator to follow schedule or CADC
failure.
Figure 2-130. pilot Indicator Lights (Sheet 3 of 5)
2-257 ORIGINAL
NOMENCLATURE
R INLET
L INLET
(caution)
INLET ICE
(CautlOrl)
INTEG TRIM
(advisory)
LAD/CANOPY
(caution)
LAUNCH BAR
(advisory)
MACH TRIM
(advisory)
OBOGS
(caution)
L OIL HOT
R OIL HOT
(caution)
OIL PRESS
(caution)
READ MFD
(caution)
FUNCTION
ndicates AICS programmer and/or system failure.
ndicates ice accumulated on ice detector in left inlet with
ENG/PROBE/AICS ANTI-ICE switch in AUTO/OFF or OAIDE/ON selected.
ndicates a discrepancy between input command signal and actuator
)osition, or an electrical power loss within the computer.
idvises that the boarding ladder is not in an up and locked position or that
:anopy is not in down and locked position.
weight-on-Wheels:
l Aircraft kneeled, either throttle less than MIL, launch bar not
up and locked (normal indication until MRT checks).
Meeight-off-Wheels:
l Launch bar not up and locked.
l Launch bar not wlthin f 15” of center, cocked nosegear.
l Nose strut not fully extended.
ndicates failure of Mach trim actuator to follow schedule.
ndicates a switchover to backup oxygen or OBOGS switch OFF
ndicates oil temperature too high. May be an indication of the
righ-scavenge oil temperature: continued engine operation will result in
educed gearbox life and lubrication degradation.
ndicates left or right engine oil pressure is 11 psi or less.
ndicates any or all of the following warning/caution legends that appear on
he upper left corner of the MFD.
L N2 OSP
R N2 OSP
L Ni OSP
R Nl OSP
L TBT OT
RTBTOT
L FLMOUT
R FLMOUT
L IGV SD
R IGV SD
W/S
Figure 2-130. Pilot Indicator Lights (Sheet 4 of 5)
ORIGINAL 2-258
NAVAIR Ql-Fl4AAD-1
NOMENCLATURE
L RAMPS
R RAMPS
(caution)
PITCH STAB 1
PITCH STAB 2
(caution)
RATS
(advisory)
ROLL STAB 1
ROLL STAB 2
(caution)
RUDDER AUTH
(caution)
SAHRS
(advisory)
SPOILERS
(caution)
START VALVE
(caution)
TRANSIRECT
(advisory)
WING SWEEP
(advisory)
WSHLD HO-f
(advisory)
YAW STAB
OP (caution)
YAW STAB
OUT (caution)
FUNCTION
Indicates ramps are neither positioned in stow nor trail locks during critical
flight conditions. (See figure 2-5.)
Indicates inoperative pitch channel.
RATS operation is enabled.
Indicates inoperative roll channel (roil SAS failure).
Indicates disagreement between position and command failure of rudder
authority actuators to follow schedule, or CADC.
Indicates attiiude or heading information from SAHRS is unreliable.
Indicates spoiler failure causing a set of spoilers to be locked down.
Starter solenoid air valve open after start. Starter overspeed and/or
destruction possible.
Indicates one operable transformer-rectifier is powertng the total dc load,
or dual transformer-rectifier failure.
Indicates failure of a single channel in the system.
Indicates center windshield is overheated.
One yaw channel inoperative.
Two yaw channels inoperative (yaw SAS failure).
Figure 2-130. Pilot Indicator Lights (Sheet 5 of 5)
2-259
Figure2. -131.R IO IndicatorL ights( Sheet1 of 3)
ORIGINAL 2-260
NAVAIR 0%FlrlAAD-1
NOMENCLATURE
a
INS status indicators
@ Evis0t-y)
FUNCTION
Not operational.
Indicates mode 4 interrogation was received, but system has not
generated reply.
RCV
(advisory)
Indicates ALQ-165 is receiving a threat identification signal.
XMIT
(advisory)
Indicates ALQ-165 is transmitting.
SAM
(warning)
AAA
(warning)
Krning)
Al
(warning)
Steady illumination when a suriacs-to-air missile tracking radar is
detected. Flashing when a missile has been launched.
Steady illumination when an anti-aircraft tracking radar is detected.
　
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