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recommended.
1. Execute the FCS procedures for a Stabilator
Actuator Failure.
2. Set up for a controlled ejection.
A1-F18EA-NFM-000
Figure 12-1. Warning/Caution/Advisory Displays (Sheet 46 of 55)
V-12-48 ORIGINAL
HYD CAUTIONS
INDICATOR · CAUSE / REMARKS CORRECTIVE ACTION
HYD 1A
HYD 1B
HYD 2B
· Triple HYD circuit failure (e.g., battle damage).
Both TEFs lost (locked 5° TED).
Left aileron lost (faired and damped).
Right stabilator lost (locked 2° TEU).
Right rudder lost (faired and damped).
UA flight exhibits sluggish roll characteristics
above 15° AOA. Expect loose and sluggish response
in PA with high approach speeds due to TEF failure.
See the Hydraulic Subsystem Malfunction Guide.
CV landings not recommended since approach
speed may be in excess of 200 KCAS.
1. Execute the FLAPS OFF caution procedures
(TEF Failure).
2. Comply with steps 7, 8, and 14 of the FCS Stabilator
Actuator Failure procedure.
3. Also see remarks for FCS Stabilator and Rudder
Actuator Failures.
HYD 5000
FCES
Caution Light
· Hydraulic pressure is less than 4,600 psi when
5,000 psi operation is requested from the hydraulic
system.
Expect degraded flying qualities above 380 KCAS
and reduced departure resistance above 650 KCAS.
Uncommanded roll possible following aggressive
lateral maneuvering at greater than 4 g above 650
KCAS.
If above 650 KCAS -
1. Do not command rolling maneuvers above 4 g.
2. Full symmetric g capability still available.
HYD1 HOT
HYD2 HOT
· Hydraulic pump case temperature has exceeded
400°F and respective reservoir temperature exceeds
275°F.
May be an indication of an internal hydraulic
pump failure.
Hydraulic pump overheat may result in pump
case failure and fire in the AMAD bay.
*1. Throttle affected engine - OFF
2. Land as soon as practical.
A1-F18EA-NFM-000
Figure 12-1. Warning/Caution/Advisory Displays (Sheet 47 of 55)
V-12-49 ORIGINAL
DDI Advisories
INDICATOR · CAUSE / REMARKS CORRECTIVE ACTION
ABLIM
· Afterburner limiting function of the FADEC is
activated.
The ABLIM function is used during MAX power
catapult launches only. ABLIM limits engine power
to half afterburner with the throttles at MAX.
ABLIM is disabled with an FCC Ch 2 or 4, MC1,
FADEC, or INS failure.
Information
ALGN
· INS switched to NAV without a complete alignment.
1. INS knob - IFA or GYRO
AM DL · Radar hardware needed to support AMRAAM
data link not installed. Information
ARMAMENT
ADVISORIES · Refer to A1-F18EA-TAC-Series.
BALT · Autopilot barometric altitude hold mode engaged.
Information
BIT · Built-in test failure detected. 1. BIT format - Identify failure.
COM1H
COM2H
· ARC 210 COM1 or COM2 not loaded with Have
Quick time. Information
COM1L
COM2L
· Indicates COMM 1 or COMM 2 is reporting
failed checksum or validity fill loading error.
When selected on the MUMI format, COMM 1
boxes while the data is downloaded from the AMU
to COMM 1 and 2 and unboxes when the download
is complete.
With COMM 1 and 2 on -
1. MUMI format - SELECT COMM
COM1S
COM2S
· ARC 210 COM1 or COM2 not loaded with SINCGARS
time. Information
CDATA · Onboard unit other than MU contains classified
data. Information
CONFG
· All systems have not been checked for configuration
compatibility because one or more of the
systems is off or not communicating. Typical
poststart with RADAR knob in OFF.
Information
CPLD · Autopilot coupled to WYPT, OAP, SEQ #, or
TCN. Information
CRUIS · GAIN switch in ORIDE with FLAP switch in
AUTO. Information
D BAD · ALE-47 dispenser failure. Information
A1-F18EA-NFM-000
Figure 12-1. Warning/Caution/Advisory Displays (Sheet 48 of 55)
V-12-50 ORIGINAL
DDI Advisories
INDICATOR · CAUSE / REMARKS CORRECTIVE ACTION
D LOW · ALE-47 dispenser expendables quantity below
set BINGO level. Information
DCSCS · Indicates a failure of the COMSEC capability
has been detected. Information
DECM · IDECM suite has indicated a failure resulting in
a loss of functionality. Information
ECSDR
· ECS auxiliary duct door not in commanded position.
If the advisory is displayed above 0.4 Mach, a
door is failed open. If the advisory is displayed below
0.32 Mach, a door is failed closed. The advisory
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NATOPS Flight Manual 飞行手册 2(42)
