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· ROMA is not connected.
1. Verify HMD properly connected.
2. Verify QDC is properly connected and mounted
in the hip mount.
3. HMD - ALIGN
4. Verify ROMA properly connected.
A1-F18EA-NFM-000
Figure 12-1. Warning/Caution/Advisory Displays (Sheet 50 of 55)
V-12-52 CHANGE 1
DDI Advisories
INDICATOR · CAUSE / REMARKS CORRECTIVE ACTION
HOSE
With ARS control panel power switch ON:
· Drogue deployed for normal refueling (wet or
dry).
· Hose reel has failed to secure hose.
With ARS control panel power switch OFF, the
ARS DROGUE caution message is displayed.
If ARS switch ON and drogue deployed -
Information
If ARS switch ON and hose reel failed to secure
hose -
1. Hose EXT/RETR switch - CONFIRM
RETR
If drogue still does not retract -
2. Refer to ARS DROGUE caution.
HSEL · Autopilot Heading Select mode engaged. Information
LAND · GAIN switch in ORIDE with the FLAP switch in
HALF or FULL. Information
LOAD · Improper weapon load or codes or incompatible
fuzing. Refer to A1-F18EA-TAC-series.
1. SMS processor - Check for proper codes.
If LOAD remains -
2. Do not takeoff.
M4 OK
· Transponder replied to a valid Mode 4 interrogation.
IFF MODE 4 switch must be in DIS or DIS/AUD
to enable this advisory.
Information
MNTCD · AMU/maintenance card problem. Advisory is disabled
in flight.
1. Verify maintenance card installed in proper
AMU slot and AMU door is closed.
2. If indication does not clear - Abort
MSNCD · AMU/mission card problem. Advisory is disabled
in flight.
1. Verify mission card installed in proper AMU
slot and AMU door is closed.
2. If indication does not clear - Pilot discretion
MU FL · Memory Unit memory full.
Oldest stored data will be overwritten. Information
P/INS
· GPS satellite communication lost. Position keeping
has reverted from POS/AINS to POS/INS.
INS not being updated with GPS data.
Information
PCODE · GPS keys incorrect or not loaded. Information
RALT · Autopilot Radar Altitude hold mode engaged. Information
RCDR · MU turned off. Information
ROLL · Autopilot roll attitude hold mode engaged. Information
RSET · FCS RESET attempt successful. Information
RSET · FCS RESET attempt unsuccessful. FCS failure
and failure indications remain. Information
A1-F18EA-NFM-000
Figure 12-1. Warning/Caution/Advisory Displays (Sheet 51 of 55)
V-12-53 ORIGINAL
DDI Advisories
INDICATOR · CAUSE / REMARKS CORRECTIVE ACTION
SKID · Landing gear down with the ANTI SKID switch
in OFF. Information
TRIM
· Pitch, roll, and yaw trim properly set for takeoff.
(Stabilators 4° TEU, roll trim zero, RUD TRIM
knob mechanically neutral.)
Information
VVEL
· GPS assisted velocity vector enhancement disabled.
Only the air data function is being used to
smooth the velocity vector and may result in degraded
velocity vector accuracy.
With a VVEL advisory displayed, sustained climbs
and descents, such as penetration from the marshal
stack, can result in uncued (i.e., no cautions) vertical
velocity errors and a possible inaccurate velocity
vector position. Error magnitudes increase at slower
airspeeds and lower altitudes. Errors of up to 3°
(e.g., actual flightpath 3° below the displayed velocity
vector) have been observed in the landing configuration.
1. Monitor velocity vector for errors.
If errors noted -
2. Maintain level flight for 3 minutes (if practical)
Y CODE · GPS receiver is not receiving encrypted code in
secure mode.
If GPS signals are believed to be accurate -
1. HSI/DATA/(A/C) format - SELECT NOSE
GPS OPTION
If GPS signals believed to be corrupted -
2. INS knob - NAV
A1-F18EA-NFM-000
Figure 12-1. Warning/Caution/Advisory Displays (Sheet 52 of 55)
V-12-54 ORIGINAL
Advisory Lights
INDICATOR · CAUSE / REMARKS CORRECTIVE ACTION
AAA · AAA threat detected. 1. Refer to A1-F18EA-TAC-Series.
A/A · Air-to-Air master mode selected. 1. Refer to A1-F18EA-TAC-Series.
A/G · Air-to-Ground master mode selected. 1. Refer to A1-F18EA-TAC-Series.
AI · Airborne threat detected. 1. Refer to A1-F18EA-TAC-Series.
CW · Continuous wave (RF Threat) detected. 1. Refer to A1-F18EA-TAC-Series.
DCOY ON
· ALE-50 transmit enabled.
When the JAMMER switch on the ECM panel is
placed to ON, the system initiates self test. The
　
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