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2. The BATT switch is OFF inflight and should be placed to ON to provide essential bus backup
capability from the PMGs and battery.
3. The battery is not being recharged inflight (BATT switch ON). The battery charger has failed or
the right generator has failed with the buses isolated (R GEN and GEN TIE cautions).
4. The battery is powering the essential bus inflight. A dual generator failure and a dual PMG
failure has occurred and at least 5 to 10 minutes of battery power remains to run the FCCs.
B.2.9.1.1 LEX Vents. This section was deleted from the NATOPS. However, although physically
present on the aircraft, the LEX vents have been completely disabled in FCS logic and should be in the
full up position at all times.
B.2.9.1.1 Spoilers. The spoilers are mounted on top of the fuselage near the aft end of the LEX. The
spoilers are controlled by the FCCs and have three fixed positions: 0° (down), 13° TEU, or 60° TEU.
The spoilers are commanded to the 13° TEU position at greater than 1.5 Mach to open engine inlet
bleed air doors. The 60° TEU position is activated by the speed brake function or when more than 15°
TED stabilator is commanded (forward stick) above 22° AOA to aid in recovery from high AOA.
A1-F18EA-NFM-000
B-1 CHANGE 1
B.2.9.2 FCCs - Flight Control Computers (Aircraft 165660 and Up). These aircraft do not have
Attitude and Heading Reference Sets (AHRS).
B.2.16.4.4.2. GPWS Voice Commands. Refer to figure B2-38 for GPWS aural warning cues.
GPWS Warning
Condition Aural Cue Repetition Rate
Excessive bank angle
(MC OFP 13E)
²ROLL OUT, ROLL OUT² 2.2 seconds
ALDR or floor
altitude
(MC OFP 13E)
²POWER, POWER² for airspeed <210 KCAS and
AOB £45°
²ROLL OUT, ROLL OUT² for AOB >45°
²PULL UP, PULL UP² all other flight
conditions
2 seconds
2.2 seconds
2 seconds
Figure B2-38. GPWS Aural Cues
B.2.17.5 8 Day Clock. A standard 8 day clock is installed.
B.2.18.7.4.3 VTR 1 Selector Switch. The VTR 1 selector switch is used to select the video input
source for recording on VTR 1.
RDDI Selects right over-the-shoulder camera video.
LDDI Selects left over-the-shoulder camera video.
A1-F18EA-NFM-000
B-2 CHANGE 1
B.2.18.7.4.4 VTR 2 Selector Switch. The VTR 2 selector switch is used to select the video input
source for recording on VTR 2.
HUD Selects HUD camera video.
UFCD Selects direct video input to the UFCD.
MPCD Selects direct video input to the MPCD.
B.2.18.4.6.10 HUD Symbology. There is no energy caret.
B.2.22.5 HUD Video Record Panel (Aircraft 165660 and 165669). See figure B2-60 for HUD video
record panel applicable to aircraft 165660 and 165669.
B.7.1.3 Exterior Inspection. Verify the LEX vents are FULL UP and their condition is satisfactory.
The hydraulic reservoir gauge is located in the wheelwell and not on the aft fuselage.
B.7.1.5 Interior Checks - Pilot.
Left Console -
16. EXT LT panel - SET
a. STROBE switch - BRT or DIM
b. FORMATION knob - AS REQUIRED
c. POSITION knob - AS REQUIRED
Figure B.2-60. HMD Controls
A1-F18EA-NFM-000
B-2A (Reverse Blank) CHANGE 1

Pedestal Panel (aircraft 165533 thru 165544) -
1. ECM JETT button - NOT PUSHED IN
2. DISPENSER switch - OFF
3. ECM knob - OFF
4. DECOY switch - OFF
5. AUX REL switch - NORM
6. RWR switch - OFF
7. Clock - CHECK AND SET
8. RUD PED ADJ lever - ADJUST PEDAL POSITION
B.7.2.2 Engine Start Checks Aircraft 165533 thru 165544).
2. There is no battery gauge for aircraft.
9. MC OFP 13E commands ²ROLL OUT, ROLL OUT² while MC OFP 18E commands ²ROLL
LEFT, ROLL LEFT².
10. There is no battery gauge for aircraft.
NOTE
Slow canopy movement, EFD blanking, or uncommanded APU
shutdown is indicative of a weak battery.
B.8.2.6 Takeoff Checks.
For MAX power catapult launches only -
11. ABLIM option - BOX
NOTE
Prior to OFP 18E, the ABLIM option may be misinterpreted as a DDI
caution due to similar font size and location. There is no ABLIM
caution.
B.15.12 FCS FAILURE INDICATIONS AND EFFECTS (Aircraft 165533 thru 165544).
Figure 15-24, Spoiler Channels 1 and 4 or 2 and 3 Failure, engine bleed air may be degraded at high
Mach number with spoiler failed closed and flaps AUTO.
Figures B.15-37 thru B.15-40, and figures B.15.43 and B.15.44, are applicable to these aircraft.
A1-F18EA-NFM-000
B-3 CHANGE 1
B.23.1.1 ICS VOL Control Knobs (Aircraft 165533 thru 165544). The ICS VOL control knobs are
located on the VOL control panel on the left console in each cockpit. The knob are stacked in pairs,
　
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