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If the left and right buses are isolated because of a
detected fault, cycling the GEN TIE CONTROL
switch reenergizes the faulty bus/equipment and
may cause further damage or loss of the remaining
generator.
For first engine starts with the PARK BRK released,
the GEN TIE caution light comes on when
the first GEN comes online (battery start) or when
external electrical power is disconnected (external
power start). If an electrical fault isolated the buses
when the PARK BRK is set, the generators do not
reset following a dual outage.
GROUND
If PARK BRK released during first engine
start -
Battery Start
1. PARK BRK handle - SET
2. Operating GEN switch - CYCLE
3. Start second engine.
External Power Start
1. PARK BRK handle - SET
2. GEN TIE CONTROL switch - CYCLE
3. Start second engine.
INFLIGHT
1. GEN TIE CONTROL switch - NORM (DO
NOT CYCLE)
If both GENs operating -
2. Continue mission with ac buses isolated.
With L or R GEN caution light -
2. GEN switch affected side - CYCLE
4. Electrical RESET button - PRESS
If GEN restored -
4. Continue mission with ac buses isolated.
If GEN still failed -
4. GEN switch affected side - OFF
5. Land as soon as practical.
6. Refer to Emergency Power Distribution chart.
G-LIM 7.5G
²Flight Controls,
Flight Controls²
· Nz REF set to 7.5 g regardless of gross weight
G-limiter will not prevent an aircraft overstress at
gross weights above 42,097 lb. Above 42,097 lb gross
weight, pilot must limit g to prevent an overstress.
1. Limit intentional accelerations to the following:
GW (lb) Acceleration (g)
42,097 or less -3.0 to +7.5
45,000 -2.8 to +7.0
50,000 -2.5 to +6.3
55,000 -2.3 to +5.7
60,000 -2.1 to +5.2
66,000 -1.9 to +4.7
G-LIM OVRD
· G-limiter overridden. Selected by momentarily
pressing the paddle switch when the stick is near
the full aft limit. Maximum allowed g-limit increased
by 33% (allows a 10 g command at 7.5 g
Nz REF). Unless g-limiter override is desired,
control maximum g-level. If the paddle switch
has failed electrically, NWS and the autopilot
may be commanded off without pilot action or
notification.
1. Stick - Return to near neutral to disengage
override.
GPS DEGD
·GPS approach flight phase and EHPE exceeds
108 feet for 10 seconds.
Discontinue using GPS for approach navigation.
1. Do not execute GPS approach procedure.
A1-F18EA-NFM-000
Figure 12-1. Warning/Caution/Advisory Displays (Sheet 20 of 55)
V-12-22 ORIGINAL
DDI Cautions and Caution Lights
INDICATOR · CAUSE / REMARKS CORRECTIVE ACTION
GUN GAS
· Gun purge air pressure low.
Failure to purge cartridge combustion gases may
result in a gun bay explosion and significant aircraft
damage.
1. Do not fire gun, even if caution clears.
HAND CNTRL · Either hand controller inoperative. Information
HEAT FAIL
· Engine anti-ice failure detected while the ENG
ANTI ICE switch is ON.
· The corresponding L HEAT or R HEAT advisory
is removed on the failed side. Engine and inlet
device anti-ice capability lost on failed side.
If the ENG ANTI ICE switch is placed to OFF,
the HEAT FAIL caution is replaced by the HEAT
advisory.
1. Avoid icing conditions.
If icing conditions encountered -
2. Refer to Extreme Weather Procedures.
HOME FUEL
· FPAS calculated fuel remaining at the selected
HOME waypoint is 2,000 lb or less.
HOME FUEL caution logic is disabled with
WonW, the refueling probe extended, the landing
gear cycled down then up, or within 5 seconds after
a HOME waypoint change.
1. Change HOME waypoint (if appropriate) or
analyze configuration, fuel flow, and profile for
BINGO.
ID LT
· A failure is detected in the day ID strobe light,
interconnecting wiring, or the day ID power supply.
1. Identify aircraft type on approach to make sure
of proper arresting gear weight setting.
IFF 4
²Mode 4 reply,
Mode 4 reply²
· Transponder failed to respond to a valid mode 4
interrogation (failure or mode 4 not enabled).
· Failure in the KIT 1C.
· Mode 4 codes zeroized, or KIT 1C installed but
not keyed with crypto.
The IFF 4 caution and voice alert are disabled
with the IFF MODE 4 switch in the OFF position.
Information
IFFAI · Unable to interrogate Mode 4. Information
IFF OVRHT · IFF overheat detected. 1. IFF - OFF (if practical)
　
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本文鏈接地址：NATOPS Flight Manual 飛行手冊 2(27)