FOLDOUTS
TABLE OF CONTENTS
Cockpit F/A-18E/F........................................................................................................... FO-3
Rear Cockpit F/A-18F ..................................................................................................... FO-7
Electrical Bus Power........................................................................................................ FO-11
Ejection Seat .................................................................................................................... FO-13
Fuel System....................................................................................................................... FO-17
Environmental Control System ...................................................................................... FO-21
FOLDOUT SECTION
The purpose of the Foldout Section is to make these illustrations available for ready reference while
reading the associated text. The illustrations are referenced from several sections of the manual and are
referred to in the text as (see figure FO-, foldout section).
The System Foldouts are simplified to provide a general understanding of complicated systems.
They do not contain all components, circuits, etc. For a complete diagram(s) of a system, refer to the
applicable maintenance publication.
A1-F18EA-NFM-000
FO-1 (Reverse Blank) ORIGINAL
Figure FO-1. Cockpit F/A-18E/F (Sheet 1 of 2)
A1-F18EA-NFM-000
FO-3 (Reverse Blank) CHANGE 1
Figure FO-1. Cockpit F/A-18E/F (Sheet 2 of 2)
A1-F18EA-NFM-000
FO-5 (Reverse Blank) ORIGINAL
Figure FO-2. Rear Cockpit F/A-18F (Sheet 1 of 2)
A1-F18EA-NFM-000
FO-7 (Reverse Blank) CHANGE 1
Figure FO-2. Rear Cockpit F/A-18F (Sheet 2 of 2)
A1-F18EA-NFM-000
FO-9 (Reverse Blank) ORIGINAL
RIGHT 115
VOLT AC BUS
ALE-50 CONTROLLER
APPROACH LTS (AC)
ARM STA 6 THRU 11
ARS POWER
AVIONICS GROUND
BATT CHARGER
BATT HEATER
COCKPIT STROBE
LIGHT
COOLING FAN
CSC (AC)
CVRS (AC)
GPS
HARM CLC (AC)
HUD (AC)
ICE DETECTOR (AC)
INTERFERENCE
BLANKER
MC 2
POSITION LTS
R AOA HEATER (AC)
R ECS DUCT DOOR
R PITOT HEATER
R TR
R WINGFOLD EDU
RAD ALT
RDDI(s)
RECCE WINDOW DEFOG
SMS (AC)
STBY ATTITUDE
REFERENCE
INDICATORS
TACAN
TACTS (AC)
TK 1 XFR PUMP
26 VAC AUTO XFMR
RIGHT 26 VOLT
AC BUS
ADF
MAGNETIC AZIMUTH DETECTOR (CH 2 & 4)
RIGHT 28 VOLT
DC BUS
ALE-47 CONTROLLER
ALE-47 SEQUENCERS
ALE-50 CONTROLLER
ARM STA 6 THRU 11
CBN RAM AIR VALVE
COMM 2
CSC (DC)
CVRS (DC)
ECS CONTROLLER
HARM CLC (DC)
HUD (DC)
HYD 1 PRESSURE
INDICATOR
HYD 2 PRESSURE
INDICATOR
ICE DETECTOR (DC)
ICS
INTERIOR LIGHTS
LGCU
LST/CAM
NVG FLOOD LIGHTS
R AOA HEATER (DC)
R ENG FADEC CH B
R PRIMARY BLEED
AIR SHUTOFF VALVE
R PROBE HEATER
CONTROLLER
R WING UNLOCK
MOTOR
SECONDARY BLEED
AIR SHUTOFF VALVE
SMS (DC)
TACTS (DC)
UNDER COOL SENSOR
ESSENTIAL
28 VOLT
DC BUS
APU CONTROL
BK PRESS IND
BL AIR LK DET ABL
AIR LK DET B
CABIN EMERG VENT
VALVE
COMM 1
CROSSFEED VALVE
CROSS COOLING
VALVE
EMER JETT STAs
(2, 3, 4, 6, 9, 10)
EMER PROBE EXTEND
EFD
ENG START
CONTROL
FCES 1 (EBB)
FCES 2 (EBB)
FCES 3 (EBB)
FCES 4 (EBB)
FCS AV COOL
ACTUATOR
FEED TK SHUTOFF
VALVE
FIRE DET LOOP A
FIRE DET LOOP B
FIRE EXTINGUISHER
FUEL DUMP
ICS
IFF EMERG
L ENG FADEC CH A
L ENG OIL PRESSURE
INDICATOR
PITCH TRIM
R ENG FADEC CH A
R ENG OIL PRESSURE
INDICATOR
R FUEL S/O VALVE
R LG PROXIMITY
SWITCH
SMS
STBY ALTIMETER
STBY ARI (FRONT
COCKPIT ONLY)
UTILITY LIGHTS
WARNING/CAUTION
LIGHTS
LEFT 28 VOLT
DC BUS
ADF
ALE-47 SEQUENCERS
ALR-67 (DC)
ANTI-SKID CONTROL
UNIT
ANTENNA SELECT
BCN AUGMENTATOR
BUS TIE
DATA LINK
DBFSS
DFIRS POWER
DIG MAP SET (DC)
ECM COOLING
ENG IDL/A-B LKOUT
EXT FUEL TANK
CONTROL
EXT LTS CONTROL
FCCB ASYM BRK DC
FUEL LOW LEVEL
WARNING
FUEL TK PRESS
VALVES
FUEL TRANSFER
VALVES
GND PWR CONTROL
GUN
HOOK LIGHT
HOSE JETTISON
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本文链接地址：NATOPS Flight Manual 飞行手册 2(168)
