F18. FLIGHT MANUAL (2008)

A1-F18EA-NFM-000

135. If the velocity vector begins to flash slowly but is not HUD limited:

a. Selected ordnance has been released.

b. The mission computer may be displaying a degraded velocity vector

c. The waterline symbol is HUD limited

d. STBY attitude indicator is providing HUD attitude information

136. The HUD landing display (elongated horizon bar, AOA bracket, waterline symbol, steering

display) will be presented:

a. When selected through the HUD control panel

b. When selected on the right DDI

c. When gear is down and NAV master mode is selected

d. Any time that the gear is down

137. True/False: While using NAV master mode, the flight crewmember has the option to cage or

uncage the velocity vector on the HUD.

138. At what altitude will the cockpit begin to pressurize?

139. What action should be taken if FCS HOT caution light comes on in flight?

140. When the G XMT switch is placed to COMM 1 or COMM 2 the:

a. Selected radio will receive/transmit on 243.0 only

b. Selected radio will receive only 243.0

c. Selected radio will transmit only 243.0

141. The hydraulic pumps are located on the

and maintain the hydraulic pressure at

approximately

psi.

142. The HYD 2 priority valves close at approximately

psi.

143. Placing the HI mode selector switch to NORMAL displays compass rose aligned with the

aircraft:

a. Magnetic ground track

b. Magnetic heading

X-30-16

ORIGINAL

A1-F18EA-NFM-000

144. By what method are external tanks pressurized on the ground?

145. What indication does the flight crewmember have to indicate low or lost motive flow pressure?

146. Fuel is transferred from external tanks by:

a. The passing of motive flow fuel through an ejector pump which utilizes the venturi principle

to induce fuel flow.

b. Bleed air to pressurize each external tank.

c. Electrically powered boost pumps located inside each tank.

d. AMAD driven boost pumps that utilize the venturi principle to induce the flow from each tank.

147. True/False: In the F/A-18F there is no provision to raise the landing gear from the rear cockpit.

148. With a failure of hydraulic system 2A, what alternate method exists for extending the air

refueling probe?

149. Fuel dump is accomplished by:

a. Motive flow (ejector pumps)

b. Electrical pump powered by essential bus

c. AMAD driven boost pump

d. Variable displacement pumps driven by hydraulic system 2A

150. Normal brake system pressure is provided by hydraulic system

151. What optical indications of NWS failure will the flight crewmember have available besides the

MASTER CAUTION light?

152. Where is the manual canopy crank handle located inside the F/A-18 cockpit?

153. Depending on aircraft attitude and power setting, the fuel dump rate is about

pounds/minute.

154. True/False: Mechanical linkage will allow normal retraction of the nose gear even with the

launch bar extended.

155. After emergency extension of the air refueling probe, how is the probe retracted? (With loss of

2A system)

156. How many low fuel indications does the flight crewmember receive?

What are they?

X-30-17

ORIGINAL

A1-F18EA-NFM-000

157. Switching to RDR position on the HUD altitude switch will:

a. Cause radar altimeter information to be displayed at all times, until BARO is reselected.

b. Cause radar altimeter information to be displayed when at or below 5,000 feet AGL and valid.

c. Cause radar altimeter information to be displayed on the HUD while barometric altitude

continues to be displayed on the DDI.

d. Cause radar altimeter information to be displayed just below the boxed barometric altitude

display.

158. When data link information has been lost during an ACL mode 1 or 2 approach, the HUD

indication will be:

a. TILT cue

b. Break X

c. Flashing velocity vector

d. Both a and b

159. While using the A/A master mode the velocity vector on the HUD will be:

a. Caged

b. Uncaged

160. True/False: With an air-to-ground store or tank on a wing station, maximum roll rate is

automatically reduced about 33%.

X-30-18

ORIGINAL

A1-F18EA-NFM-000

APPENDIX A

SYSTEM ORGANIZATIONAL MAINTENANCE MANUALS.

System Organizational Maintenance Manuals are in the Interactive Electronic Technical Manuals

(IETM).

The IETM also references System Schematic Manuals. The following list contains the publication

numbers and titles of the System Schematic Manuals.

System Schematics

System Title

A1-F18EA

-120-500

Seat, Canopy, Survival Equipment,

and

Boarding

Ladder

-130-500

Landing Gear and Related Systems

-240-500

Secondary Power System

-270-500

Power Plant and Related Systems

-410-500

Environmental Control Systems

-420-500

Electrical System

-440-500

Lighting System

-450-500

Hydraulic System

-460-500

Fuel System

-510-500

Instrument Systems

-570-500

Integrated Flight Controls System

-580-500

Flight Incident Recorder and Monitoring System

-600-500

Communication, Navigation, and Identification

Systems

A-1

ORIGINAL

A1-F18EA-NFM-000

System Schematics

System Title

A1-F18EA

-630-500

Data Link, Instrument Landing, and Radar Beacon

Systems

-710-500

Global Positioning System

-730-500

Inertial Navigation, Backup Altitude, and Navigation

Systems

-731-500

Digital Map Set/TAMMAC Digital Map Set

-732-500

Accurate Navigation (ANAV) System

-740-500

Weapon Control System

-741-500

Mission Computer System

-742-500

Radar System

-743-500

APG-79 AESA Radar System

-744-500

Forward Looking Infrared System

-745-500

Multipurpose Display Group

-746-500

Navigation Infrared Receiving System

-750-500

Gun System

-760-500

Tactical Electronic Warfare Systems

-770-500

Video Recording and Reconnaissance Systems

-771-500

Shared Reconnaissance POD (SHARP)

A-2

ORIGINAL

A1-F18EA-NFM-000

APPENDIX B

Aircraft Differences

(LOTs 21 - 22 Aircraft)

AIRCRAFT DIFFERENCES (LOTs 21 - 22 Aircraft)

The baseline aircraft for the NATOPS manual is aircraft 165779 and up. As a result, this chapter

documents the differences from the baseline aircraft for aircraft 165533 thru 165679.

The numbering scheme for this chapter differs from that used throughout the NATOPS manual.

The ″B″ indicates the text is from this chapter, however the remaining numbers indicate the specific

paragraph in this manual affected by the difference.

B.2.1.1.1.13 ABLIM - Afterburner Limiting Function. The ABLIM function is disabled with a FCC

CH 1, 2, or 4; MC1, FADEC, or INS failure.

B.2.5.3.6 Automatic Battery Cutoff (LOT 21 Aircraft). Automatic battery cutoff occurs after 1

minute.

B.2.5.3.7 Battery Gauge (LOT 21 Aircraft). There is no cockpit indication of battery voltage. Refer to

figure B-FO-1.

B.2.5.3.8 BATT SW Caution and Caution Light (LOT 21 Aircraft). The BATT SW caution and

caution light are set to alert the aircrew of an improperly placed BATT switch, or a battery related

malfunction. After a dual GEN failure, the BATT SW caution light must be referenced to determine

whether an EBB PMG or the battery is powering the essential bus. These cautions are set in only four

circumstances.

1. The BATT switch is ON on the ground in the absence of ac power (i.e., first engine start). The

battery is depleting and the switch should be placed to OFF unless APU start is about to be made.

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.2.10.1.1 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.

B-1

ORIGINAL

A1-F18EA-NFM-000

The spoilers are commanded to the 13° TEU position at greater than Mach 1.5 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.

B.2.10.2 FCCs - Flight Control Computers (LOT 22 and up Aircraft). These aircraft do not have

Attitude and Heading Reference Sets (AHRS).

B.2.10.7.4 G-Bucket (Before FCC Software 18E-004). Due to the aerodynamic phenomenon known

as transonic pitchup, the g-limiter incorporates a g-bucket designed to prevent an aircraft over-g

during transonic deceleration. In the g-bucket, the g-limiter reduces the positive command g-limit to

a value below Nz REF. This reduction is 1.0g above 20,000 ft and 1.7g below 15,000 ft, but at no time

is the symmetrical command limit reduced below +4.5g. For instance, if Nz REF is +7.5 g (at or below

42,097 lb GW), the g-limiter only allows +5.8 g to be commanded while in the g-bucket. FSR limits are

also reduced in the g-bucket to 80% of (Nz REF minus the reduction).

The Mach numbers at which the g-bucket is entered are dependent on external stores configuration.

The g-bucket is entered at Mach 0.905 accelerating (with wing tanks or A/G stores) or at Mach 0.941

accelerating (clean or with A/A stores). Regardless of stores loading, the g-bucket is entered at Mach

1.045 decelerating and is exited at Mach 0.875 decelerating. So, if the pilot wants to have maximum-g

available during a turning maneuver (e.g., the merge), Mach in the HUD should be 0.90 or less (with

wing tanks or A/G stores) or 0.93 or less (clean or with A/A stores) to keep out of the g-bucket.

B-2

ORIGINAL

A1-F18EA-NFM-000

B.2.17.9.1 GPWS/TAWS Voice Warnings. Refer to figure B2-41.

CFIT Warning Condition

Voice Warning

Repetition Rate

″Power...Power″

for V < 210 KCAS and

AOB < 45° (gear up)

V < 175 KCAS and AOB < 45°

(gear down)

″Roll-Left...Roll-Left″

ARR

for AOB > 45°

(-1018)

seconds

Floor Altitude

″Roll-Right

Roll-Right″

for AOB < 45°

(-1018)

″Roll-Out...Roll-Out″

for AOB > 45°

(-1016)

″Pull-Up... Pull-Up″

for AOB < 45°

Excessive Take-off/Wave-off

″Power

Power″

seconds

Sink Rate

Excessive Landing Sink Rate

″Power

Power″

seconds

″Check Gear″ with gear handle

seconds

down

Gear Up Landing

″Pull-Up ...Pull-Up″ or

″Power...Power″ then

″Check

seconds

Gear″ when handle is up

Figure B2−41. CFIT Conditions, Voice Warning, and Repetition Rates

B.2.17.5 8 Day Clock. This section was deleted from NATOPS. A standard 8 day clock is installed.

B.2.19.7.4.3 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.

B.2.19.7.4.4 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.

B-3

ORIGINAL

A1-F18EA-NFM-000

MPCD

Selects direct video input to the MPCD.

B.2.19.4.6.10 HUD Symbology. There is no energy caret display in the HUD landing symbology.

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. This section was deleted from NATOPS. Verify the LEX vents are

FULL UP and their condition is satisfactory.

B.7.1.5 Interior Checks - Pilot.

Left Console -

17. EXT LT panel - SET

a. STROBE switch - BRT or DIM

b. FORMATION knob - AS REQUIRED

c. POSITION knob - AS REQUIRED

Pedestal Panel (LOT 21 Aircraft) -

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

Figure B2-60. HMD Controls

B-4

ORIGINAL

A1-F18EA-NFM-000

7. Clock - CHECK AND SET

8. RUD PED ADJ lever - ADJUST PEDAL POSITION

B.7.2.2 Engine Start Checks (LOT 21 Aircraft).

2. There is no battery gauge for aircraft.

10. MC OFP 13E commands ROLL OUT, ROLL OUT while MC OFP 18E commands ROLL

LEFT, ROLL LEFT.

11. 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 -

2. 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.11.1.3 Flaps AUTO Handling Qualities (Before OFP 18E-004).

Flight test showed the most sensitive area for over-g to be localized around 20,000 feet and

0.93 IMN

even with a nominal CG.

B.Figure 12-1. Advisory Displays. (LOTs 21 - 22 Aircraft)

Advisory Lights

INDICATOR

• CAUSE / REMARKS

CORRECTIVE ACTION

AAA

• AAA threat detected.

1. Refer to A1-F18EA-TAC-Series.

• Airborne threat detected

1. Refer to A1-F18EA-TAC-Series.

DISP

• ALE-47 dispense activated.

1. Refer to A1-F18EA-TAC-Series.

B.15.13 FCS FAILURE INDICATIONS AND EFFECTS (LOT 21 Aircraft).

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.

B-5

ORIGINAL

A1-F18EA-NFM-000

Figures B.15-37 thru B.15-40, and figures B.15.43 and B.15.44, are applicable to these aircraft.

B.23.2.1 ICS VOL Control Knobs (LOT 21 Aircraft). The ICS VOL control knobs are located on the

VOL control panel on the left console in each cockpit. The knobs are stacked in pairs, upper and lower.

Clockwise rotation increases headset volume for the controlled sub-system from the LO to the HI

position. The six knobs control the indicated sub-system and are labeled as follows:

1. TACAN morse code identification (TCN knob (upper))

2. Intercockpit and aircrew/ground crew voice (ICS knob (lower))

3. ALR-67 tones (RWR knob (upper))

4. ECM equipment (when installed) (ECM knob (lower))

5. AIM-9 seeker audio (WPN knob (upper))

6. Unused (AUX knob (lower))

The ground crew headset plug in jack and ICS volume control knob are located in door 8R on the

right side of the forward fuselage.

B.23.7 DCS - DIGITAL COMMUNICATION SYSTEM

LOT 21 Aircraft do not incorporate DCS.

Foldouts. Refer to figures B-FO-1 and B-FO-2 for specific cockpit component locations.

B-6

ORIGINAL

A1-F18EA-NFM-000

FOLDOUTS

TABLE OF CONTENTS

Cockpit F/A-18E/F (Lots 21 thru 25)

FO-3

Rear Cockpit F/A-18F (Lots 21 thru 25)

FO-7

Cockpit F/A-18E/F (Lot 26 AND UP)

FO-11

Rear Cockpit F/A-18F (Lot 26 AND UP)

FO-15

Electrical Bus Power

FO-19

Ejection Seat

FO-21

Fuel System

FO-25

Environmental Control System

FO-29

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.

FO-1 (Reverse Blank)

ORIGINAL

A1-F18EA-NFM-000

ALE-50 CONTROLLER

BATT CHARGER

CSC (AC)

ICE DETECTOR (AC)

R AOA HEATER (AC)

RDDI(s)

TACAN

APPROACH LTS (AC)

BATT HEATER

CVRS (AC)

INTERFERENCE

R ECS DUCT DOOR

RECCE WINDOW DEFOG

TACTS (AC)

RIGHT 115

ARM STA 6 THRU 11

COCKPIT STROBE

GPS

BLANKER

R PITOT HEATER

SMS (AC)

TK 1 XFR PUMP

VOLT AC BUS

ARS POWER

LIGHT

HARM CLC (AC)

JHMCS

R TR

STBY ATTITUDE

26 VAC AUTO XFMR

AVIONICS GROUND

COOLING FAN

HUD (AC)

MC2

R WINGFOLD EDU

REFERENCE

POSITION LTS

RAD ALT

INDICATORS

RIGHT 26 VOLT

ADF

MAGNETIC AZIMUTH DETECTOR (CH 2 & 4)

AC BUS

ALE-47 CONTROLLER

COMM 2

HUD (DC)

ICE DETECTOR (DC)

NVG FLOOD LIGHTS

R PROBE HEATER

SMS (DC)

ALE-47 SEQUENCERS

CPWS PRESSURE

HYD 1 PRESSURE

ICS

R AOA HEATER (DC)

CONTROLLER

TACTS (DC)

RIGHT 28 VOLT

ALE-50 CONTROLLER

SENSING

INDICATOR

INTERIOR LIGHTS

R ENG FADEC CH B

R WING UNLOCK

UNDER COOL SENSOR

DC BUS

ARM STA 6 THRU 11

CSC (DC)

HYD 2 PRESSURE

LGCU

R PRIMARY BLEED

MOTOR

CBN RAM AIR VALVE

CVRS (DC)

INDICATOR

LST/CAM

AIR SHUTOFF VALVE

SECONDARY BLEED

CK ECS CAUTION LT

ECS CONTROLLER

AIR SHUTOFF VALVE

HARM CLC (DC)

APU CONTROL

CROSSFEED VALVE

ENG START

FCS AV COOL

FUEL DUMP

R ENG FADEC CH A

SMS

BK PRESS IND

CROSS COOLING

CONTROL

ACTUATOR

ICS

R ENG OIL PRESSURE

STBY ALTIMETER

ESSENTIAL

BL AIR LK DET ABL

VALVE

FCES 1 (EBB)

FEED TK SHUTOFF

IFF EMERG

INDICATOR

STBY ARI (FRONT

28 VOLT

AIR LK DET B

EMER JETT STAs

FCES 2 (EBB)

VALVE

L ENG FADEC CH A

R FUEL S/O VALVE

COCKPIT ONLY)

CABIN EMERG VENT

(2, 3, 4, 6, 9, 10)

FCES 3 (EBB)

FIRE DET LOOP A

L ENG OIL PRESSURE

R LG PROXIMITY

UTILITY LIGHTS

DC BUS

VALVE

EMER PROBE EXTEND

FCES 4 (EBB)

FIRE DET LOOP B

INDICATOR

SWITCH

WARNING/CAUTION

CK ECS CAUTION LT

EFD

FIRE EXTINGUISHER

PITCH TRIM

LIGHTS

COMM 1

ADF

BUS TIE

EXT FUEL TANK

FUEL TRANSFER

L BLEED AIR CONT

LAUNCH BAR CONTROL

PROBE CONTROL

ALE-47 SEQUENCERS

CK ECS CAUTION LT

CONTROL

VALVES

VALVE (PRIM)

VALVE

RADAR (DC)

ALR-67 (DC)

DATA LINK

EXT LTS CONTROL

GND PWR CONTROL

L ENG FADEC CH B

LG CONTROL VALVES

SEAT ADJ (FRONT &

LEFT 28 VOLT

ANTI-SKID CONTROL

DBFSS

FCCB ASYM BRK DC

GUN

L PROBE HEATER

MEMORY UNIT (MU)

REAR)

UNIT

DFIRS POWER

FUEL LOW LEVEL

HOOK LIGHT

CONTROL

MSTR ARM

THROTTLE

DC BUS

ANTENNA SELECT

DIG MAP SET (DC)

WARNING

HOSE JETTISON

L WINGFOLD UNLOCK

NWS CONTROL VALVE

BACKDRIVE

ANAV

ECM COOLING

FUEL TK PRESS

HYD ISOL ORIDE

MOTOR

OBOGS CONTROL

WSHLD ANTI-ICE

BCN AUGMENTATOR

ENG IDL/A-B LKOUT

VALVES

ILS (DC)

REMOVAL

LEFT 115 VOLT

ALQ-165 ASPJ

EMERG AV COOLING

ILS (AC)

L PITOT HTR

LCS FAN

MC1

PROBE LT

ALR-67 (AC)

FAN

INS

L TR

LCS PUMP

MPCD(s)/UFCD(s)

RADAR (AC)

AC BUS

ARM STA 1 THRU 5

FORMATN LTS

L AOA HTRS (AC)

L WING FOLD EDU

LDDI(s)

OBOGS CONCENTRATOR

STROBE LTS

DIG MAP SET (AC)

IFF

L ECS DUCT DOOR

LDG/TAXI LT

MAINTENANCE

APU PRIM

GEN TIE LOGIC

SDC

CANOPY

INS KEEP ALIVE

SMP (CODE CHECK)

BUS

FCS KEEP ALIVE CH 1

LADDER DEPLOY

VENT TANK WET

THRU 4

LIGHT

Figure FO-5. Electrical Bus Power

FO-19 (Reverse Blank)

ORIGINAL

A1-F18EA-NFM-000

ALPHABETICAL INDEX

Page

No.

10,000 Feet Checks

III-10-24, III-10-31, III-10-34

10,000 Feet to Landing

III-10-28

10,000 Foot Checks

III-7-33

24.2.4 Navigation System BIT

VII-24-23

5-Wet (4-EFT and ARS) Loading Handling Qualities

IV-11-6

5-Wet Loading with 5-Wet FCC Gains not Set

IV-11-6

8 x 10 Display

I-2-151

8 x 10 Display Initiated BIT

I-2-199

A/A Weapon Select Switch

I-2-88

ABLIM - Afterburner Limiting Function

I-2-5

ABORT

V-14-2, V-18-3

Aborted Takeoff

III-9-1

AC Electrical Power

I-2-30

Acceleration Limitations

I-4-5

ACI Configuration Check

I-2-140

ACL Mode 1

VII-24-66

ACL MODE 1 AND 1A APPROACHES

III-8-15

ACL Mode 1A

VII-24-70

ACL Mode 2

VII-24-70

ACL MODE 2 APPROACH

III-8-18

ACL Mode Displays

VII-24-61

ACL Mode Operation

VII-24-65

ACL Option (HSI Format)

VII-24-9

Adaptability/Flexibility

IX-28-1

ADF (AUTOMATIC DIRECTION FINDER)

VII-24-51

Aerobraking Technique

III-7-40

AFCS - AUTOMATIC FLIGHT CONTROL SYSTEM

I-2-84

AFCS Mode Deselection

I-2-86

AFCS Mode Selection

I-2-84

AFCS Related Caution and Advisories

I-2-87

Aft Cooling Fan Shutoff Valve

I-2-98

Aft UFCD MUX FAIL

I-2-168

Index-1

ORIGINAL

A1-F18EA-NFM-000

Page

No.

After Landing

III-7-43

AFTER LANDING

VI-21-2

After Landing Checks

III-7-43, III-10-29

After Takeoff Checks

III-7-33, III-10-21

AFTERBURNER FAILURE

V-15-1

A/G Weapon Release Button

I-2-90

AGI (Armament Gas Ingestion) Protection

I-2-5

AHRS Failure Flying Qualities

IV-11-17

AILERON HINGE FAILURE - SUSPECTED, INBOARD

V-15-47

AIR COMBAT MANEUVERING

IV-11-7

Air Conditioning System (ACS) Pack

I-2-97

Air Data Function

I-2-72

Air Refueling Checklist

III-9-5

AIR REFUELING (RECEIVER)

III-9-5

Air Refueling Store (ARS)

III-9-9

AIR REFUELING (TANKER)

III-9-9

AIRBORNE CHECKS

III-7-33

Airborne HMD Accuracy Check with CATM/AIM-9X

III-9-23

Airborne HMD Accuracy Check with Radar

III-9-23

AIRBORNE HMD ACCURACY CHECKS

III-9-22

Aircraft (A/C) Programming

VII-24-35

Aircraft Attitude Data

I-2-215

AIRCRAFT DESCRIPTION

I-1-1

Aircraft Gross Weight

I-1-2

AIRCREW RESPONSIBILITIES BY FLIGHT PHASE

IX-28-3

Airspeed during Ejection

V-17-2

Airspeed Limitations

I-4-1

Air-to-Air Gun Tracking

IV-11-7

AJ MENU From Fixed Frequency COMM Sublevel

VII-23-13

AJ MENU From Have Quick COMM Sublevel

VII-23-20

AJ MENU From SINCGARS COMM Sublevel

VII-23-21

ALE-47 Advisories

I-2-185

ALE-47 Countermeasures Dispensing Set

I-2-185

ALE-47 DISP Switch

I-2-95

ALE-50 BIT Anomalies

I-2-185

ALE-50 Decoy Dispensing Set

I-2-185

Alert Five Launch

III-9-21

ALERT Indicators

III-9-11

ALERT SCRAMBLE LAUNCH PROCEDURES

III-9-20

Alignment Exit

I-2-214

Alignment Verification

I-2-214

All Equipment

I-2-193

ALT Selector Switch

I-2-157

Altitude Required for Recovery (ARR)

I-2-134

AMAD - Airframe Mounted Accessory Drive

I-2-27

AMAD Related Cautions

I-2-29

AMU Maintenance Format Options and Display Information

I-2-181

AMU/PC Cards Cautions and Advisories

I-2-184

Index-2

ORIGINAL

A1-F18EA-NFM-000

Page

No.

ANAV

VII-24-23

ANGLE OF ATTACK (AOA) FAILURE

V-15-44

Angle Of Attack Indexer

I-2-141

ANTI SKID Switch

I-2-53

Anti-g System

I-2-104

Anti-Jam Operation

VII-23-13

Anti-skid BIT and the ANTISKID Caution

I-2-53

Anti-skid System

I-2-51

AOA Indexer Control Knob

I-2-157

AOA Limit Display

I-4-5

AOA Limitations - Flaps AUTO

I-4-5

AOA PROBE DAMAGE OR BINDING

V-15-45

AOA PROBE SELECTION

V-15-46

AOA Probes

I-2-72

AOA Warning Tone

I-2-76

Applicable Publications

X-30-4

Approach

III-9-6, III-9-19, IX-29-5

Approach Lights

I-2-39

Approaches

VI-19-2

Approach/Landing (*)

X-30-4

APU - Auxiliary Power Unit

I-2-28

APU Fire Extinguishing System

I-2-113

APU FIRE Light

I-2-112

APU FIRE LIGHT

V-18-1

APU READY Light

I-2-28

APU Switch

I-2-28

ARC-210/DCS

VII-23-28

Area

X-30-2

Arrested Landing

III-9-19

ARRESTED LANDING AND EXIT FROM THE LANDING AREA

III-8-20

Arresting Gear Types

V-16-13

Arresting Hook System

I-2-58

ARRESTMENT - FIELD

V-16-13

Arrestment - Long Field

V-16-14

Arrestment - Short Field

V-16-14

Arrestment and Exit From the Landing Area

III-8-23

Arrestment Decision

V-16-14

ARS DROGUE Caution

III-9-12

ARS Hose Fails to Retract

V-15-25

ARS Hydraulic Pressure Light

V-15-25

ARS Interior Checks -

III-9-13

ARS Jettison

III-9-18

ARS Limitations

I-4-17

ARS Limitations

III-9-18

ARS MALFUNCTIONS

V-15-25

ARS Refueling Hose Jettison

V-15-25

ARS (Tanker) Procedures

III-9-12

Assertiveness

IX-28-1

Index-3

ORIGINAL

A1-F18EA-NFM-000

Page

No.

Asymmetric Stores Landings

III-7-43

ATC - Automatic Throttle Control

I-2-10

ATC Approach Mode Technique

III-8-14

ATC Approaches

III-7-38

ATC Automatic Disengagement

I-2-11

ATC Disengagement

I-2-11

ATC Engagement

I-2-10

ATC Related Cautions

I-2-11

ATFLIR Limitations

I-4-19

ATS Air Sources

I-2-28

ATS Protection

I-2-29

ATT Selector Switch

I-2-157

AUG PULL

I-2-29, I-2-101

AUTO BIT

I-2-196

AUTO Option (HSI Format)

VII-24-8

AUTO Sequential Steering

VII-24-44

AUTO Update

VII-24-39

Automatic Battery Cutoff

I-2-33

Automatic Carrier Landing Mode

VII-24-59

Automatic Erase

I-2-145

AUX REL Switch

I-2-129

AV COOL Switch

I-2-63, I-2-105

Avionics BIT

I-2-186

Avionics Cooling Fans

I-2-98

AVIONICS SUBSYSTEM

I-2-142

Backpad Adjustment Mechanism (SJU-17A (V)1/A, 2/A, and 9/A)

I-2-126

BACKUP ATTITUDE AND NAVIGATION SYSTEM

VII-25-2

Backup Attitude and Navigation System Controls and Indicators

VII-25-3

Backup Erase Controller

I-2-146

BACKUP FREQUENCY CONTROL

VII-25-6

Backup Heading Mode Control

VII-25-5

Backup HSI Display

VII-25-1

Backup HUD Display

VII-25-1

Backup Navigational Information on Backup HUD

VII-25-2

BAL Control Knob

I-2-157

Balanced Cruise Formation

III-9-4

BALT - Barometric Altitude Hold

I-2-86

Barometric (BARO)/Radar Low Altitude Warning Programming

VII-24-35

BARRICADE ARRESTMENT

V-16-14

Basic Autopilot

I-2-86

BATT SW Caution and Caution Light

I-2-33

BATT Switch

I-2-33

Battery

I-2-32

Battery Gauge

I-2-33

Before Engine Shutdown Checks

III-7-45, III-10-29

Before Entering Cockpit

III-7-8

Index-4

ORIGINAL

A1-F18EA-NFM-000

Page

No.

BEFORE ENTERING COCKPIT

VI-22-1

Before Landing

III-9-17

Before Takeoff

VI-19-1

Before Takeoff Checks

III-7-30

Before Taxi

III-8-21

BEFORE TAXI

VI-22-1

BEFORE TAXI CHECKS

III-7-23

Before Taxi Checks

III-8-2, III-10-15, III-10-32

BIT Initiation

I-2-190

BIT Recording On The Memory Unit

I-2-213

BIT Top Level Display

VII-23-32

BITE Flag Indicator

III-9-11

BIT-STATUS MONITORING SUBSYSTEM

I-2-186

Black Level Control Knob

I-2-156

BLEED AIR Knob

I-2-96

Bleed Air Leak Detection (BALD) System

I-2-114

Bleed Air Leak Detection System Test

I-2-114

Bleed Air Shutoff Valves

I-2-95

Bleed Air Subsystem

I-2-96

BLIN Codes

I-2-201

BLOCK NUMBERS

I-1-4

Boarding Ladder

I-2-118

Bolter

III-9-20

Boresight Reference Unit (BRU)

I-2-208

Brake Accumulator Pressure Gauge

I-2-45

BRAKE FAILURE/EMERGENCY BRAKES

V-13-4, V-18-3

Braking Technique

III-7-40

Breathing Regulator

I-2-109

Briefing

III-6-1

BRIEFING/DEBRIEFING

III-6-1

Brightness and Contrast Controls

I-2-150

Brightness Knob - AMCD Aircraft

I-2-147

Brightness Selector Knob - Non-AMCD Aircraft

I-2-147

BRK PRESS Switch

I-2-45

BRT Control Knob - Non-AMCD Aircraft

I-2-147

Built-In Test (BIT)

I-2-211

CABIN Caution Light

I-2-103

Cabin Louvers/Foot Air Outlet

I-2-102

CABIN PRESS Switch

I-2-103

Cabin Pressure Altimeter

I-2-103

Cabin Pressurization

I-2-103

Cabin Pressurization Warning System (CPWS)

I-2-103

CABIN TEMP knob

I-2-102

Cage/Uncage Button

I-2-91

CAINS and GPS

VII-24-23

CANOPY JETT Handle

I-2-118

Index-5

ORIGINAL

A1-F18EA-NFM-000

Page

No.

CANOPY JETT Handle (F/A-18F)

I-2-118

Canopy Jettison System

I-2-118

Canopy Operation

I-2-116

Canopy Switch (External)

I-2-116

CANOPY Switch (Internal)

I-2-116

Canopy System

I-2-115

CAS Operating Modes

I-2-64

Catapult Endspeed Requirements

III-8-11

Catapult Hook-Up

III-8-9, III-8-21

Catapult Launch

III-8-10, III-8-21

Catapult Launch Flyaway Characteristics

III-8-12

Catapult Suspend

III-8-11, III-8-23

Catapult Trim

III-8-3

Cautions and Advisories

I-2-190, VII-23-32

Cautions/Advisories

I-2-208

Ceiling/Visibility Requirements

II-5-3

CFIT Conditions

I-2-133

CFIT Protection Levels

I-2-132

CFIT Warnings

I-2-135

CG Limitations

I-4-1

Chaff/Flare Dispense Switch

I-2-94

Chaff/Flare/ALE-50 Dispense Switch

I-2-90

CHART Light Knob

I-2-41

Ciphered Reception

VII-23-23

Ciphered Relay Mode

VII-23-24

Ciphered Transmission

VII-23-23

Circuit Breakers

I-2-36

CK ECS Caution Light

I-2-104

CK SEAT Caution

I-2-122

CK SEAT Caution (F/A-18F)

I-2-127

Climb

III-7-33

Climb/Cruise

X-30-4

Closed Book Examination

X-30-2, X-30-3

Coarse Alignment

I-2-214

Cockpit Controls and Displays

I-2-146

Cockpit Displays Initiated BIT

I-2-196

COCKPIT SMOKE, FUMES, OR FIRE

V-15-16, V-18-4

COCKPIT TEMPERATURE HIGH

V-15-15

Cockpit Unit (CU)

I-2-208

COMM 1 and 2 Channel Knobs

I-2-170

COMM 1 and 2 Operation

VII-23-8

COMM 1 and 2 VOL (Volume) Control Knobs

VII-23-4

COMM 1 and COMM 2 Channel Select Knobs

VII-23-4

COMM 1 and COMM 2 Volume Controls

VII-23-28

COMM 1 ANT SEL (Antenna Select) Switch

VII-23-7

COMM BIT Sub-Level Display

VII-23-32

COMM Control Panel

VII-23-6

COMM Foot Pedal Switches (F/A-18F)

VII-23-7

Index-6

ORIGINAL

A1-F18EA-NFM-000

Page

No.

COMM Keypad Options and Scratchpad Display

VII-23-5

COMM Sublevel - Guard and Cue Presets

VII-23-9

COMM Sublevel - Manual Preset

VII-23-10

COMM Sublevel - Presets 1 Thru 20 (Anti-Jam)

VII-23-18

COMM Sublevel - Presets 1 Thru 20 (Fixed Frequency)

VII-23-12

COMM Sublevel - Ship Maritime Preset

VII-23-9

COMM Sublevel Selection

VII-23-8

COMM Throttle Switch

VII-23-7

COMM Touch Option/Displays

VII-23-5

COMM VOL Knobs

I-2-170

Communication

IX-28-1

COMMUNICATION-NAVIGATION-IDENTIFICATION INTERFACE

VII-23-47

COMMUNICATIONS

IX-29-1

Communications

X-30-4

CONCEPT

X-30-1

Conditionally Qualified

X-30-1

CONFIG Display

I-2-202

CONFIG Display Country ID Code

I-2-202

Configuration Check

I-2-211

CONSOLES Lighting Knob

I-2-41

CONT Control

I-2-148

Contact

III-9-7

Control Augmentation System (CAS)

I-2-65

CONTROLLABILITY CHECK

V-15-22

Controlled Flight Into Terrain (CFIT) Protection Systems

I-2-131

Countdown Time (CD)

VII-24-36

COUNTERMEASURES DISPENSING SYSTEM

I-2-185

Coupled Auto Sequential Steering

VII-24-45

Coupled Data Link Modes

I-2-87

Coupled TACAN Steering

VII-24-54

Coupled Waypoint / OAP Steering

VII-24-41

CPL - Coupled Steering Modes

I-2-87

CREW BRIEFING

IX-29-1

Critical Area/Sub-area

X-30-2

CRITICAL SKILLS OF AIRCREW COORDINATION

IX-28-1

Critique

X-30-5

Crossfeed Valve

I-2-12

Crosswind Landings

III-7-42

Crosswind Takeoff

III-7-33

CRS Select Switch

VII-24-10

CRS Set Switch

I-2-147, I-2-165

Cruise

III-7-34, IX-29-4

Cruise Check

III-7-34

Crypto Key Options

VII-23-28

CRYPTO Switch

I-2-144, VII-23-47

CURRENCY REQUIREMENTS

II-5-2

CV Alignment Modes

VII-24-12

CV MAN (Manual) Alignment

VII-24-13

Index-7

ORIGINAL

A1-F18EA-NFM-000

Page

No.

CV RECOVERY MATRIX

V-16-15

CVRS - Cockpit Video Recording System

I-2-171

CVRS Control Switches

I-2-172

CVRS Mode Switch

I-2-173

CVRS RDCR ON Light

I-2-173

CVRS Video Tape Recorders/Solid State Recorder (SSR)

I-2-172

Data Entry Using the Shifted Keypad

I-2-167, VII-24-78

DATA LINK SYSTEM

VII-24-59

DATA Option (HSI Format)

VII-24-7

Data Sources

I-2-132

Date (DATE)

VII-24-37

Day ID Light

I-2-40

Day ID Test Switch

I-2-40

DAY OPERATIONS

III-8-1

DBFS - Dry Bay Fire Suppression System

I-2-115

DC Electrical Power

I-2-32

DCS - Avionics Subsystem

VII-23-31

DCS COMSEC (Communications Security)

VII-23-28

DDI Controls

VII-23-28

DDI Formats on MPCD

I-2-151

DDI Pushbuttons

I-2-148

DDI/HUD Initiated BIT

I-2-196

DDIs

I-2-147

Debriefing

III-6-4

DEBRIEFING

IX-29-7

Decision-Making

IX-28-1

DEFINITION

IX-28-1

Definitions

X-30-1

DEFOG Handle

I-2-102

DEGRADED MODE HANDLING QUALITIES

IV-11-11

DEGRADED SYSTEMS

VI-19-2

Departure

IX-29-3

Departure Characteristics

IV-11-8

Departure from Controlled Flight

V-15-19

Departure Recovery

V-15-19

Departure Resistance

IV-11-8

Departures with Lateral Weight Asymmetries

V-15-19

Descent

VI-19-2

Descent/Penetration

III-7-35

Descent/Penetration Checks

III-7-35

DESCENT/RECOVERY

VI-21-2

Design Limit-g

I-2-69

Designation

VII-24-47

Designation (DSG) Update

VII-24-38

Designator Controller (DC)

I-2-92

Designator Controller (DC) Assignment Switch

I-2-92

Index-8

ORIGINAL

A1-F18EA-NFM-000

Page

No.

DFIRS - Deployable Flight Incident Recorder Set

I-2-186

DIGITAL COMMUNICATION SYSTEM (DCS)

VII-23-27

Digital Imaging Processor (DIP)

I-2-178

Dimming and Test Functions

I-2-130

Dimming (BRT/DIM) Switch

III-9-11

Disengagement

III-9-7

DISPENSER Switch

I-2-185

DISPLAY MALFUNCTION - AMCD AIRCRAFT

V-15-19

DISPLAY MALFUNCTION - NON-AMCD AIRCRAFT

V-15-18

DITCHING

V-17-4

D/L Option (HSI Format)

VII-24-9

DOUBLE TRANSFORMER-RECTIFIER FAILURE

V-15-10

DOWNLOCK ORIDE Button

I-2-47

Drogue Extension

III-9-15

Drogue Retraction

III-9-17

DUAL AOA FAILURE ON TAKEOFF

V-15-47

DUAL L BLEED and R BLEED WARNING LIGHTS//L/R ATS CAUTION

V-18-1

Dual Midboard with Outboard Stores Handling Qualities

IV-11-7

DUAL MISSION COMPUTER (MC) FAILURE - AMCD AIRCRAFT

V-15-19

ECS - ENVIRONMENTAL CONTROL SYSTEM

I-2-95

ECS AUTO Mode

I-2-99

ECS Auxiliary Duct Doors

I-2-97

ECS MAN Mode

I-2-100

ECS MODE Switch

I-2-101

ECS OFF/RAM Mode

I-2-100

ECS Operating Modes

I-2-99

ECS Related Warnings, Cautions, and Advisories

I-2-106

ECS RESET

I-2-105

ECS RESET and AV COOL Switch

I-2-105

EFD - Engine Fuel Display, Engine Parameters

I-2-7

EFD - Engine Fuel Display, Fuel Parameters

I-2-21

EFD Initiated BIT

I-2-199

Effects of Light

III-9-18

Effects on Vision

III-9-18

EJECTION

V-17-1

Ejection Control Handle

I-2-122

EJECTION MODE Handle (F/A-18F)

I-2-126

Ejection Procedures

V-17-4

Ejection Seat

I-2-119

Ejection Seat Restrictions

V-17-1

Ejection Seat SAFE/ARMED Handle

I-2-122

Ejection Seat System (F/A-18F)

I-2-126

Elapsed Time (ET)

VII-24-36

Electrical Fault Protection Circuitry

I-2-30

ELECTRICAL POWER SUPPLY SYSTEM

I-2-30

Electrical RESET Button

I-2-30

Index-9

ORIGINAL

A1-F18EA-NFM-000

Page

No.

Electrical System Cautions and Caution Lights

I-2-36

Electronic Attitude Display Indicator (EADI)

I-2-149

Electronic Unit Failure

I-2-218

Electronics Unit (EU)

I-2-208

EMCON - Emission Control Pushbutton

VII-23-6

EMCON Pushbutton

I-2-171

EMERG BRK Handle (Front Cockpit)

I-2-55

EMERG BRK Handle (Rear Cockpit Lots 21 thru 25)

I-2-55

EMERG JETT Button

I-2-128

EMERG LDG GEAR Handle (F/A-18F)

I-2-48

EMERGENCIES

IX-28-4

Emergencies

IX-29-7

Emergency

X-30-2

Emergency Braking

I-2-54

EMERGENCY CATAPULT FLYAWAY

V-14-1, V-18-3

EMERGENCY EGRESS

V-13-3

EMERGENCY EQUIPMENT

I-2-127

Emergency Fuel Transfer

III-9-16

Emergency High Gain NWS

I-2-50

Emergency Instrument Lights

I-2-41

Emergency Jettison

I-2-127

Emergency Landing Gear Extension

I-2-47

Emergency Oxygen

I-2-110

EMERGENCY TANKER DISENGAGEMENT

V-15-26

Emergency/Malfunction Procedures (*)

X-30-4

Emission Control Button

VII-23-46

ENG ANTI ICE Switch

I-2-6

ENG CRANK Switch

I-2-6, I-2-29

ENG Display

I-2-9

Engine Anti Ice

I-2-5

Engine Anti-Ice Advisories

I-2-6

Engine Anti-Ice Related Cautions and Advisories

I-2-6

ENGINE CAUTIONS

V-18-2

Engine Controls and Displays

I-2-6

ENGINE FAILS TO START/HUNG START

V-13-1

Engine Feed System

I-2-12

Engine Functional Checks

III-10-1

Engine Idle Schedules

I-2-3

Engine Instrument Light

I-2-42

Engine Operation Limitations

I-4-1

Engine Related Cautions and Advisories

I-2-5

Engine Shutdown Checks

III-7-46, III-10-30

ENGINE START

III-7-18

Engine Start

III-8-2

ENGINE START

VI-22-1

Engine Start Checks

III-7-19, III-10-6

Engine Status

I-2-2

Engine Vibration Limitations

I-4-1

Index-10

ORIGINAL

A1-F18EA-NFM-000

Page

No.

Engine/AMAD Fire Extinguishing System

I-2-113

Engines

I-2-1

Enroute

IX-28-3

ENTRANCE/EGRESS SYSTEMS

I-2-115

Equipment Groups

I-2-193

Equipment Status Displays

I-2-188, I-2-201

Erase and Hold Data

I-2-144

Exceeding 360° Roll Limit

IV-11-9

Exceeding Asymmetric Loading AOA Limits

IV-11-9

Excessive Landing Sink Rate

I-2-134

Excessive Take-off Sink Rate

I-2-134

Excessive Wave - off Sink Rate

I-2-134

EXT TANKS Transfer Switches

I-2-16

Exterior Inspection

III-7-2

EXTERIOR INSPECTION

VI-22-1

Exterior Lighting

I-2-36

Exterior Lights Master Switch

I-2-36

External Electrical Power

I-2-34

External Fuel Transfer

I-2-15

External Power Switch

I-2-34

EXTERNAL STORES JETTISON

V-15-23

EXTERNAL STORES LIMITATIONS

I-4-13

F/A-18F

I-1-2

Factors That Degrade Aircrew Coordination

IX-28-2

FADEC - Full Authority Digital Engine Control

I-2-1

FADEC Power Sources

I-2-1

FADEC Reset

I-2-3

FADEC/Engine Degrades

I-2-2

Fan Speed Lockup

I-2-4

Fast Data Entry

I-2-167, VII-24-78

Fast Tactical Imaging Set (FTI-II)

I-2-178

FCC Electrical Redundancy

I-2-33

FCC Temperature Monitoring

I-2-63

FCCs - Flight Control Computers

I-2-61

FCES Caution Light

I-2-79

FCF CHECKLIST - PROFILE A

III-10-4

FCF CHECKLIST - PROFILE C

III-10-31

FCF CHECKLIST - PROFILE D (REAR COCKPIT)

III-10-32

FCF CHECKLIST - PROFILE E

III-10-33

FCF PROCEDURES

III-10-2

FCF QUALIFICATIONS

III-10-2

FCF REQUIREMENTS

III-10-2

FCS - FLIGHT CONTROL SYSTEM

I-2-60

FCS BIT Consent Switch

I-2-81

FCS Exerciser Mode

I-2-80, I-2-195

FCS FAILURE INDICATIONS AND EFFECTS

V-15-27

Index-11

ORIGINAL

A1-F18EA-NFM-000

Page

No.

FCS Failures

I-2-79

FCS Initiated BIT (IBIT)

I-2-193

FCS Redundancy and Survivability

I-2-63

FCS Related Cautions

I-2-81

FCS RESET Button

I-2-80

FCS Status Display

I-2-82

Feed Shutoff Valves

I-2-12

Feed Tank Balancing

I-2-13

Feed Tank Imbalance with One Engine at Idle

I-2-13

Feed Tanks

I-2-12

Final Approach

III-7-38

Final Grade Determination

X-30-5

Fine Alignment

I-2-214

FIRAMS - Flight Incident Recorder and Aircraft Monitoring Set

I-2-186

FIRE DETECTION, FIRE EXTINGUISHING, AND BLEED AIR LEAK DETECTION

SYSTEMS

I-2-111

FIRE Detection System Test

I-2-113

FIRE EXTGH READY/DISCH Light

I-2-112

FIRE LIGHT

V-18-2

FIRE Lights

I-2-111

FIRE Test Switch

I-2-115

FIRE Warning Lights (F/A-18F)

I-2-112

FIRE Warning Voice Alerts

I-2-112

Flap Position Lights

I-2-64

Flap Scheduling

I-2-66

FLAP Switch

I-2-64

Flaps AUTO

IV-11-11

Flaps AUTO Handling Qualities

IV-11-2

Flaps HALF or FULL

IV-11-11

Flight Codes

III-6-1

Flight Control Mode Effects on Handling Qualities

IV-11-1

Flight Control Surfaces

I-2-61

Flight Control System Functional Checks

III-10-1

Flight Controls

I-2-73

FLIGHT EVALUATION

X-30-3

Flight Evaluation Grade Determination

X-30-5

Flight Evaluation Grading Criteria

X-30-5

FLIGHT MEMBER POSITIONS

IX-28-2

FLIGHT PHASES

IX-29-2

Flight Preparation

III-9-19

FLIR, ATFLIR, NAV Pod Restrictions with 480 Gallon Centerline

I-4-19

FLIR Carriage Handling Qualities

IV-11-5

FLOOD Lights Knob

I-2-41

Floor Altitude

I-2-134

FOLLOW-ON TRAINING

II-5-1

FORCED LANDING

V-16-4

FORMATION FLIGHT

III-9-1

Formation Flights

IX-28-4

Index-12

ORIGINAL

A1-F18EA-NFM-000

Page

No.

Formation Leader

IX-28-2

Formation Lights

I-2-39

FORMATION Lights Knob

I-2-39

Formation Taxi/Takeoff

III-9-1

FPAH - Flight Path Angle Hold

I-2-86

FPAH/ROLL - ATC Approach Technique (field only)

III-7-39

FPAH/ROLL - ATC Approaches

III-7-39

FPAS - FLIGHT PERFORMANCE ADVISORY SYSTEM

I-2-24

FPAS CLIMB Option

I-2-25

FPAS CURRENT RANGE and ENDURANCE

I-2-24

FPAS Default Area

I-2-25

FPAS Display

I-2-24

FPAS Fuel Flow

I-2-25

FPAS HOME FUEL Caution

I-2-25

FPAS HOME Waypoint Selection

I-2-25

FPAS OPTIMUM RANGE and ENDURANCE

I-2-25

FPAS Waypoint/Tacan Steering and the HSI Display

I-2-24

F-QTY Advisory

I-2-22

FTI-II Major Components

I-2-178

FUEL Display

I-2-21

Fuel DUMP Switch

I-2-19

Fuel Dump System

I-2-18

Fuel Low Level Indicating System

I-2-23

Fuel Quantity Indicating System

I-2-19

FUEL SYSTEM

I-2-11

Fuel System Related Cautions

I-2-24

Fuel Tank Pressurization and Vent

I-2-16

Fuel Transfer

III-9-15

Fuel Transfer - Internal Wing Tanks

I-2-14

Fuel Transfer - Tanks 1 and 4

I-2-13

Fuel Transfer Schedule/CG Control

I-2-14

Fuel Transfer System

I-2-13

Fuel/Air Heat Exchanger

I-2-18

Fuel/Air Heat Exchanger Leak Detection

I-2-18

Full Stop Landings

III-7-39

Full-Crab-to-Touchdown Technique

III-7-42

Functional Check Flights

IX-29-7

Functional Checkflights

IX-28-4

FUSELAGE FUEL LEAK

V-15-4

G XMIT (Guard Transmit) Switch

VII-23-7

GAIN Control - AMCD Aircraft

I-2-147

GAIN ORIDE

I-2-78, IV-11-16

GAIN Switch

I-2-79

G-Bucket

I-2-70

Gear-Up Landing

I-2-135

GEN Switches

I-2-30

Index-13

ORIGINAL

A1-F18EA-NFM-000

Page

No.

GEN TIE Caution Light

I-2-32

GEN TIE Switch

I-2-32

General

III-6-1

GENERAL

III-8-1

General

III-8-21

GENERAL

III-10-1

General

X-30-2

Glideslope

III-8-14

G-Limiter

I-2-69

G-Limiter Considerations

I-2-69

G-Limiter Override

I-2-72

Global Positioning System (GPS)

VII-24-11

GO AROUND

V-14-3

GPS Page

VII-24-24

GPS Waypoint Programming

VII-24-26

Grab Handle Chaff/Flare Dispense Switches (Rear Cockpit LOT 26 and up)

I-2-95

Grab Handle Chaff/Flare Dispense Switches (Rear Cockpit LOTs 21 thru 25)

I-2-95

Grading Instructions

X-30-2

Gross Weight and Lateral Weight Asymmetry Limitations

I-4-3

GROUND EVALUATION

X-30-2

GROUND FIRE

V-13-2

Ground (GND) Alignment

VII-24-14

Ground Operation

VI-20-1

GROUND OPERATIONS

VI-21-1

Ground Power Switches

I-2-35

Ground Proximity Warning System

I-2-215

Groundspeed Cuing

VII-24-45

Groundspeed Programming

VII-24-29

GSEL - Ground Track Select

I-2-87

GTRK - Ground Track Hold

I-2-86

Guard Transmit on Top Level CNI Format

VII-23-23

Guidelines for Effective Communications

IX-29-2

Gyro Recovery

VII-24-23

Half-Crab Kickout Technique

III-7-42

Hand Controllers (Missionized Rear Cockpit Lots 21 thru 25)

I-2-91

Hand Controllers (Rear Cockpit LOT 26 AND UP)

I-2-95

HANDLING QUALITIES

IV-11-1

Handling Qualities with Flaps HALF or FULL

IV-11-1

Hangar Deck Operation

III-8-1

Have Quick Menu From AJ Menu Fixed Frequency COMM Sublevel

VII-23-14

HAVE QUICK SYSTEM

VII-23-14

HDG - Heading Hold

I-2-87

HDG/TK Set Switch

I-2-147, I-2-165

Heavy Gross Weight Braking Technique

III-7-41

Heavy Gross Weight Landings

III-7-41

Helmet Display Unit (HDU)

I-2-205

Index-14

ORIGINAL

A1-F18EA-NFM-000

Page

No.

Helmet Mounted Display (HMD)/Aft Helmet Mounted Display (AHMD)

I-2-205

Helmet Not Installed

I-2-221

Helmet Tracker Failure

I-2-221

Helmet-Vehicle Interface (HVI) Connectors

I-2-205

High Altitude (above 30,000 feet)

III-10-27

High Altitude Ejection

V-17-4

HMD Alignment

III-9-22

HMD/AHMD OFF/BRT Knobs

I-2-208

HMD/AHMD Symbology

I-2-214

Holding

VI-19-2

HOOK BYPASS Switch

I-2-40

HOOK Handle

I-2-58

HOOK Light

I-2-58

HOSE CUT/SAFE Switch

III-9-11

HOSE Switch

III-9-12

HOT BRAKES

V-13-5

HOT BRAKES/BRAKE FIRE

V-13-2

Hot Refueling

III-7-45

HOT SEAT PROCEDURE

III-9-20

HOT START

V-13-1, V-18-3

HSEL - Heading Select

I-2-87

HSI Display

VII-25-5

HSI Display Symbology

I-2-153

HSI Format

VII-24-2

HSI Format on a DDI

VII-24-9

HSI Option

VII-24-2

HSI-DATA-A/C Controls

I-2-138

HUD - Head-Up Display

I-2-156

HUD - Navigation Information

VII-24-9

HUD ACL Display

VII-24-64

HUD Advisory Data Symbology

I-2-165

HUD BIT Checks

I-2-165

HUD Camera

I-2-172

HUD Camera BIT Button

I-2-172

HUD Event Marker

I-2-172

HUD Symbology

I-2-157

HUD Symbology Brightness Selector Switch

I-2-156

HUD Symbology BRT Control Knob

I-2-156

HUD Symbology Degrades

I-2-162

HUD Symbology Not Replicated on the HMD

I-2-214

HUD Symbology Reject Switch

I-2-156

HUD Symbology Replicated on the HMD

I-2-214

HUD Video Control Switch

I-2-157

HUD Video Record Panel

I-2-208

HYD ISOL Switch

I-2-46

HYD1 (2) HOT CAUTION

V-18-2

Hydraulic Accumulators

I-2-45

HYDRAULIC FAILURES

V-15-5

Index-15

ORIGINAL

A1-F18EA-NFM-000

Page

No.

Hydraulic Isolation Valves

I-2-45

HYDRAULIC POWER SUPPLY SYSTEM

I-2-42

Hydraulic Pressure Gauge

I-2-44

Hydraulic Pumps

I-2-44

Hydraulic Reservoirs

I-2-44

Hydraulic System

I-2-42

Hydraulic System Related Cautions and Caution Light

I-2-46

Hydro-mechanical (HYDRO MECH) Initiated BIT

I-2-201

HYPOXIA/LOW MASK FLOW/NO MASK FLOW

V-15-17

IBU (Increased Bleed Usage) Signal

I-2-5

ICE AND RAIN

VI-20-1

ICLS BIT

VII-24-58

ICLS Decoder

VII-24-58

ICLS Initialization

VII-24-58

ICLS Receiver

VII-24-54

ICLS Steering

VII-24-59

ICS - INTERCOM SYSTEM

VII-23-1

ICS Aft Cockpit Kick Switches (F/A-18F Lot 26 and up)

VII-23-2

ICS Function Selector Switch Aft Cockpit (F/A-18F)

VII-23-2

ICS Function Selector Switch (F/A-18F)

VII-23-2

ICS Function Selector Switch Front Cockpit (F/A-18F)

VII-23-2

ID (IDENT) Pushbutton

I-2-170

IDENT (ID) Button

VII-23-46

IDENT Knob

I-2-38

IDENTIFICATION FRIEND OR FOE (IFF)/COMBINED INTERROGATOR TRANSPONDER

(CIT)

VII-23-32

IFA (APG-73)

VII-24-18

IFA (APG-79)

VII-24-22

IFF Antenna Select Switch

VII-23-47

IFF BIT

VII-23-43

IFF Control Panel

VII-23-46, VII-24-10

IFF Controls

VII-23-46

IFF Interrogator

VII-23-43

IFF on Top Level CNI UFCD Format

VII-23-35

IFF PROG EDIT Sublevel

VII-23-44

IFF Programming (IFF PROG) Page

VII-23-43

IFF Related Cautions and Advisories

VII-23-47

IFF Transponder

VII-23-32

IFF Transponder UFCD Sublevel

VII-23-35

Ignition System

I-2-3

ILS Channel Thumbwheels

VII-24-10

ILS Option (HSI Format)

VII-24-9

ILS UFC/MAN Switch

VII-24-10

Immediate Action Items

V-12-1

Implementation

X-30-1

In Maintenance Control

III-7-1

Index-16

ORIGINAL

A1-F18EA-NFM-000

Page

No.

Individual Units

I-2-193

Inertial Navigation (NAV) Mode

VII-24-11

Inertial Navigation System (INS)

VII-24-11

INERTIAL NAVIGATION SYSTEM (INS)/GLOBAL POSITIONING SYSTEM (GPS) . VII-24-10

Inflight

VI-19-1

INFLIGHT

VI-21-1

In-Flight Alignment (IFA)

VII-24-17

Inflight Refueling

IX-29-4

INITIAL QUALIFICATION

II-5-1

Initialization

VII-24-65

Initiated BIT (IBIT)

I-2-211

Injury Risks - Nude Weight Greater than 213 Pounds (245 Pounds for SJU-17A)

V-17-2

Injury Risks - Nude Weight Less than 136 Pounds

V-17-1

INS Initiated BIT

I-2-195

INS Knob

VII-24-25

INS Mode Select Knob

VII-24-9

INS Terminal Data

I-2-203

INS Updates (not available in AINS)

VII-24-50

INS/GPS Related Cautions and Advisories

VII-24-25

Inspection of RCS Reduction Features

III-7-1

INST PNL Lighting Knob

I-2-41

INSTRUMENT CARRIER LANDING SYSTEM (ICLS)

VII-24-54

Instrument Evaluation Flights

II-5-2

INSTRUMENT FLIGHT

VI-19-1

Instrument Qualification

II-5-2

INSTRUMENTS

I-2-140

Intercockpit Communications (F/A-18F)

III-7-19

Interconnect Valve

I-2-12

INTERIOR CHECK

VI-22-1

Interior Checks - Pilot

III-7-11

Interior Checks - WSO

III-7-16

Interior Lighting

I-2-40

Interior Lighting (F/A-18F)

I-2-42

INTR WING Control Switch

I-2-15

Intra-Cockpit Communications (ICS)

IX-29-1

JAMMER Switch

I-2-185

JETT STATION SELECT Buttons

I-2-128

Jettison Systems

I-2-127

JHMCS Alignment

I-2-213

JOINT HELMET MOUNTED CUEING SYSTEM (JHMCS)

I-2-205

KC-10 Refueling Operations

III-9-7

KC-135 BDA Refueling

III-9-8

KC-135 MPRS Refueling

III-9-9

Index-17

ORIGINAL

A1-F18EA-NFM-000

Page

No.

KC-135 Refueling Operations

III-9-8

KY-58 - SECURE SPEECH SYSTEM

VII-23-23

KY-58 Cipher Mode

VII-23-26

KY-58 Control Panel Assembly

VII-23-23

KY-58 Controls and Indicators

VII-23-25

KY-58 Fill Select Knob

VII-23-25

KY-58 Mode Select Knob

VII-23-25

KY-58 Operation

VII-23-25

KY-58 Power Knob

VII-23-25

KY-58 Relay Mode

VII-23-26

KY-58 Volume Control Knob

VII-23-25

L BAR Warning/Advisory Lights

I-2-57

L or R BLD OFF Cautions

I-2-96

Ladder Remote Release Button (After AFC 366)

I-2-119

Ladder Remote Release Switch (Before AFC 366)

I-2-119

Landing

IX-29-6

Landing Aid Symbology

I-2-215

LANDING CHECKS

III-7-35

Landing Checks

III-7-36, III-10-28

Landing Gear Control Unit (LGCU)

I-2-48

LANDING GEAR EMERGENCY EXTENSION

V-16-5

LANDING GEAR FAILS TO RETRACT

V-14-5

Landing Gear Functional Checks

III-10-2

Landing Gear Position Lights

I-2-49

Landing Gear Position Lights (F/A-18F)

I-2-49

Landing Gear System

I-2-46

Landing Gear UNSAFE Light (F/A-18F)

I-2-49

LANDING GEAR UNSAFE/FAILS TO EXTEND

V-16-4

Landing Gear Warning Light and Warning Tone

I-2-48

Landing in Heavy Rain

VI-20-3

Landing Pattern

III-8-12, III-9-19

Landing/Taxi Light

I-2-40

Lateral Weight Asymmetry Calculations

I-4-3

Latitude/Longitude Display/Entry

VII-24-35

LAUNCH BAR Switch

I-2-57

Launch Bar System

I-2-56

LB Circuit Breaker

I-2-57

LCS - Liquid Cooling System

I-2-105

LDG GEAR Handle

I-2-47

LDG/TAXI Light Switch

I-2-40

Leadership

IX-28-1

Leading Edge Flap Asymmetry

IV-11-12

LEF Failure Landing Handling Qualities (Symmetric or Asymmetric)

IV-11-12

Leg Restraint Snubber Release Tabs

I-2-123

Leg Restraint System

I-2-122

LIGHTING

I-2-36

Index-18

ORIGINAL

A1-F18EA-NFM-000

Page

No.

LIMITATIONS OF THE BASIC AIRCRAFT

I-4-1

Limitations with Flaps HALF or FULL

I-4-9

Local Time Of Day Programming (LTOD)

VII-24-37

LOSS OF CABIN PRESSURIZATION

V-15-18

LOSS OF DC ESSENTIAL BUS

V-13-1

LOSS OF DIRECTIONAL CONTROL DURING TAKEOFF OR LANDING (BLOWN TIRE,

NWS FAILURE)

V-14-4

LOSS OF DIRECTIONAL CONTROL DURING TAKEOFF OR LANDING/ PLANING LINK

FAILURE

V-18-3

Low Altitude Ejection

V-17-3

Low Altitude Warning Tone

I-2-170

L/R FUEL INLT CAUTION

V-18-2

LT TEST Switch

I-2-42

Magnetic Azimuth Detector

VII-25-3

Magnetic Transmitter Unit (MTU)

I-2-208

Main Wheel Anti-Spin

I-2-56

Malfunction

X-30-2

Maneuvering Outside of NATOPS Limits

IV-11-9

Maneuvering with Flight Control System Failures

IV-11-10

Maneuvering within NATOPS Limits

IV-11-8

Manual Canopy Actuation Fitting (External)

I-2-118

Manual Canopy Handcrank (Internal)

I-2-118

Manual Erase

I-2-145

Manual Override Handle

I-2-125

Map Data

VII-24-6

Map Loading Format Options

I-2-181

Map Loading Format Status Information

I-2-182

Map Loading Interruptions

I-2-183

MAP Modes/Data Products

VII-24-6

MAP Operating Mode Option

VII-24-2

MAP Option (HSI Option)

VII-24-1

Map Orientation Option

VII-24-6

Map Theater Data Loading

I-2-181

MAP Update

VII-24-39

MASTER CAUTION Light

I-2-129

MASTER CAUTION Light (F/A-18F)

I-2-130

Master Modes

I-2-146

MASTER Switch

VII-23-46

MC CONFIG Caution

I-2-202

MC Switch

I-2-143

Medium Altitude Checks (above 10,000 feet)

III-10-22, III-10-33

Meet The Super Hornet

I-1-1

MENU Formats

I-2-148

MENU Option (HSI Format)

VII-24-9

Minimum Flight Training Requirements

II-5-1

Minimum Ground Training Requirements

II-5-1

Index-19

ORIGINAL

A1-F18EA-NFM-000

Page

No.

Missed Approach

III-9-7

Mission Analysis

IX-28-2

Mission Commander

IX-28-2

Mission Computer Failure

I-2-218

MISSION COMPUTER FAILURE

VII-25-1

Mission Computer Failure (AMCD Aircraft)

VII-25-1

Mission Computer Failure (AMCD Aircraft) - Dual

VII-25-1

Mission Computer Failure (AMCD Aircraft) - Single

VII-25-1

Mission Computer Failure (Non-AMCD Aircraft)

VII-25-1

Mission Computer System

I-2-142, VII-23-31

Mission Critique

IX-28-4

Mission Data Entry

I-2-143

Mission Evaluation

X-30-4

Mission Initialization

I-2-143, VII-23-32

MISSION PLANNING

III-6-1

Mission Planning and Briefing

IX-28-3

Mission Planning/Briefing

X-30-3

MK Option (HSI Format)

VII-24-7

MODE 4 Switch

VII-23-47

MODE Backup

VII-24-2

MODE Option (HSI Format)

VII-24-2

Mode S

VII-23-35

MODE Switch

I-2-40

Motive Flow/Boost Pumps

I-2-12

Moving Map - Digital Map Set (DMS)

VII-24-1

Moving Map Range Scales

VII-24-1

MPCD - Multipurpose Color Display

I-2-150

MPCD Formats

I-2-151

MPCD Initiated BIT

I-2-199

MPCD (or 8 x 10 Display)

VII-25-3

MULTIFUNCTION INFORMATION DISTRIBUTION SYSTEM (MIDS)

VII-23-1

Multi-Function Switch (MFS)

I-2-92

Multipurpose Display Group

I-2-146

MUMI - Memory Unit Mission Initialization Format

I-2-143

NAMT Systems Check

X-30-2

NATOPS Admin Briefing Guide

III-6-1

NATOPS Evaluation

X-30-1

NATOPS Evaluation Question Bank

X-30-5

NATOPS EVALUATION QUESTION BANK

X-30-6

NATOPS Reevaluation

X-30-1

NATOPS Tactical Admin Briefing Guide

III-6-4

NAV Master Mode TDC Priority

I-2-215

NAVCK Display

VII-24-23

NAVIGATION BACKUP

VII-25-4

NAVIGATION CONTROLS AND INDICATORS

VII-24-1

Navigation Controls and Indicators

VII-25-5

Index-20

ORIGINAL

A1-F18EA-NFM-000

Page

No.

NAVIGATION DATA ENTRY

VII-24-70

Navigation Master Mode

I-2-215

NAV/TAC Bank Limit Options

VII-24-39

Night Landings

III-8-23

NIGHT OPERATIONS

III-8-21

NIGHT VISION DEVICE (NVD) OPERATIONS

III-9-18

No RDY Light

V-15-26

Non-Avionic BIT

I-2-201

Non-BIT Status

I-2-202

Non-Precision

VI-19-2

Normal Braking

I-2-51

Normal Landing Gear Extension and Retraction

I-2-47

Normal Takeoff

III-7-32

Nosewheel Steering System (NWS)

I-2-49

NWS Button

I-2-75

NWS Engagement/Disengagement

I-2-50

Object/Target Detection

III-9-19

OBOGS Control Switch

I-2-110

OBOGS DEGD Caution

I-2-108

OBOGS DEGD CAUTION//HYPOXIA/LOW MASK FLOW/NO MASK FLOW//LOSS OF

CABIN PRESSURIZATION/CABIN CAUTION LIGHT BELOW 47,000 FEET

V-18-2

OBOGS Monitor

I-2-107

OCF RECOVERY

V-18-4

OCF Recovery Procedures

V-15-20

OFT/WST Procedures Evaluation

X-30-2

Oil Pressure Sensing System

I-2-3

On Board Oxygen Generating System (OBOGS)

I-2-107

Open Book Examination

X-30-2, X-30-3

OPERATING LIMITATIONS (LOT 21)

I-4-19

Operation

VII-23-28

Oral Examination

X-30-2

Oral Examination and OFT Procedure Check (If Conducted)

X-30-3

OUT-OF-CONTROL FLIGHT (OCF)

IV-11-8, V-15-19

Over the Shoulder Camera BIT Buttons (LOTs 21−24)

I-2-172

Over the Shoulder Cameras (LOTs 21−24)

I-2-172

Overfly Designation

VII-24-47

Overheat Condition

I-2-213

Over-the-Top Maneuvering

IV-11-8

OVRD Button

I-2-203

OXY FLOW Knob

I-2-110

OXYGEN SYSTEMS

I-2-107

Paddle Switch

I-2-75

Parade

III-9-1

Index-21

ORIGINAL

A1-F18EA-NFM-000

Page

No.

PARK BRK Handle

I-2-56

Parking Brake System

I-2-56

Pattern Adjustments

III-7-38

Pattern Strobe Lights

I-2-38

PERSONAL FLYING EQUIPMENT

II-5-4

PHILOSOPHY

IX-29-1

Pilot In Command

IX-28-2

Pitch and Roll Trim Switch

I-2-74

Pitch CAS

I-2-65

Pitch-Axis Pilot Relief Modes

I-2-86

PITOT ANTI ICE Switch

I-2-73

Pitot-Static/Total Temperature Probes

I-2-72

Plane Captain Brief

III-10-4

PLANING LINK FAILURE

V-16-12

Planing Links

I-2-46

PMG - Permanent Magnet Generator

I-2-32

POS Data

VII-23-46

POS Option Display

VII-25-5

Position Keeping

VII-24-37

Position Lights

I-2-38

POSITION Lights Knob

I-2-39

Position Updating

VII-24-38

Post Departure Dive Recovery

V-15-21

Post Flight

IX-29-7

Post Flight Procedures

X-30-4

POST-FLIGHT CHECKS

III-7-43

Post-flight Update

VII-24-39

Post-Start Checks

III-10-7

POS/XXX Option (HSI Format)

VII-24-6

POWER PLANT SYSTEMS

I-2-1

Power Switch (PWR)

III-9-10

Precision Approaches

VI-19-2

Preflight

III-8-21

PRE-FLIGHT

IX-29-2

PREFLIGHT CHECKS

III-7-1

Preflight Checks

III-8-1, III-10-4, III-10-32

Preflight FCS Initiated BIT

I-2-194

Preflight FCS Initiated BIT Operation

I-2-194

Preflight FCS Initiated BIT PASS/FAIL

I-2-194

Preflight/Line Operations

X-30-3

Pre-Start Checks

III-10-5

Pretakeoff

IX-28-3

Primary Heat Exchanger

I-2-97

PROBE Switch

I-2-18

Prohibited Maneuvers

I-4-9

Prohibited Maneuvers

I-4-19

Index-22

ORIGINAL

A1-F18EA-NFM-000

Page

No.

Qualified

X-30-1

Radar Altimeter Initiated BIT

I-2-200

Radar Cross Section (RCS) Reduction

I-1-3

Radar Elevation Control

I-2-91, I-2-92

RAID Button

I-2-91

RALT - Radar Altimeter Function

I-2-168

RALT - Radar Altitude Hold

I-2-86

Ram Air Exhausts

I-2-97

RATS - Reduced Authority Thrust System

I-2-4

Receiver Hook-up and Refueling

III-9-16

Records and Reports

X-30-5

Recovery

IX-28-4

Reference Load Factor (Nz REF)

I-2-69

Refuel Data Display Switch

III-9-10

REFUEL Display

III-9-10

Refuel RST Button

III-9-10

Refuel SLEW Switch

III-9-11

Refueling Limitation

I-4-9

Refueling System

I-2-18

Refueling Technique

III-9-6

Regaining Currency

II-5-2

Relay Mode Of Operation

VII-23-29

Remote Switching Control (RSC)

I-2-178

Rendezvous and Formation

IX-29-3

Repetition of Preflight FCS Initiated BIT

I-2-195

Requirements for Instrument Qualification in E/F-Series Aircraft

II-5-3

REQUIREMENTS FOR VARIOUS FLIGHT PHASES

II-5-2

Reservoir Level Sensing (RLS) System

I-2-44

RESTART

V-15-1

Reversion

I-2-187

RF/CBL SINS Alignment

VII-24-13

RLY (Relay) Switch

VII-23-6

ROLL - Roll Attitude Hold

I-2-86

Roll CAS

I-2-65

Roll Rate Limiting

I-2-72

Roll-Axis Pilot Relief Modes

I-2-86

RUD PED ADJ Lever

I-2-74

RUD TRIM Knob

I-2-75

Rudder Pedals

I-2-73

Running Preflight FCS Initiated BIT After Flight

I-2-195

RVSM Checks

III-7-34

Index-23

ORIGINAL

A1-F18EA-NFM-000

Page

No.

SA Display

VII-24-62

SDC - Signal Data Computer

I-2-171

Seat Bucket Position Switch

I-2-125

SEAT CAUT MODE Switch (F/A-18F)

I-2-127

Seat Position Sensor (SPS)

I-2-208

Seat Survival Kit (SKU-10/A)

I-2-123

SEAWARS - SEAWATER Activated Release System

I-2-122

SEAWATER ENTRY

V-17-4

Secondary Heat Exchanger

I-2-98

SECONDARY POWER SYSTEM

I-2-27

Section Approaches/Landing

III-9-4

SECTION CCA

III-8-21

Section Landing

III-9-5

Section Takeoff

III-9-1

SECURE ERASE Button

I-2-172

SELECT JETT Knob

I-2-128

Selective Jettison

I-2-128

Sensor Control Panel

VII-24-9

Sensor Control Switch

I-2-89

SENSORS Option (HSI Format)

VII-24-9

SEQ # Option (HSI Format)

VII-24-8

SERVICING

I-3-1

SETLIM - Supersonic Engine Thrust Limiting

I-2-4

Setting the Alert

III-9-20

SEVER Caution

I-2-186

Shaped Attitude Display Indicator

I-2-149

Shipboard Taxi/Takeoff Checks

III-10-20

Shorebased Takeoff Checks

III-10-20

SHORT AIRFIELD FOR TACTICAL SUPPORT (SATS) PROCEDURES

III-9-19

Shoulder Harness Inertia Reel

I-2-122

Shoulder Harness Lock/Unlock Handle

I-2-122

SINCGARS Menu From AJ Menu Fixed Frequency COMM Sublevel

VII-23-17

SINCGARS SYSTEM

VII-23-20

SINGLE AOA FAILURE ON TAKEOFF

V-15-46

SINGLE ENGINE APPROACH AND LANDING

V-16-1

SINGLE ENGINE FAILURE IN LANDING CONFIGURATION

V-16-1, V-18-4

Single Engine Operation

IV-11-11

Single Engine Waveoff

IV-11-12

SINGLE ENGINE WAVEOFF/BOLTER

V-16-3

SINGLE L BLEED or R BLEED WARNING LIGHT

V-18-1

Situation Awareness

IX-28-1

SJU-17(V) 1/A, 2/A, and 9/A, and SJU-17A (V)1/A, 2/A, and 9/A NACES Seat

I-2-120

SLEW Option (HSI Format)

VII-24-6

Slow Speed Maneuvering

IV-11-8

SMS Initiated BIT

I-2-195

Software Configuration

VII-23-32

SPD BRK Light

I-2-69

Index-24

ORIGINAL

A1-F18EA-NFM-000

Page

No.

SPECIAL CONSIDERATIONS

IX-28-4, IX-29-7

Speedbrake Function

I-2-67

Speedbrake Switch

I-2-68

Spin

V-15-20

Spin Characteristics

IV-11-10

Spin Recovery

V-15-20

Spin Recovery Displays

I-2-77

Spin Recovery System

I-2-76

SPIN Switch

I-2-78

Spoilers

I-2-61

SSR Advisories

I-2-172

Stabilator Failure

IV-11-14

Stabilator Failure Control Law Reconfiguration

I-2-78

Stalls with Flaps HALF or FULL

IV-11-1

Standard Data Entry

I-2-167, VII-24-78

STANDARD ICS TERMS

IX-29-8

Standby Airspeed Indicator

I-2-140

Standby Altimeter

I-2-140

Standby Attitude Reference Indicator

I-2-140, VII-25-2

Standby Attitude Reference Indicator Controls and Indicators

VII-25-3

Standby Indication

I-2-150

Standby Magnetic Compass

I-2-141

Standby Rate of Climb Indicator

I-2-141

Start/Taxi/Takeoff

IX-29-2

Start-up BIT (SBIT)

I-2-211

Static Power Inverter

VII-25-3

Status Lights

III-9-11

Status Messages

I-2-213

Status Monitoring

VII-23-32

Status Monitoring Backup

I-2-201

Steering

VII-24-39

Steering Information

I-2-146

Stick

I-2-73

Stick Grip FCS Controls

I-2-74

Stick Grip Switches/Controls (Front Cockpit)

I-2-88

Stick Grip Switches/Controls (Trainer Configured F/A-18F)

I-2-90

STOP Button

I-2-200

Stopping Fuel Transfer

III-9-16

STORE Switch

III-9-10

Stored Heading (STD HDG) Alignment

VII-24-17

STROBE Switch

I-2-38

Sub-area

X-30-2

Suspected Inboard Aileron Hinge Failure Corrective Action

V-15-48

S/W CONFIG Caution

I-2-203

Switching Valve Operation

I-2-44

Switching Valves

I-2-44

Symbology Rocker Switch

I-2-150

System BIT Steps

I-2-193

Index-25

ORIGINAL

A1-F18EA-NFM-000

Page

No.

System Check - Airborne

III-9-14

System Check - Prestart

III-9-14

System Limitations and Constraints

I-2-132

TACAN BIT

VII-24-53

TACAN Mode Selection

VII-24-53

TACAN Position Keeping

VII-24-54

TACAN Position Updating

VII-24-54

TACAN Programming

VII-24-53

TACAN Steering

VII-24-54

TACAN (TACTICAL AIR NAVIGATION)

VII-24-52

TACTICAL AIRCRAFT MOVING MAP CAPABILITY (TAMMAC)

I-2-178

TAKEOFF

III-7-30, VI-22-2

Takeoff (*)

X-30-4

Takeoff and Landing

IV-11-1

Takeoff Checks

III-8-9

Takeoff/Departure

IX-28-3

TAMMAC Status Monitoring

I-2-179

Tanker Safety Precautions

III-9-12

Taxi

III-8-9, III-8-21, X-30-4

TAXI CHECKS

III-7-30

Taxi Checks

III-10-19, III-10-32

TCN Option (HSI Format)

VII-24-9

TD Control

VII-23-28

TDC - Throttle Designator Controller

I-2-91

TEF Failure Landing Handling Qualities

IV-11-13

TGT (Target) Programming

VII-24-29

Thermal Management System

I-2-17

Throttle Grip Switches/Controls (Front Cockpit)

I-2-90

Throttle Grip Switches/Controls (Trainer Configured Rear Cockpit)

I-2-91

Throttles

I-2-6

Throttles (Trainer Configured F/A-18F)

I-2-6

TIME Data

VII-23-45

Time Zone

VII-24-37

TIMEUFC Option (HSI Format)

VII-24-8

T/O TRIM Button

I-2-76

Top Level CNI Format Channel or Manual Frequency Change

VII-23-8

Top Level IFF PROG Page

VII-23-43

TOT (Time On Target) Programming

VII-24-29

TR - Transformer-rectifiers

I-2-32

Traffic Control Couple

VII-24-66

Trailing Edge Flap Failure

IV-11-13

TRANS Switch

III-9-12

Transfer Fuel from ARS to Tanker (Own Ship)

III-9-17

Trigger

I-2-89

True/Magnetic Heading Selection

VII-24-35

TURBULENT AIR AND THUNDERSTORM OPERATION

VI-20-4

Index-26

ORIGINAL

F18. FLIGHT MANUAL (2008) - page 31