F16C/D (BLOCKS 50 AND 52+). FLIGHT MANUAL (15 OCTOBER 2002) - page 28

T.O. GR1F16CJ1

1208

ADI

HSI

EGI/INS PITCH AND

ROLL ATTITUDE

The TCN mode has no effect

on HUD symbology.

GR1F-16CJ-1-0085A37

ADI

HSI

INS/EGI PITCH AND

ROLL ATTITUDE

The NAV mode has no effect

on HUD symbology.

NAV

TCN

Instrument Modes (Typical)

BEARING TO INS/EGI

DESTINATION

HEADING REFERENCE MARKER

MANUALLY SELECTED

(OUT OF VIEW)

RANGE TO INS/EGI

DESTINATION

TO-FROM INDICATOR

COURSE

EGI/INS MAGNETIC HEADING

SIGNAL UNRELIABLE

EGI/INS MAGNETIC HEADING

MANUALLY SELECTED

COURSE

BEARING TO TACAN

STATION

HEADING REFERENCE MARKER

MANUALLY SELECTED

TO-FROM INDICATOR

COURSE

TACAN COURSE SIGNAL

UNRELIABLE

EGI/INS MAGNETIC HEADING

MANUALLY SELECTED

COURSE

RANGE TO TACAN

STATION OR DME

NAV AID

INSTR MODE

SELECT PANEL

(IMSP)

INSTR MODE

SELECT PANEL

(IMSP)

DEVIATION FROM

SELECTED COURSE

DEVIATION FROM

SELECTED COURSE

NOTE:

NOTE:

Figure 186.(Sheet 1)

T.O. GR1F16CJ1

1209

ADI

INSTR MODE

SELECT PANEL

LOCALIZER

DEVIATION

GLIDE SLOPE

DEVIATION

GR1F-16CJ-1-0086A37

NOTES:

LOCALIZER SIGNAL

UNRELIABLE

GLIDE SLOPE

SIGNAL

Glide slope and localizer

bars indicate deviation

only, not steering.

Command steering is

referenced to the

localizer course

displayed on the DED.

1.

2.

UNRELIABLE

(IMSP)

INS PITCH AND

ROLL ATTITUDE

HSI

HEADING REFERENCE MARKER

MANUALLY SELECTED

(OUT OF VIEW)

TO-FROM INDICATOR

COURSE

ILS LOCALIZER SIGNAL

UNRELIABLE

INS MAGNETIC HEADING

MANUALLY SELECTED

COURSE

BEARING TO TACAN

STATION

ILS/TCN

Instrument Modes (Typical)

LOCALIZER

DEVIATION

HUD

GLIDE SLOPE

DEVIATION

AOA BRACKET

(NLG LOWERED)

CALIBRATED

AIRSPEED

FLIGHTPATH

MARKER (FPM)

INS MAGNETIC HEADING

SELECTED COURSE

(  CROSSWIND COMPONENT)

(LIMITED)

RADAR ALTITUDE

ALTITUDE LOW

SETTING

PITCH SCALE (DIVE)

BAROMETRIC ALTITUDE

20

150

10

C

5

06 065 07

02,2

02,100

02,0

R 01,450

AL 200

10

10

10

10

5

5

5

PITCH SCALE (CLIMB)

LOCALIZER

DEVIATION

RANGE TO TACAN

STATION OR DME

NAV AID

HORIZON LINE

ROLL SCALE

COMMAND STEERING

(CMD STRG)

DISTANCE TO STEERPOINT/

STEERPOINT NUMBER

150 03

PX II

Figure 186.(Sheet 2)

T.O. GR1F16CJ1

1210

ADI

INSTR MODE

SELECT PANEL

LOCALIZER

DEVIATION

GLIDE SLOPE

DEVIATION

GR1F-16CJ-1-1086X37

NOTES:

LOCALIZER SIGNAL

UNRELIABLE

GLIDE SLOPE

SIGNAL

Glide slope and localizer

bars indicate deviation

only, not steering.

Command steering is

referenced to the

localizer course

displayed on the DED.

1.

2.

UNRELIABLE

(IMSP)

EGI PITCH AND

ROLL ATTITUDE

HSI

HEADING REFERENCE MARKER

MANUALLY SELECTED

(OUT OF VIEW)

TO-FROM INDICATOR

COURSE

ILS LOCALIZER SIGNAL

UNRELIABLE

EGI MAGNETIC HEADING

MANUALLY SELECTED

COURSE

BEARING TO TACAN

STATION

ILS/TCN

Instrument Modes (Typical)

LOCALIZER

DEVIATION

HUD

GLIDE SLOPE

DEVIATION

AOA BRACKET

(NLG LOWERED)

CALIBRATED

AIRSPEED

FLIGHTPATH

MARKER (FPM)

EGI MAGNETIC HEADING

SELECTED COURSE

(  CROSSWIND COMPONENT)

(LIMITED)

RADAR ALTITUDE

ALTITUDE LOW

SETTING

PITCH SCALE (DIVE)

BAROMETRIC ALTITUDE

20

150

10

C

5

06 065 07

02,2

02,100

02,0

R 01,450

AL 200

10

10

10

10

5

5

5

PITCH SCALE (CLIMB)

LOCALIZER

DEVIATION

RANGE TO TACAN

STATION OR DME

NAV AID

HORIZON LINE

ROLL SCALE

COMMAND STEERING

(CMD STRG)

DISTANCE TO STEERPOINT/

STEERPOINT NUMBER

PX III

OWNSHIP BEARING

AND RANGE FROM

BULL'S-EYE

F008.0

05:50

035 05

4.1

ILS

090 25

0.88

Figure 186.(Sheet 3)

T.O. GR1F16CJ1

1211

ADI

INSTR MODE

SELECT PANEL

LOCALIZER

DEVIATION

GLIDE SLOPE

DEVIATION

GR1F-16CJ-1-0087A37

NOTES:

LOCALIZER SIGNAL

UNRELIABLE

GLIDE SLOPE

SIGNAL

Glide slope and localizer

bars indicate deviation

only, not steering.

Command steering is

referenced to the

localizer course

displayed on the DED.

1.

2.

UNRELIABLE

(IMSP)

INS PITCH AND

ROLL ATTITUDE

HSI

HEADING REFERENCE MARKER

MANUALLY SELECTED

(OUT OF VIEW)

TO-FROM INDICATOR

COURSE

ILS LOCALIZER SIGNAL

UNRELIABLE

INS MAGNETIC HEADING

MANUALLY SELECTED

COURSE

BEARING TO INS

DESTINATION

RANGE TO INS

DESTINATION

ILS/NAV

Instrument Modes (Typical)

LOCALIZER

DEVIATION

HUD

GLIDE SLOPE

DEVIATION

AOA BRACKET

(NLG LOWERED)

CALIBRATED

AIRSPEED

FLIGHTPATH

MARKER (FPM)

INS MAGNETIC HEADING

SELECTED COURSE

(  CROSSWIND COMPONENT)

(LIMITED)

RADAR ALTITUDE

ALTITUDE LOW

SETTING

PITCH SCALE (DIVE)

BAROMETRIC ALTITUDE

20

150

10

C

5

06 065 07

02,2

02,100

02,0

R 01,450

AL 200

10

10

10

10

5

5

5

PITCH SCALE (CLIMB)

LOCALIZER

DEVIATION

HORIZON LINE

ROLL SCALE

COMMAND STEERING

(CMD STRG)

DISTANCE TO STEERPOINT/

STEERPOINT NUMBER

150 03

PX II

Figure 186.(Sheet 4)

T.O. GR1F16CJ1

1212

ADI

INSTR MODE

SELECT PANEL

LOCALIZER

DEVIATION

GLIDE SLOPE

DEVIATION

GR1F-16CJ-1-1087X37

NOTES:

LOCALIZER SIGNAL

UNRELIABLE

GLIDE SLOPE

SIGNAL

Glide slope and localizer

bars indicate deviation

only, not steering.

Command steering is

referenced to the

localizer course

displayed on the DED.

1.

2.

UNRELIABLE

(IMSP)

EGI PITCH AND

ROLL ATTITUDE

HSI

HEADING REFERENCE MARKER

MANUALLY SELECTED

(OUT OF VIEW)

TO-FROM INDICATOR

COURSE

ILS LOCALIZER SIGNAL

UNRELIABLE

EGI MAGNETIC HEADING

MANUALLY SELECTED

COURSE

BEARING TO EGI

DESTINATION

RANGE TO EGI

DESTINATION

ILS/NAV

Instrument Modes (Typical)

LOCALIZER

DEVIATION

PX III

HUD

GLIDE SLOPE

DEVIATION

AOA BRACKET

(NLG LOWERED)

CALIBRATED

AIRSPEED

FLIGHTPATH

MARKER (FPM)

EGI MAGNETIC HEADING

SELECTED COURSE

(  CROSSWIND COMPONENT)

(LIMITED)

RADAR ALTITUDE

ALTITUDE LOW

SETTING

PITCH SCALE (DIVE)

BAROMETRIC ALTITUDE

20

150

10

C

5

06 065 07

02,2

02,100

02,0

R 01,450

AL 200

10

10

10

10

5

5

5

PITCH SCALE (CLIMB)

LOCALIZER

DEVIATION

HORIZON LINE

ROLL SCALE

COMMAND STEERING

(CMD STRG)

DISTANCE TO STEERPOINT/

STEERPOINT NUMBER

OWNSHIP BEARING

AND RANGE FROM

BULL'S-EYE

F008.0

05:50

035 05

4.1

ILS

090 25

0.88

Figure 186.(Sheet 5)

T.O. GR1F16CJ1

1213

GR1F-16CJ-1-0088X37

INBOUND LOCALIZER COURSE = 090

45

45  INTERCEPT HEADING

(090  - 45  = 045

AIRCRAFT HEADING)

INITIAL AIRCRAFT

HEADING = 015

01

02

04

05

AIRCRAFT IS ON 45  INTERCEPT HEADING

30  BANK ACHIEVED

01

02

02

03

6

5

7

8

9

10

2

3

4

1

1

2

3

4

RUNWAY

015

023

045

015

Instrument Modes (Typical)

ILS HUD DISPLAYS

CMD STRG SYMBOL APPEARS (NO PITCH

STEERING PROVIDED)

LOCALIZER DEVIATION BAR IS SOLID (VALID)

A RIGHT TURN IS COMMANDED (CMD STRG

SYMBOL IS TO RIGHT OF FPM)

NO CMD STRG SYMBOL

LOCALIZER AND GLIDE SLOPE DEVIATION

BARS ARE DASHED (INVALID)

COURSE CARET IS LIMITED

HORIZON LINE IS DISPLAYED FOR

REFERENCE

Figure 186.(Sheet 6)

T.O. GR1F16CJ1

1214

GR1F-16CJ-1-0089X37

04

05

A RIGHT TURN IS COMMANDED (CMD STRG SYMBOL IS TO

RIGHT OF FPM)

LOCALIZER DEVIATION BAR INDICATES APPROXIMATELY 2

DOTS LEFT

30  BANK ACHIEVED

LOCALIZER DEVIATION BAR INDICATES APPROXIMATELY

06

07

AIRCRAFT IS ON LOCALIZER COURSE (CMD STRG SYMBOL,

COURSE CARET, AND LOCALIZER DEVIATION BAR ARE ALL

COURSE CARET INDICATES 083  VS 090  HEADING DUE TO

08

09

080

08

09

08

09

5

6

7

10

9

8

083

045

062

083

09

07

ILS HUD DISPLAYS

Instrument Modes (Typical)

1 DOT LEFT

083

ALIGNED)

CROSSWIND

AIRCRAFT IS LEFT OF LOCALIZER COURSE AND GLIDE SLOPE

IS INVALID (CMD STRG SYMBOL HAS X ON IT. NO PITCH

STEERING IS PROVIDED)

AFTER TIC MARK APPEARS ON TOP OF CMD STRG SYMBOL,

PITCH STEERING IS PROVIDED

AIRCRAFT IS ON LOCALIZER COURSE AND ABOVE GLIDE

SLOPE

AIRCRAFT IS ON LOCALIZER COURSE AND GLIDE SLOPE

(ALL SYMBOLS ALIGNED)

Figure 186.(Sheet 7)

T.O. GR1F16CJ1

1215

FLIGHT INSTRUMENTS

Refer to figure 187. The flight instruments are

located on the instrument panel. The instruments

listed below are common and are not illustrated in

detail.

D

Airspeed/Mach Indicator.

D

Clock.

D

Magnetic Compass.

D

ServoPneumatic Altimeter.

D

Standby Attitude Indicator.

D

Vertical Velocity Indicator.

ALTIMETER

The servopneumatic altimeter is a dual mode

pressure altitude indicator with a range of -1000 to

+80,000 feet. The operating mode is manually

selected by the mode lever located at the lower right

corner of the instrument. In the ELECT (primary)

operating mode, the altimeter is electrically driven by

the CADC. In the PNEU (secondary) operating mode,

the altimeter is pneumatically operated by static

pressure supplied by the pitotstatic system. Should

the CADC or altimeter servo malfunction, the

altimeter automatically reverts to the pneumatic

mode and the PNEU flag appears on the face of the

altimeter. The PNEU flag may also appear when

accelerating or decelerating through the transonic

region or while performing high g maneuvers.

The barometric setting knob, located at the lower left

corner of the instrument, is used to set the desired

altimeter setting. 

C

 

DF

 The barometric setting of the

altimeter is electrically transmitted to the CADC as

a manual input correction for the pressure altitude

display on the HUD. The barometric setting is shown

in inches of mercury (Hg).

Flight Instruments (Typical)

GR1F-16CJ-1-0090X37

DR

C DF

1. AOA Indexer

2. Standby Attitude Indicator

3. Altimeter

4. Vertical Velocity Indicator

5. Magnetic Compass

6. Clock

Horizontal Situation

Indicator

Attitude Director Indicator

AOA Indicator

Airspeed/Mach Indicator

7.

8.

9.

10.

2

6

5

3

4

7

8

9

10

1

2

6

3
4

7

8

9

10

1

Figure 187.