F16C/D (BLOCKS 50 AND 52+). FLIGHT MANUAL (15 OCTOBER 2002) - page 5

T.O. GR1F16CJ1

124Change 1

HUD Combiner Glass

AOA Indexer

AR Status/NWS Indicator

Integrated Control Panel (ICP)

Standby Attitude Indicator

FUEL FLOW Indicator

Data Entry Display

ENG FIRE and ENGINE Warning

Lights (Red)

HYD/OIL PRESS Warning Light (Red)

FLCS and DBU ON Warning

Lights (Red)

TO/LDG CONFIG Warning Light (Red)

CANOPY and OXY LOW Warning Lights (Red)

Right MFD

OIL Pressure Indicator

NOZ POS Indicator

RPM Indicator

FTIT Indicator

Vertical Velocity Indicator

MRK BCN Light

FUEL QTY SEL Panel

Rudder PEDAL ADJ Knob

AOA Indicator

INSTR MODE Select Panel

Airspeed/Mach Indicator

Attitude Director Indicator

Horizontal Situation Indicator

Altimeter

Left MFD

Autopilot PITCH Switch

Autopilot ROLL Switch

ADV MODE Switch

MASTER ARM Switch

LASER ARM Switch

34. IFF IDENT Button

35. DRAG CHUTE Switch

36. RWR Prime Control Panel

37. Azimuth Display/Indicator

38. F-ACK Button

39. TF FAIL Warning Light (Red)

40. MASTER CAUTION Light (Amber)

1

4

5

38

37

13

28

24 27

25

26 20

3

7

6 8 9

10

11 12

14

15

16

17

18

19

21

23

22

29

30

31

33

35

32

34

36

39

40

41

2

1.

2.

3.

4.

5.

6.

7.

8.

9.

10.

11.

12.

13.

14.

15.

16.

17.

18.

19.

20.

21.

22.

23.

24.

25.

26.

27.

28.

29.

30.

31.

32.

33.

DF

41. ECM Light (Green),      ECM (Green)

DF

INSTRUMENT PANEL

Cockpit Arrangement        (Typical)

DF

C

GR1F-16CJ-1-1009X37

    and OVRD (Amber) Light

PX III

Figure 13. (Sheet 14)

T.O. GR1F16CJ1

Change 1125

RIGHT CONSOLE

Cockpit Arrangement        (Typical)

DF

C

GR1F-16CJ-1-1010X37

DF

1

2

3

7

10

12

11

9 8

19

16

15

14

SNSR PWR Control Panel

HUD Control Panel

NUCLEAR CONSENT Switch (Guarded)

AIR COND Control Panel

ENGINE ANTI-ICE Switch

Utility Light

ANT SEL Panel

AVIONICS POWER Panel

OBOGS MONITOR Panel

UDTU

Stowage

Oxygen/Communication Hookup

VOICE MESSAGE Switch

ZEROIZE Switch

Stick

SEAT ADJ Switch

    NWS Control Button/Indicator (Green)

DF

1.

2.

3.

4.

6.

7.

8.

9.

10.

11.

12.

13.

14.

15.

16.

19.

18.

DF

18

17

13

5.

6

5

PLAIN Cipher Switch

17.

Interior LIGHTING Control Panel

4

PX III

20

OXYGEN Panel

20.

Figure 13. (Sheet 15)

T.O. GR1F16CJ1

126

INSTRUMENT

PANEL

LEFT

AUXILIARY

CONSOLE

THROTTLE

LEFT

CONSOLE

RIGHT

CONSOLE

STICK

RIGHT

AUXILIARY

CONSOLE

GR1F-16CJ-1-1011X37

DR

Cockpit Arrangement    (Typical)

PX III

Figure 13. (Sheet 16)

T.O. GR1F16CJ1

127

LEFT CONSOLE

AUDIO 1 Control Panel

AUDIO 2 Control Panel

G-Suit Hose Connection

ANTI G TEST Button

MAL & IND LTS Test Button

FUEL MASTER Switch

MANUAL PITCH Override Switch

ENG CONT Switch

Throttle

CANOPY JETTISON T-Handle

Stowage

1.

2.

3.

4.

5.

6.

7.

8.

9.

10.

11.

1

2

8

7

6

4

5

11

10

9

3

GR1F-16CJ-1-1012X37

DR

Cockpit Arrangement    (Typical)

PX III

Figure 13. (Sheet 17)

T.O. GR1F16CJ1

128

GR1F-16CJ-1-1013X37

DR

Cockpit Arrangement    (Typical)

LEFT AUXILIARY CONSOLE

Clock

FUEL Quantity Indicator

System B HYD PRESS Indicator

System A HYD PRESS Indicator

EJECTION MODE SELECT Handle

Caution Light Panel

1.

2.

3.

4.

5.

6.

RIGHT AUXILIARY CONSOLE

1 2

6

3

4

5

EMER STORES JETTISON Button (Covered)

WHEELS Down Lights (Green)

HOOK Switch (Lever Lock)

DN LOCK REL Button

LG Handle Down Permission Button

LG Handle Warning Light (Red)

LG Handle

ALT GEAR Handle

ALT GEAR Reset Button

SPEED BRAKE Position Indicator

ALT FLAPS Switch (Lever Lock)

HORN SILENCER Button

GND JETT ENABLE Switch (Lever Lock)

1.

2.

3.

4.

5.

6.

7.

8.

9.

10.

11.

12.

14.

13.

Blank Panel

1 2

3

4

7

5

6

11

13

8

9

12

14

10

15

DRAG CHUTE Switch

15.

PX III

Figure 13. (Sheet 18)

T.O. GR1F16CJ1

129

2. ENG FIRE and ENGINE Warning

3. HYD/OIL PRESS Warning Light (Red)

4. FLCS and DBU ON Warning Lights (Red)

5. AR Status/NWS Indicator

6. TO/LDG CONFIG Warning Light (Red)

7. CANOPY and OXY LOW Warning Lights (Red)

8. Right MFD (NVIS)

9. VIDEO SEL Switch

10. Standby Attitude Indicator

11. FUEL FLOW Indicator

12. OIL Pressure Indicator

13. FAULT ACK Button

14. NOZ POS Indicator

15. RPM Indicator

16. FTIT Indicator

17. Pilot Fault List Display

18. Accelerometer

19. Altimeter

20. Vertical Velocity Indicator

21. Attitude Director Indicator

22. Horizontal Situation Indicator

23. MRK BCN Light

24. Rudder PEDAL ADJ Knob

25. INSTR MODE Select Panel

26. AOA Indicator

27. Airspeed/Mach Indicator

28. ARMT CONSENT Switch (Guarded)

29. MASTER MODE Caution Lights (NVIS)

30. Data Entry Display

31. Integrated Keyboard Panel (IKP) (NVIS)

32. IFF IDENT Button

33. Stick Indicator

34. Blank

35. Azimuth Display/Indicator (NVIS)

36. Left MFD (NVIS)

37. AOA Indexer (NVIS)

38. TF FAIL Warning Light (Red)

39. Handgrip

   Lights (Red)

INSTRUMENT PANEL

GR1F-16CJ-1-1014X37

DR

Cockpit Arrangement    (Typical)

MASTER CAUTION Light (Amber) (NVIS)

1.

34

33

32

30 29

28

26

25

24

22

21

31

35

36

8

11

27 19 18

17

20

23

16

10

15

14

13

12

9

7

5

4

3

2

41

38

37

39

1

6

41. Aft Seat HUD Monitor (NVIS)

40. ECM and OVRD Lights (Amber)

40

PX III

Figure 13. (Sheet 19)

T.O. GR1F16CJ1

130

1

2

4

6

5

8

Interior LIGHTING Control Panel

OXYGEN REGULATOR Panel

Utility Light

Oxygen/Communications Hookup

Stowage

NWS Control Button/Indicator (Green)

Stick

SEAT ADJ Switch

RIGHT CONSOLE

1.

2.

3.

4.

5.

6.

7.

8.

3

GR1F-16CJ-1-1015X37

DR

Cockpit Arrangement    (Typical)

7

STICK CONTROL/ASIU Panel

9.

9

PX III

Figure 13. (Sheet 20)

T.O. GR1F16CJ1

131

ENGINE 

PW 229

ENGINE GENERAL DESCRIPTION 

PW 229

Refer to figure 14. The aircraft is powered by a single

F100PW229 afterburning turbofan engine. Maxi

mum thrust is approximately 29,000 pounds.

ENGINE FUEL SYSTEM 

PW 229

Refer to figure 15. The engine fuel system delivers

the required fuel to the engine for combustion and for

use by the control system for scheduling the engine

variable geometry.

ENGINE CONTROL SYSTEM 

PW 229

The engine control system is composed of three major

components:the main fuel control (MFC), the AB

fuel control, and the digital electronic engine control

(DEEC). The engine has two modes of opera

tion:primary (PRI) and secondary (SEC).

Main Fuel Control (MFC) 

PW 229

The MFC operates in both the PRI and SEC modes.

During PRI control, the MFC receives throttle inputs,

fuel from the main fuel pump, and electrical

commands from the DEEC. It controls main ignition,

start bleed strap position, main engine fuel flow, and

rear compressor variable vane (RCVV) position. The

MFC also provides actuation pressure to the

compressor inlet variable vane (CIVV) control, the

convergent exhaust nozzle control (CENC), and both

the AB fuel control and AB pump controller.

In SEC, the MFC receives throttle inputs, fuel from

the main fuel pump, and static pressure and total

temperature signals from the fan inlet case. The MFC

controls main engine fuel flow, start bleed strap

position, RCVV's, and engine ignition.

Afterburner (AB) Fuel Control 

PW 229

During primary operation, the AB fuel control

receives fuel from the AB fuel pump and electrical

commands from the DEEC. It provides AB ignition,

AB segment sequencing, and fuel flow to the AB

segments. During SEC control, AB fuel flow is

inhibited.

F100-PW-229 Engine

INLET

PRESSURE

PROBE

CIVV

MAIN FUEL PUMP

DIGITAL ELECTRONIC ENGINE CONTROL

HIGH PRESSURE TURBINE

AB SPRAY RINGS

AND FLAME HOLDER

FAN

3 STAGES

RCVV

FAN MODULE

FAN DRIVE

TURBINE

MODULE

AB MODULE

CORE ENGINE

MODULE

1F-16X-1-4004X

ENGINE-DRIVEN GEARBOX

ENGINE

DIAGNOSTIC

AB FUEL CONTROL

MAIN FUEL CONTROL

CONVERGENT

NOZZLE

DIVERGENT

NOZZLE

AB LIGHT-OFF DETECTOR

UNIT

REAR COMPRESSOR

10 STAGES

COMBUSTION

CHAMBER

FAN

DUCT

Figure 14.