F16C/D. FLIGHT MANUAL (2002) - page 3

T.O. GR1F16CJ1

118

GR1F-16CJ-1-0013A37

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 II

Figure

 13.(Sheet 8)

T.O. GR1F16CJ1

119

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 Warning Light (Red)

8. Right MFD

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. IFF IDENT Button

30. Data Entry Display

31. Integrated Keyboard Panel (IKP)

32. Stick Indicator

33. OVRD Light (Amber)

34. Blank

35. Azimuth Display/Indicator

36. Left MFD

37. AOA Indexer

38. TF FAIL Warning Light (Red)

39. Handgrip

   Lights (Red)

INSTRUMENT PANEL

GR1F-16CJ-1-0014A37

DR

Cockpit Arrangement    (Typical)

MASTER CAUTION Light (Amber)

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

40. ECM Light (Green)

40

PX II

Figure

 13.(Sheet 9)

T.O. GR1F16CJ1

120

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-1-0015A37

DR

Cockpit Arrangement    (Typical)

7

PX II

Figure

 13.(Sheet 10)

T.O. GR1F16CJ1

Change 1121

LEFT

AUXILIARY

CONSOLE

LEFT

CONSOLE

STICK

RIGHT

AUXILIARY

CONSOLE

RIGHT

CONSOLE

DF

DF

DF

Cockpit Arrangement        (Typical)

DF

C

GR1F-16CJ-1-1006X37

INSTRUMENT

PANEL

DF

PX III

THROTTLE

Figure 13. (Sheet 11)

T.O. GR1F16CJ1

122

LEFT CONSOLE

Cockpit Arrangement        (Typical)

DF

C

GR1F-16CJ-1-1007X37

DF

24

23

1

2

3

4
5

6

8

9

10

11

13

15

17

16

20

19

22

21

18

14

12

25

1.

2.

3.

4.

5.

6.

7.

8.

9.

10.

11.

12.

13.

14.

15.

16.

17.

18.

19.

20.

21.

22.

23.

24.

UHF Backup Control Panel

AUDIO 1 Control Panel

AUDIO 2 Control Panel

ECM Control Panel

AVTR Control Panel

EXT LIGHTING Control Panel

MANUAL TRIM Panel

G-Suit Hose Connection

ANTI G TEST Button

    STICK CONTROL Switch

Stowage

TEST Switch Panel

DEFOG Lever

FLT CONTROL Panel

Fuel Control Panel

IFF Panel

CANOPY JETTISON T-Handle

EPU Control Panel

ELEC Control Panel

Throttle FRICTION Control

ENG & JET START Control Panel

MANUAL PITCH Override Switch

CHAFF/FLARE Dispense Button

Throttle

DF

PX III

25.

JHMCS Connection

7

Figure 13. (Sheet 12)

T.O. GR1F16CJ1

123

Cockpit Arrangement        (Typical)

DF

C

GR1F-16CJ-1-1008X37

LEFT AUXILIARY CONSOLE

RIGHT AUXILIARY CONSOLE

1.

2.

3.

4.

5.

6.

7.

8.

9.

10.

11.

12.

13.

14.

15.

16.

17.

18.

EMER STORES JETTISON Button (Covered)

WHEELS Down Lights (Green)

HOOK Switch (Lever Lock)

ANTI-SKID Switch

DN LOCK REL Button

LG Handle Down Permission Button

LG Handle

LANDING TAXI LIGHTS Switch

LG Handle Warning Light (Red)

CMDS Control Panel

HMCS Panel

RWR Aux Control Panel

ALT GEAR Handle

ALT GEAR Reset Button

SPEED BRAKE Position Indicator

STORES CONFIG Switch

HORN SILENCER Button

GND JETT ENABLE Switch (Lever Lock)

BRAKES Channel Switch

10

1 2 3

4

7

6

8

14

15

16

17

18

19

5

19.

13

12

11

9

1.

2.

3.

4.

5.

6.

7.

8.

9.

Magnetic Compass

FUEL Quantity Indicator

Pilot Fault List Display

System A HYD PRESS Indicator

System B HYD PRESS Indicator

Caution Light Panel

EPU FUEL Quantity Indicator

Cockpit Pressure Altimeter

Clock

1

2

4

5

7

8

9

6

3

DF

PX III

Figure 13. (Sheet 13)

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.

T.O. GR1F16CJ1

132

ENGINE F100-PW-229

Engine Fuel/Control System Schematic

(Typical)

FROM FFP

AIRFRAME

ENGINE

LEGEND:

ELECTRICAL

ENG BLEED AIR
FUEL (COOLING)

AB FUEL FLOW

MECHANICAL

SERVO PRESSURE

AB FUEL

PUMP

FUEL FLOW

TRANSMITTER

ENGINE ELECTRONIC

CONTROL COOLING

FUEL SHUTOFF VALVE

FUEL/OIL HEAT

EXCHANGER

MAIN FUEL

SHUTOFF VALVE

AIRFRAME SIGNALS

MAIN

FUEL

CONTROL

(MFC)

AB FUEL

CONTROL

(AFC)

ENGINE LUBE OIL TO

AND FROM OIL SYSTEM

BOOST PUMP PRESS

GR1F-16CJ-1-1017X37

FUEL LINE

STRAINER

MAIN

FUEL

PUMP

ENGINE

SIGNALS

CENC

ENGINE

BLEED AIR

(FOR ACTUATION)

OVBD

ST

AR

T

BLEED

CIVV

RCVV

FUEL/OIL

COOLER

ACTUATION

PRESSURE

FUEL PRESSURI-

ZATION AND

DUMP VALVE

DIGITAL

ELECTRONIC

ENGINE

CONTROL

(DEEC)

LIGHT-OFF

DETECTOR

ENGINE

FAN

DUCT

ENGINE CONTROL

AND FEEDBACK

RCVV

ACTUATOR

CONTROL AND

FEEDBACK

MFP BOOST PRESS
MFP PRESSURE

ENGINE

DIAGNOSTIC

UNIT (EDU)

ENGINE

CONTROL

AND

FEEDBACK

THROTTLE

AIRFRAME

SIGNALS

ANTI-

ICING

VALVE

AB PUMP

CONTROLLER

ENGINE INLET

CASE

ENGINE BLEED AIR

ENGINE

BLEED

AIR FOR

TURBINE

POWER

RTN

TO

RSVRS

CIVV

ACTUATOR

AB RESET

COCKPIT ANTI-ICE

ENGINE DATA REQUEST

ICE DETECTOR SIGNAL

MACH

ENGINE FAULT

FTIT

NOZ POS

OIL

RPM

ENGINE SIGNALS

Figure 15.

T.O. GR1F16CJ1

133

Digital Electronic Engine Control (DEEC) 

PW 229

The DEEC is an enginemounted, fuelcooled, solid

state digital full authority computer.

Control functions provided by the DEEC during PRI

operation are:

D

Fuel flow scheduling.

D

Fan speed control.

D

Engine pressure ratio scheduling.

D

Core compressor speed limiting.

D

FTIT limiting.

D

Minimum and maximum compressor discharge

pressure limiting.

D

Nozzle position control.

D

RCVV scheduling.

D

CIVV scheduling.

D

Compressor start bleed system scheduling.

D

AB segment sequencing and cancellation.

D

Logic to detect and compensate for control system

malfunctions.

D

Logic to provide automatic transfer to SEC in the

event of a critical PRI failure.

The DEEC closedloop idle control schedules MFC

fuel flow for three different idle levels. For functional

description, refer to ENGINE OPERATING CHAR

ACTERISTICS 

PW 229

, this section.

The DEEC limits minimum engine rpm throughout the

flight envelope to maintain stable operation. At high

altitude, low airspeed conditions, the DEEC protects

against engine stalls. During transonic and supersonic

conditions, the DEEC limits minimum idle rpm as a

function of mach number (from CADC) to provide

sufficient engine airflow.

To minimize the possibility of stalls during AB operation

at high altitude and low airspeed, the DEEC commands

termination of segment 11 AB. At extremely high

altitude and low airspeed, the DEEC limits AB operation

to eight AB segments. When a stall is sensed, the DEEC

cancels the AB (if throttle is in AB range) and opens the

nozzle until the stall clears. For subsequent AB

operation, the throttle must be retarded below AB before

AB can be reinitiated.

An engine overspeed or overtemperature condition

causes the DEEC to automatically transfer to SEC and

illuminate the SEC caution light.

The DEEC receives power directly from the engine

alternator. In the event of an engine alternator or engine

gearbox failure indicated by rapid decrease to zero rpm

and illumination of the ENGINE warning light, the

DEEC loses power and an automatic transfer to SEC

occurs.

Secondary Engine Control (SEC) 

PW 229

The SEC is a hydromechanical system which provides

engine control in the event of a DEEC malfunction. In

SEC, the CIVV's move to a fixed (cambered) position,

nozzle position is closed, the RCVV's are positioned by a

hydromechanical control in the MFC, and AB operation

is inhibited. SEC is selected manually with the ENG

CONT switch or automatically by the DEEC. During

SEC operation, the SEC caution light illuminates.

Main Fuel Pump 

PW 229

The gearboxmounted main fuel pump provides

pressurized fuel to the MFC and boosts pressure to

the AB fuel pump.

Afterburner (AB) Fuel Pump 

PW 229

The AB fuel pump is driven by engine bleed air and

provides pressurized fuel to the AB. The pump operates

only during AB operation.

Compressor Inlet Variable Vane (CIVV) 

Control 

PW 229

The CIVV control positions the CIVV's using MFC fuel

pressure in response to an electrical signal from the

DEEC. In SEC, the CIVV's are in a fixed (cambered)

position.

Rear Compressor Variable Vanes (RCVV's) 

PW 229

The first three stages of the rear compressor are

equipped with variable geometry vanes. In PRI,

RCVV's are controlled by the DEEC and are positioned

using pressurized fuel from the main fuel pump. In

SEC, the RCVV's are positioned by a hydromechanical

control in the MFC as a direct function of throttle

position.