F16C/D (BLOCKS 50 AND 52+). FLIGHT MANUAL (15 OCTOBER 2002) - page 3

 

  Index      Manuals     Lockheed Martin F16C/D (BLOCKS 50 AND 52+). FLIGHT MANUAL (15 OCTOBER 2002)

 

Search            copyright infringement  

 

   

 

   

 

Content      ..     1      2      3      4      ..

 

 

 

F16C/D (BLOCKS 50 AND 52+). FLIGHT MANUAL (15 OCTOBER 2002) - page 3

 

 

T.O. GR1F16CJ1

18

GR1F-16CJ-1-0004-1A37

15

22.20

49 FT 5.2 IN.

OVERALL LENGTH

82.05

108.62

95.0 101.0

16 FT 10.0 IN.

OVERALL

HEIGHT

STATIC GROUND LINE

49.81

29.08

15.35

46.80

MISSILE LAUNCHER

15.16

FLAPERON

40

37.39

69.63

SPEEDBRAKE HINGE

29.72

12.05

8.45

70.87

190.43

44.42

135.84

195.52

30.63

28.63

370-GALLON FUEL TANK

OUTBOARD STORES LOCATIONS

13.32

AIM-9 MISSILE

18 FT 4.2 IN.

95.82

General Data

NOTE:

Dimensions are in inches unless specified otherwise.

19.5

D

SHADED AREA REPRESENTS             AIRCRAFT

PX III

Figure

 11.(Sheet 1)

T.O. GR1F16CJ1

19

GR1F-16CJ-1-0004-2A37

31 FT

OVERALL SPAN W/O MISSILES

93.0

46.5

10

WINGS

   Area

   Span

   Aspect Ratio

   Taper Ratio

   Sweep (LE)

   Dihedral

   Airfoil

   Incidence

   Twist

      At BL 54.0

      At BL 180.0

   Flaperon Area

   LEF Area

HORIZONTAL TAILS

   Area

   Aspect Ratio

   Taper Ratio

   Sweep (LE)

   Dihedral

   Airfoil

      At Root

      At Tip

VERTICAL TAIL

   Area

   Aspect Ratio

   Taper Ratio

   Sweep (LE)

   Airfoil

      At Root

      At Tip

   Rudder Area

300 Sq Ft

30 Ft

3.0

0.2275

40

0

NACA 64A204

0

0

3

31.32 Sq Ft

36.71 Sq Ft

63.70 Sq Ft

2.114

0.390 (Theo)

40

-10

6% Biconvex

3.5% Biconvex

54.75 Sq Ft

1.294

0.437

47.5

5.3% Biconvex

3.0% Biconvex

11.65 Sq Ft

VENTRAL FIN (EACH)

   Area

   Span

   Aspect Ratio

   Taper Ratio

   Sweep (LE)

   Dihedral (Cant)

   Airfoil

      At Root

      At Tip

SPEEDBRAKES

   Area (4 Element Clamshell)

LANDING GEAR (LG)

   Main Gear (MLG)

      Tire Size

      Stroke

      Static Rolling Radius

   Nose Gear (NLG)

      Tire Size

      Stroke

      Static Rolling Radius

ENGINE

8.03 Sq Ft

23.356 In. Theo (27.5 In. Actual)

0.472 (Theo)

0.760 (Theo)

30

15  Outboard

3.886% Modified Wedge

Constant 0.03R

14.26 Sq Ft (3.565 Sq Ft Ea)

27.75 x 8.75-14.5 24 Ply

10.5 In.

11.9 In.

17.9 x 6.7R8 22 Ply

10.0 In.

7.5 In.

      Engine Compressor

        Face Diameter

        Engine Length

   F100PW229

      Thrust

29,000 Lb Class

34.8 In.

208 In.

32 FT 10 IN.

OVERALL SPAN W/MISSILES

*

Add 3 inches for AIM-120 missiles

*

      Engine Compressor

        Face Diameter

        Engine Length

   F110-GE-129

      Thrust

29,500 Lb Class

35.8 In.

183.76 In.

Figure 11.(Sheet 2)

GR1F-16CJ-1-0005X37

General Arrangement (Typical)

Air Data (Pitot) Probe

Nose Radome

AOA Probe

AOA Transmitter

Forward Electronic Equipment Bay

Cockpit Pressure Regulator

Cockpit Pressure Safety Valve

HUD/ASHM

Instrument Panel

Canopy (Movable)

Ejection Seat

Canopy (Fixed)

AIM-9 Missile

Missile Launcher

AR and Formation Light

Position/Formation Light

Static Discharger

LEF Drive Unit

Hydraulic Reservoir

AR Slipway

FLCS Accumulators

Anticollision Strobe Light Power Supply

Vertical Tail Attachment Fittings

Vertical Tail

Vertical Tail-Mounted Floodlight

Anticollision Strobe Light

Rudder

Position Light

Rudder ISA

Turbofan Engine

Speedbrake

Speedbrake Actuator

Chaff/Flare Dispenser

Horizontal Tail ISA

Horizontal Tail

Formation Light

Flaperon ISA

Hook

Flaperon

Wing Structural Box

Fixed Trailing Edge Panel

Asymmetry Brake

LEF Rotary Actuator

LEF Torque Shaft

LEF

Wing Attachment Fittings

MLG

MLG Door

LEF Angle Drive Gearbox

Air-Conditioning Package

M61A1 20MM Gun

Ammunition Drum

EPU Nitrogen Bottle

Gun Port

NLG Door

Position Light

NLG

Engine Air Inlet

Left Console

Throttle

Strake

Lower Equipment Compartment

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.

30.

31.

32.

33.

34.

35.

36.

37.

38.

39.

40.

41.

42.

43.

44.

45.

46.

47.

48.

49.

50.

51.

52.

53.

54.

55.

56.

57.

58.

59.

60.

61.

62.

63.

D

C

8

11 8

11

15

1

2

34

5

7

8

4

3

63

9 10 11

12

13 14

15

62 61

60

59

56

55

54 53

52 51 50

17

18

16

19

20

21

22

23

24

25

26

17

27

29

30

31

32

33

34 17

35

36

37

38

39

40

41

42

17

13

16

14

43

44

44

45

46

44

47

48

44

49

6

58 57

For antenna locations, refer

to ANTENNA LOCATIONS,

this section.

28

Drag Chute Fairing

29.

T.

O

. GR1F

16CJ

1

110

Figure 12.

T.O. GR1F16CJ1

111

LEFT

AUXILIARY

CONSOLE

THROTTLE

LEFT

CONSOLE

STICK

RIGHT

AUXILIARY

CONSOLE

RIGHT

CONSOLE

DF

DF

DF

Cockpit Arrangement        (Typical)

DF

C

GR1F-16CJ-1-0006A37

INSTRUMENT

PANEL

DF

PX II

Figure

 13.(Sheet 1)

T.O. GR1F16CJ1

112

LEFT CONSOLE

Cockpit Arrangement        (Typical)

DF

C

GR1F-16CJ-1-0007A37

DF

DF

23

22

1

2

3

4
5

6

7

8

9

10

12

14

16

15

19

18

21

20

17

13

11

24

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

AUX COMM 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 II

Figure

 13.(Sheet 2)

T.O. GR1F16CJ1

113

Cockpit Arrangement        (Typical)

DF

C

GR1F-16CJ-1-0008A37

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

RF Transmit 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.

10.

Magnetic Compass

FUEL Quantity Indicator

Pilot Fault List Display

System A HYD PRESS Indicator

System B HYD PRESS Indicator

Caution Light Panel

LIQUID OXYGEN Quantity Indicator

EPU FUEL Quantity Indicator

Cockpit Pressure Altimeter

Clock

1

2

4

5

7

8

10

9

6

3

DF

PX II

Figure

 13.(Sheet 3)

T.O. GR1F16CJ1

114

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 Warning Light (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

ALT REL Button

LASER ARM Switch

35. IFF IDENT Button

36. DRAG CHUTE Switch

37. RWR Prime Control Panel

38. Azimuth Display/Indicator

39. F-ACK Button

40. TF FAIL Warning Light (Red)

41. 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

42

41

2

39

32

34

DF

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.

34.

DF

C

29

30

31

36

42. ECM Light (Green),      ECM (Green)

DF

DF

INSTRUMENT PANEL

Cockpit Arrangement        (Typical)

DF

C

GR1F-16CJ-1-0009A37

    and OVRD (Amber) Light

PX II

Figure

 13.(Sheet 4)

T.O. GR1F16CJ1

115

RIGHT CONSOLE

Cockpit Arrangement        (Typical)

DF

C

GR1F-16CJ-1-0010A37

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

OXYGEN REGULATOR Panel

DTU Control Panel

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 II

Figure

 13.(Sheet 5)

 

 

 

 

 

 

 

 

Content      ..     1      2      3      4      ..