F16C/D. FLIGHT MANUAL (2002) - page 87

T.O. GR1F16CJ11

C846Change 7

1F-16CJ-1-1-1054X37

Turn Performance    10,000 Feet

DATA BASIS ESTIMATED

CONFIGURATION:

CONDITIONS:

ENGINE F100-PW-229/CFT

STANDARD DAY

MIL

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 0

GW = 22,000 POUNDS

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

22

24

26

24

20

16

12

8

4

0

0.0

0.2

0.4

0.6

0.8

1.0

1.2

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

QUICKEST TURN

(20.2 DEGREES/SECOND)

MAXIMUM AIRSPEED

TIGHTEST TURN

(RADIUS =

1836 FEET)

28

30

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

  TURN RA

TE

(DEGREES/SECOND)

TEMPERATURE EFFECT

TEMP DEV FROM

STD DAY    C

3
2

1

-1

-2
-3

10

20

-20

-10

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

Figure C816.

T.O. GR1F16CJ11

Change 7C847

1F-16CJ-1-1055X37

0.8

1.0

0

4

8

12

16

20

24

0

0.2

0.4

0.6

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.2

QUICKEST TURN

(18.5 DEGREES/SECOND)

MAXIMUM AIRSPEED

TIGHTEST TURN

(RADIUS =

2181 FEET)

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

22

24

26

Turn Performance    15,000 Feet

DATA BASIS ESTIMATED

CONFIGURATION:

CONDITIONS:

ENGINE F100-PW-229/CFT

STANDARD DAY

MIL

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 0

GW = 22,000 POUNDS

28

30

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

  TURN RA

TE

(DEGREES/SECOND)

TEMPERATURE EFFECT

TEMP DEV FROM

STD DAY    C

3
2

1

-1

-2
-3

10

20

-20 -10

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

Figure C817.

T.O. GR1F16CJ11

C848Change 7

1F-16CJ-1-1-1056X37

0.8

1.0

0

4

8

12

16

20

24

0

0.2

0.4

0.6

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.2

QUICKEST TURN

(17.0 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

2605 FEET)

MAXIMUM AIRSPEED

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

22

24

26

Turn Performance    20,000 Feet

DATA BASIS ESTIMATED

CONFIGURATION:

CONDITIONS:

ENGINE F100-PW-229/CFT

STANDARD DAY

MIL

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 0

GW = 22,000 POUNDS

28

30

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

  TURN RA

TE

(DEGREES/SECOND)

TEMPERATURE EFFECT

TEMP DEV FROM

STD DAY    C

3
2

1

-1

-2
-3

10

20

-20

-10

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

Figure C818.

T.O. GR1F16CJ11

Change 7C849

1F-16CJ-1-1-1057X37

0.8

1.0

0

4

8

12

16

20

24

0

0.2

0.4

0.6

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.2

MAXIMUM AIRSPEED

QUICKEST TURN

(15.5 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

3125 FEET)

Turn Performance    25,000 Feet

DATA BASIS ESTIMATED

CONFIGURATION:

CONDITIONS:

ENGINE F100-PW-229/CFT

STANDARD DAY

MIL

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 0

GW = 22,000 POUNDS

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

22

24

26

28

28

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

  TURN RA

TE

(DEGREES/SECOND)

TEMPERATURE EFFECT

TEMP DEV FROM

STD DAY    C

3
2

1

-1

-2
-3

10

20

-20 -10

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

Figure C819.

T.O. GR1F16CJ11

C850Change 7

1F-16CJ-1-1-1058X37

0.8

1.0

0

4

8

12

16

20

24

0

0.2

0.4

0.6

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.2

Turn Performance    30,000 Feet

DATA BASIS ESTIMATED

CONFIGURATION:

CONDITIONS:

ENGINE F100-PW-229/CFT

STANDARD DAY

MIL

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 0

GW = 22,000 POUNDS

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

22

24

26

28

30

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

  TURN RA

TE

(DEGREES/SECOND)

TEMPERATURE EFFECT

TEMP DEV FROM

STD DAY    C

3
2

1

-1

-2
-3

10

20

-20 -10

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

QUICKEST TURN

(13.9 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

3795 FEET)

MAXIMUM AIRSPEED

Figure C820.

T.O. GR1F16CJ11

Change 7C851

1F-16CJ-1-1-1059X37

0.8

1.0

0

4

8

12

16

20

24

0

0.2

0.4

0.6

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.2

QUICKEST TURN

(22.1 DEGREES/SECOND)

MAXIMUM AIRSPEED

TIGHTEST TURN

(RADIUS =

1580 FEET)

Turn Performance    Sea Level

DATA BASIS ESTIMATED

CONFIGURATION:

CONDITIONS:

ENGINE F100-PW-229/CFT

STANDARD DAY

MIL

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 50

GW = 26,000 POUNDS

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

26

28

30

32

34

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

  TURN RA

TE

(DEGREES/SECOND)

TEMPERATURE EFFECT

TEMP DEV FROM

STD DAY    C

3
2

1

-1

-2
-3

10

20

-20

-10

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

Figure C821.

T.O. GR1F16CJ11

C852Change 7

1F-16CJ-1-1-1060X37

0.8

1.0

0

4

8

12

16

20

24

0

0.2

0.4

0.6

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.2

MAXIMUM AIRSPEED

QUICKEST TURN

(18.4 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

2195 FEET)

Turn Performance    10,000 Feet

DATA BASIS ESTIMATED

CONFIGURATION:

CONDITIONS:

ENGINE F100-PW-229/CFT

STANDARD DAY

MIL

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 50

GW = 26,000 POUNDS

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

26

28

30

32

34

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

  TURN RA

TE

(DEGREES/SECOND)

TEMPERATURE EFFECT

TEMP DEV FROM

STD DAY    C

3
2

1

-1

-2
-3

10

20

-20

-10

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

Figure C822.

T.O. GR1F16CJ11

Change 7C853

1F-16CJ-1-1-1061X37

0.8

1.0

0

4

8

12

16

20

24

0

0.2

0.4

0.6

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.2

MAXIMUM AIRSPEED

QUICKEST TURN

(15.6 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

3100 FEET)

CONFIGURATION:

CONDITIONS:

STANDARD DAY

MIL

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 50

GW = 26,000 POUNDS

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

26

28

30

  TURN RA

TE

(DEGREES/SECOND)

3
2

1

-1

-2
-3

10

20

-20

-10

TEMP DEV FROM

STD DAY    C

TEMPERATURE EFFECT

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

32

34

Turn Performance    20,000 Feet

ENGINE F100-PW-229/CFT

DATA BASIS ESTIMATED

Figure C823.

T.O. GR1F16CJ11

C854Change 7

1F-16CJ-1-1-1062X37

0.8

1.0

0

4

8

12

16

20

24

0

0.2

0.4

0.6

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.2

MAXIMUM AIRSPEED

QUICKEST TURN

(11.8 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

4545 FEET)

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

26

28

30

  TURN RA

TE

(DEGREES/SECOND)

3
2

1

-1

-2
-3

10

20

-20

-10

TEMP DEV FROM

STD DAY    C

TEMPERATURE EFFECT

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

Turn Performance    30,000 Feet

DATA BASIS ESTIMATED

CONFIGURATION:

CONDITIONS:

ENGINE F100-PW-229/CFT

STANDARD DAY

MIL

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 50

GW = 26,000 POUNDS

1

2

3

4

5

6

-2000

-1600

32

34

Figure C824.

T.O. GR1F16CJ11

Change 7C855

1F-16CJ-1-1-1063X37

0.8

1.0

0

4

8

12

16

20

24

0

0.2

0.4

0.6

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.2

MAXIMUM AIRSPEED

TIGHTEST TURN

(RADIUS =

1580 FEET)

QUICKEST TURN

(22.0 DEGREES/SECOND)

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

26

30

34

38

  TURN RA

TE

(DEGREES/SECOND)

3
2

1

-1

-2
-3

10

20

-20

-10

TEMP DEV FROM

STD DAY    C

TEMPERATURE EFFECT

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

Turn Performance    Sea Level

DATA BASIS ESTIMATED

CONFIGURATION:

ENGINE F100-PW-229/CFT

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 100

GW = 26,000 POUNDS

CONDITIONS:

STANDARD DAY

MIL

42

Figure C825.

T.O. GR1F16CJ11

C856Change 7

1F-16CJ-1-1-1064X37

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

26

30

34

38

  TURN RA

TE

(DEGREES/SECOND)

3
2

1

-1

-2
-3

10

20

-20

-10

TEMP DEV FROM

STD DAY    C

TEMPERATURE EFFECT

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

0.8

1.0

0

4

8

12

16

20

24

0

0.2

0.4

0.6

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.2

TIGHTEST TURN

(RADIUS =

QUICKEST TURN

(18.4 DEGREES/SECOND)

Turn Performance    10,000 Feet

CONFIGURATION:

CONDITIONS:

ENGINE F100-PW-229/CFT

STANDARD DAY

MIL

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 100

GW = 26,000 POUNDS

MAXIMUM AIRSPEED

2195 FEET)

DATA BASIS ESTIMATED

42

Figure C826.

T.O. GR1F16CJ11

Change 7C857

1F-16CJ-1-1-1065X37

0.8

1.0

0

4

8

12

16

20

24

0

0.2

0.4

0.6

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.2

MAXIMUM AIRSPEED

TIGHTEST TURN

(RADIUS =

QUICKEST TURN

(15.6 DEGREES/SECOND)

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

26

30

34

38

  TURN RA

TE

(DEGREES/SECOND)

3
2

1

-1

-2
-3

10

20

-20

-10

TEMP DEV FROM

STD DAY    C

TEMPERATURE EFFECT

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

Turn Performance    20,000 Feet

DATA BASIS ESTIMATED

CONFIGURATION:

CONDITIONS:

ENGINE F100-PW-229/CFT

STANDARD DAY

MIL

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 100

GW = 26,000 POUNDS

3100 FEET)

42

Figure C827.

T.O. GR1F16CJ11

C858Change 7

1F-16CJ-1-1-1066X37

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

26

30

34

38

  TURN RA

TE

(DEGREES/SECOND)

3
2

1

-1

-2
-3

10

20

-20

-10

TEMP DEV FROM

STD DAY    C

TEMPERATURE EFFECT

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

0.8

1.0

0

4

8

12

16

20

24

0

0.2

0.4

0.6

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.2

TIGHTEST TURN

(RADIUS =

QUICKEST TURN

(11.6 DEGREES/SECOND)

MAXIMUM AIRSPEED

Turn Performance    30,000 Feet

DATA BASIS ESTIMATED

CONFIGURATION:

CONDITIONS:

ENGINE F100-PW-229/CFT

STANDARD DAY

MIL

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 100

GW = 26,000 POUNDS

4545 FEET)

42

Figure C828.

T.O. GR1F16CJ11

Change 7C859

1F-16CJ-1-1-1067X37

0.8

1.0

0

4

8

12

16

20

24

0

0.2

0.4

0.6

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.2

TIGHTEST TURN

(RADIUS =

1712 FEET)

QUICKEST TURN

(21.1 DEGREES/SECOND)

MAXIMUM AIRSPEED

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

28

32

36

40

  TURN RA

TE

(DEGREES/SECOND)

3
2

1

-1

-2
-3

10

20

-20

-10

TEMP DEV FROM

STD DAY    C

TEMPERATURE EFFECT

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

Turn Performance    Sea Level

DATA BASIS ESTIMATED

CONFIGURATION:

CONDITIONS:

ENGINE F100-PW-229/CFT

STANDARD DAY

MIL

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 150

GW = 28,000 POUNDS

44

Figure C829.

T.O. GR1F16CJ11

C860Change 7

1F-16CJ-1-1-1068X37

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

28

32

36

40

  TURN RA

TE

(DEGREES/SECOND)

3
2

1

-1

-2
-3

10

20

-20

-10

TEMP DEV FROM

STD DAY    C

TEMPERATURE EFFECT

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

0.8

1.0

0

4

8

12

16

20

24

0

0.2

0.4

0.6

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.2

QUICKEST TURN

(17.7 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

MAXIMUM AIRSPEED

Turn Performance    10,000 Feet

DATA BASIS ESTIMATED

CONFIGURATION:

CONDITIONS:

ENGINE F100-PW-229/CFT

STANDARD DAY

MIL

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 150

GW = 28,000 POUNDS

2374 FEET)

44

Figure C830.

T.O. GR1F16CJ11

Change 7C861

1F-16CJ-1-1-1069X37

0.8

1.0

0

4

8

12

16

20

24

0

0.2

0.4

0.6

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.2

MAXIMUM AIRSPEED

QUICKEST TURN

(14.7 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

3351 FEET)

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

40

36

32

28

  TURN RA

TE

(DEGREES/SECOND)

3
2

1

-1

-2
-3

10

20

-20

-10

TEMP DEV FROM

STD DAY    C

TEMPERATURE EFFECT

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

Turn Performance    20,000 Feet

DATA BASIS ESTIMATED

CONFIGURATION:

CONDITIONS:

ENGINE F100-PW-229/CFT

STANDARD DAY

MIL

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 150

GW = 28,000 POUNDS

44

Figure C831.