F16C/D. FLIGHT MANUAL (2002) - page 88

 

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F16C/D. FLIGHT MANUAL (2002) - page 88

 

 

T.O. GR1F16CJ11

C862Change 7

1F-16CJ-1-1-1070X37

0.8

1.0

0

4

8

12

16

20

24

0.0

0.2

0.4

0.6

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.2

MAXIMUM AIRSPEED

QUICKEST TURN

(10.5 DEGREES/ SECOND)

TIGHTEST TURN

(RADIUS =

4929 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    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 = 150

GW = 28,000 POUNDS

44

Figure C832.

T.O. GR1F16CJ11

Change 7C863

1F-16CJ-1-1-1071X37

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 =

1712 FEET)

QUICKEST TURN

(21.0 DEGREES/SECOND)

-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    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 = 200

GW = 28,000 POUNDS

44

Figure C833.

T.O. GR1F16CJ11

C864Change 7

1F-16CJ-1-1-1072X37

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

(17.7 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

2374 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    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 = 200

GW = 28,000 POUNDS

44

Figure C834.

T.O. GR1F16CJ11

Change 7C865

1F-16CJ-1-1-1073X37

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

(14.7 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    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 = 200

GW = 28,000 POUNDS

3351 FEET)

44

Figure C835.

T.O. GR1F16CJ11

C866Change 7

1F-16CJ-1-1-1074X37

0.8

1.0

0

4

8

12

16

20

24

0.0

0.2

0.4

0.6

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.2

QUICKEST TURN

(10.3 DEGREES/SECOND)

MAXIMUM AIRSPEED

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

28

32

36

44

  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 = 200

GW = 28,000 POUNDS

TIGHTEST TURN

(RADIUS =

4929 FEET)

40

Figure C836.

T.O. GR1F16CJ11

Change 7C867

1F-16CJ-1-1-1075X37

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

1.4

LIMIT AIRSPEED

QUICKEST TURN

(24.8 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

1189 FEET)

C

H

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

22

24

26

D

E

  TURN RA

TE

(DEGREES/SECOND)

3
2

1

-1

-2
-3

10

20

-20

-10

TEMP DEV FROM

STD DAY    C

TEMPERATURE EFFECT

F

A

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

J

Turn Performance    Sea Level

DATA BASIS ESTIMATED

CONFIGURATION:

CONDITIONS:

ENGINE F100-PW-229/CFT

STANDARD DAY

MAX AB

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 0

GW = 22,000 POUNDS

F

28

A

B

I

A

G

30

Figure C837.

T.O. GR1F16CJ11

C868Change 7

1F-16CJ-1-1-1076X37

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

1.4

TIGHTEST TURN

(RADIUS =

1439 FEET)

QUICKEST TURN

(22.8 DEGREES/SECOND)

LIMIT AIRSPEED

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

22

24

26

  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    5000 Feet

DATA BASIS ESTIMATED

CONFIGURATION:

CONDITIONS:

ENGINE F100-PW-229/CFT

STANDARD DAY

MAX AB

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 0

GW = 22,000 POUNDS

28

30

Figure C838.

T.O. GR1F16CJ11

Change 7C869

1F-16CJ-1-1-1077X37

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

1.4

1.6

LIMIT AIRSPEED

TIGHTEST TURN

(RADIUS =

1719 FEET)

QUICKEST TURN

(20.6 DEGREES/SECOND)

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

22

24

26

  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    10,000 Feet

DATA BASIS ESTIMATED

CONFIGURATION:

CONDITIONS:

ENGINE F100-PW-229/CFT

STANDARD DAY

MAX AB

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 0

GW = 22,000 POUNDS

-800

28

30

Figure C839.

T.O. GR1F16CJ11

C870Change 7

1F-16CJ-1-1-1078X37

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

1.4

1.6

LIMIT AIRSPEED

QUICKEST TURN

(18.8 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

22

24

26

  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    15,000 Feet

DATA BASIS ESTIMATED

CONFIGURATION:

CONDITIONS:

ENGINE F100-PW-229/CFT

STANDARD DAY

MAX AB

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 0

GW = 22,000 POUNDS

28

2078 FEET)

GW EFFECT

30

Figure C840.

T.O. GR1F16CJ11

Change 7C871

1F-16CJ-1-1-1079X37

0.8

1.0

0

4

8

12

16

20

24

0.2

0.4

0.6

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.2

1.4

1.6

LIMIT AIRSPEED

QUICKEST TURN

(17.3 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

2506 FEET)

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

22

24

26

  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

MAX AB

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 0

GW = 22,000 POUNDS

1.8

28

GW EFFECT

30

Figure C841.

T.O. GR1F16CJ11

C872Change 7

1F-16CJ-1-1-1080X37

1.0

1.2

0

4

8

12

16

20

0.2

0.4

0.6

0.8

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.4

1.6

1.8

MAXIMUM AIRSPEED

TIGHTEST TURN

(RADIUS =

3028 FEET)

(15.8 DEGREES/SECOND)

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

22

24

26

  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    25,000 Feet

DATA BASIS ESTIMATED

CONFIGURATION:

CONDITIONS:

ENGINE F100-PW-229/CFT

STANDARD DAY

MAX AB

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 0

GW = 22,000 POUNDS

24

QUICKEST TURN

28

GW EFFECT

30

Figure C842.

T.O. GR1F16CJ11

Change 7C873

1F-16CJ-1-1-1081X37

1.0

1.2

0

4

8

12

16

20

24

0.4

0.6

0.8

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.4

1.6

1.8

MAXIMUM AIRSPEED

QUICKEST TURN

(14.1 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

3682 FEET)

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

22

24

26

  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

MAX AB

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 0

GW = 22,000 POUNDS

28

GW EFFECT

30

Figure C843.

T.O. GR1F16CJ11

C874Change 7

1F-16CJ-1-1-1082X37

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

22

24

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

0.8

1.0

0

4

8

12

16

20

24

1.8

0.4

0.6

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.2

1.4

1.6

QUICKEST TURN

(12.1 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

MAXIMUM AIRSPEED

Turn Performance    35,000 Feet

DATA BASIS ESTIMATED

CONFIGURATION:

CONDITIONS:

ENGINE F100-PW-229/CFT

STANDARD DAY

MAX AB

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 0

GW = 22,000 POUNDS

2.0

26

4538 FEET)

MAX AFT STICK

GW EFFECT

30

Figure C844.

T.O. GR1F16CJ11

Change 7C875

1F-16CJ-1-1-1083X37

0.8

1.0

0

4

8

12

16

20

24

1.8

0.4

0.6

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.2

1.4

1.6

2.0

MAXIMUM AIRSPEED

QUICKEST TURN

(9.5 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

5675 FEET)

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

26

24

22

Turn Performance    40,000 Feet

DATA BASIS ESTIMATED

CONFIGURATION:

CONDITIONS:

ENGINE F100-PW-229/CFT

STANDARD DAY

MAX AB

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 0

GW = 22,000 POUNDS

28

MAX AFT STICK

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 C845.

T.O. GR1F16CJ11

C876Change 7

Turn Performance    45,000 Feet

DATA BASIS ESTIMATED

CONFIGURATION:

CONDITIONS:

ENGINE F100-PW-229/CFT

STANDARD DAY

MAX AB

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

1F-16CJ-1-1-1084X37

24

20

16

12

8

4

0

0.4

0.6

0.8

1.0

1.2

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.4

1.6

1.8

2.0

TIGHTEST TURN

(RADIUS =

QUICKEST TURN

(7.4 DEGREES/SECOND)

MAXIMUM AIRSPEED

7169 FEET)

28

MAX AFT STICK

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 C846.

T.O. GR1F16CJ11

Change 7C877

Turn Performance    50,000 Feet

DATA BASIS ESTIMATED

CONFIGURATION:

CONDITIONS:

ENGINE F100-PW-229/CFT

STANDARD DAY

MAX AB

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 0

GW = 22,000 POUNDS

1F-16CJ-1-1-1085X37

24

20

16

12

8

4

0

0.4

0.6

0.8

1.0

1.2

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.4

1.6

1.8

2.0

QUICKEST TURN

(5.8 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

9177 FEET)

MAXIMUM AIRSPEED

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

MAX AFT STICK

-4

-2

0

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

Figure C847.

 

 

 

 

 

 

 

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