F16C/D. FLIGHT MANUAL (2002) - page 75

 

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F16C/D. FLIGHT MANUAL (2002) - page 75

 

 

T.O. GR1F16CJ11

B832Change 3

1F-16CJ-1-1-4053A

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

(22.2 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

1442 FEET)

MAXIMUM AIRSPEED

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

22

24

26

  TURN RA

TE

(DEGREES/SECOND)

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 FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MIL

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 0

GW = 22,000 POUNDS

28

3
2

1

-1

-2
-3

10

20

-20

-10

Figure B815.

T.O. GR1F16CJ11

Change 3B833

1F-16CJ-1-1-4054A

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 FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

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

  TURN RA

TE

(DEGREES/SECOND)

TEMP DEV FROM

STD DAY    C

TEMPERATURE EFFECT

24

20

16

12

8

4

0

0

0.2

0.4

0.6

0.8

1.0

1.2

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

QUICKEST TURN

(20.4 DEGREES/SECOND)

MAXIMUM AIRSPEED

TIGHTEST TURN

(RADIUS =

1723 FEET)

28

3
2

1

-1

-2
-3

10

20

-20

-10

Figure B816.

T.O. GR1F16CJ11

B834Change 3

1F-16CJ-1-1-4055A

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

(18.7 DEGREES/SECOND)

MAXIMUM AIRSPEED

TIGHTEST TURN

(RADIUS =

2065 FEET)

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

22

24

26

  TURN RA

TE

(DEGREES/SECOND)

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 FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MIL

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 0

GW = 22,000 POUNDS

28

3
2

1

-1

-2
-3

10

20

-20

-10

Figure B817.

T.O. GR1F16CJ11

Change 3B835

1F-16CJ-1-1-4056A

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

(17.1 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

2486 FEET)

MAXIMUM AIRSPEED

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 RA

TE

(DEGREES/SECOND)

TEMP DEV FROM

STD DAY    C

TEMPERATURE EFFECT

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

22

24

26

Turn Performance    20,000 Feet

DATA BASIS FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MIL

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 0

GW = 22,000 POUNDS

28

3
2

1

-1

-2
-3

10

20

-20

-10

Figure B818.

T.O. GR1F16CJ11

B836Change 3

1F-16CJ-1-1-4057A

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 =

3005 FEET)

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 FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

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

  TURN RA

TE

(DEGREES/SECOND)

TEMP DEV FROM

STD DAY    C

TEMPERATURE EFFECT

28

3
2

1

-1

-2
-3

10

20

-20

-10

Figure B819.

T.O. GR1F16CJ11

Change 3B837

1F-16CJ-1-1-4058A

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

(14.2 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

3651 FEET)

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 FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

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

  TURN RA

TE

(DEGREES/SECOND)

3
2

1

-1

-2
-3

10

20

-20

-10

TEMP DEV FROM

STD DAY    C

TEMPERATURE EFFECT

28

Figure B820.

T.O. GR1F16CJ11

B838Change 3

1F-16CJ-1-1-4059A

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

(22.0 DEGREES/SECOND)

MAXIMUM AIRSPEED

TIGHTEST TURN

(RADIUS =

1466 FEET)

Turn Performance    Sea Level

DATA BASIS FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

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

Figure B821.

T.O. GR1F16CJ11

Change 3B839

1F-16CJ-1-1-4060A

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

(18.6 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

2074 FEET)

Turn Performance    10,000 Feet

DATA BASIS FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

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

Figure B822.

T.O. GR1F16CJ11

B840Change 3

1F-16CJ-1-1-4061A

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

(15.7 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

2977 FEET)

Turn Performance    20,000 Feet

DATA BASIS FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

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

Figure B823.

T.O. GR1F16CJ11

Change 3B841

1F-16CJ-1-1-4062A

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

(12.3 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

4348 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 FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

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

Figure B824.

T.O. GR1F16CJ11

B842Change 3

1F-16CJ-1-1-4063A

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 =

1466 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 FLIGHT TEST

CONFIGURATION:

ENGINE F110-GE-129

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 100

GW = 26,000 POUNDS

CONDITIONS:

STANDARD DAY

MIL

Figure B825.

T.O. GR1F16CJ11

Change 3B843

1F-16CJ-1-1-4064A

-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

(18.6 DEGREES/SECOND)

Turn Performance    10,000 Feet

DATA BASIS FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MIL

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 100

GW = 26,000 POUNDS

MAXIMUM AIRSPEED

2074 FEET)

Figure B826.

T.O. GR1F16CJ11

B844Change 3

1F-16CJ-1-1-4065A

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

(15.7 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 FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MIL

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 100

GW = 26,000 POUNDS

2977 FEET)

Figure B827.

T.O. GR1F16CJ11

Change 3B845

1F-16CJ-1-1-4066A

-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

(12.1 DEGREES/SECOND)

MAXIMUM AIRSPEED

Turn Performance    30,000 Feet

DATA BASIS FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MIL

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 100

GW = 26,000 POUNDS

4349 FEET)

Figure B828.

T.O. GR1F16CJ11

B846Change 3

1F-16CJ-1-1-4067A

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 =

1595 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 FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MIL

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 150

GW = 28,000 POUNDS

Figure B829.

T.O. GR1F16CJ11

Change 3B847

1F-16CJ-1-1-4068A

-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

(17.9 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

MAXIMUM AIRSPEED

Turn Performance    10,000 Feet

DATA BASIS FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MIL

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 150

GW = 28,000 POUNDS

2250 FEET)

Figure B830.

 

 

 

 

 

 

 

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