F16C/D. FLIGHT MANUAL (2002) - page 77

 

  Index      Manuals     F16C/D. FLIGHT MANUAL (2002)

 

Search            copyright infringement  

 

   

 

    

 

Content      ..     75      76      77      78     ..

 

 

 

F16C/D. FLIGHT MANUAL (2002) - page 77

 

 

T.O. GR1F16CJ11

B864Change 3

Turn Performance    50,000 Feet

DATA BASIS: FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MAX AB

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 0

GW = 22,000 POUNDS

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

1F-16CJ-1-1-4083A

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

(5.9 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

8877 FEET)

MAXIMUM AIRSPEED

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

  TURN RA

TE

(DEGREES/SECOND)

3
2

1

-1

-2
-3

10

20

-20

-10

TEMP DEV FROM

STD DAY    C

TEMPERATURE EFFECT

22

24

26

28

MAX AFT STICK

Figure B847.

T.O. GR1F16CJ11

Change 3B865

Turn Performance    Sea Level

DATA BASIS: FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MAX AB

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 50

GW = 26,000 POUNDS

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

1F-16CJ-1-1-4084A

-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

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

1.4

QUICKEST TURN

(22.6 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

1320 FEET)

MAXIMUM AIRSPEED

32

Figure B848.

T.O. GR1F16CJ11

B866Change 3

Turn Performance    10,000 Feet

DATA BASIS: FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MAX AB

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 50

GW = 26,000 POUNDS

26

28

30

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

IF-16CJ-1-1-4085A

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

  TURN RA

TE

(DEGREES/SECOND)

3
2

1

-1

-2
-3

10

20

-20

-10

TEMP DEV FROM

STD DAY    C

TEMPERATURE EFFECT

24

20

16

12

8

4

0

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

0.2

0.4

0.6

0.8

1.0

1.2

1.4

QUICKEST TURN

(19.0 DEGREES/SECOND)

MAXIMUM AIRSPEED

TIGHTEST TURN

(RADIUS =

1935 FEET)

32

Figure B849.

T.O. GR1F16CJ11

Change 3B867

Turn Performance    20,000 Feet

DATA BASIS: FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MAX AB

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 50

GW = 26,000 POUNDS

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

1F-16CJ-1-1-4086A

-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

24

20

16

12

8

4

0

0.2

0.4

0.6

0.8

1.0

1.2

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.4

1.6

TIGHTEST TURN

(RADIUS =

2848 FEET)

QUICKEST TURN

(16.0 DEGREES/SECOND)

MAXIMUM AIRSPEED

32

Figure B850.

T.O. GR1F16CJ11

B868Change 3

1F-16CJ-1-1-4087A

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

1.0

1.2

0

4

8

12

16

20

24

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 =

QUICKEST TURN

(12.8 DEGREES/SECOND)

Turn Performance    30,000 Feet

DATA BASIS: FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MAX AB

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

4223 FEET)

MAX AFT STICK

32

Figure B851.

T.O. GR1F16CJ11

Change 3B869

1F-16CJ-1-1-4088A

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

TIGHTEST TURN

(RADIUS =

QUICKEST TURN

(8.2 DEGREES/SECOND)

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    40,000 Feet

DATA BASIS FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MAX AB

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 50

GW = 26,000 POUNDS

2.0

-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

32

6452 FEET)

MAX AFT STICK

Figure B852.

T.O. GR1F16CJ11

B870Change 3

1F-16CJ-1-1-4089A

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

(22.6 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

1321 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    Sea Level

DATA BASIS FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MAX AB

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 100

GW = 26,000 POUNDS

-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

Figure B853.

T.O. GR1F16CJ11

Change 3B871

1F-16CJ-1-1-4090A

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

MAX AB

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 100

GW = 26,000 POUNDS

  TURN RA

TE

(DEGREES/SECOND)

3
2

1

-1

-2
-3

10

20

-20

-10

TEMP DEV FROM

STD DAY    C

TEMPERATURE EFFECT

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

26

30

34

38

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

1.4

QUICKEST TURN

(18.9 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

1936 FEET)

MAXIMUM AIRSPEED

Figure B854.

T.O. GR1F16CJ11

B872Change 3

1F-16CJ-1-1-4091A

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

1.1

1.0

0.9

TURN RADIUS F

ACTOR

RADIUS TEMP EFFECT

TEMP DEV FROM STD DAY   C

-20

-10

0

10

20

QUICKEST TURN

(15.9 DEGREES/SECOND)

MAXIMUM AIRSPEED

Turn Performance    20,000 Feet

DATA BASIS FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MAX AB

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 100

GW = 26,000 POUNDS

TIGHTEST TURN

(RADIUS =

2848 FEET)

  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

26

30

34

38

3
2

1

-1

-2
-3

10

20

-20

-10

Figure B855.

T.O. GR1F16CJ11

Change 3B873

1F-16CJ-1-1-4092A

-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

1.0

1.2

0

4

8

12

16

20

24

0.2

0.4

0.6

0.8

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.4

1.6

1.8

MAXIMUM AIRSPEED

QUICKEST TURN

(12.8 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

4224 FEET)

Turn Performance    30,000 Feet

DATA BASIS FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MAX AB

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 100

GW = 26,000 POUNDS

MAX AFT STICK

Figure B856.

T.O. GR1F16CJ11

B874Change 3

1F-16CJ-1-1-4093A

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

(21.6 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

1450 FEET)

Turn Performance    Sea Level

DATA BASIS FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MAX AB

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 150

GW = 28,000 POUNDS

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

28

32

36

40

  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

3
2

1

-1

-2
-3

10

20

-20

-10

Figure B857.

T.O. GR1F16CJ11

Change 3B875

1F-16CJ-1-1-4094A

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

(18.2 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

2112 FEET)

MAXIMUM AIRSPEED

Turn Performance    10,000 Feet

DATA BASIS FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MAX AB

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 150

GW = 28,000 POUNDS

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

28

32

36

40

  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

3
2

1

-1

-2
-3

10

20

-20

-10

Figure B858.

T.O. GR1F16CJ11

B876Change 3

1F-16CJ-1-1-4095A

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

MAXIMUM AIRSPEED

TIGHTEST TURN

(RADIUS =

3095 FEET)

QUICKEST TURN

(15.3 DEGREES/SECOND)

Turn Performance    20,000 Feet

DATA BASIS FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MAX AB

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 150

GW = 28,000 POUNDS

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

28

32

36

40

  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

3
2

1

-1

-2
-3

10

20

-20

-10

Figure B859.

T.O. GR1F16CJ11

Change 3B877

1F-16CJ-1-1-4104X

1.0

1.2

0

4

8

12

16

20

24

0.2

0.4

0.6

0.8

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.4

1.6

MAXIMUM AIRSPEED

QUICKEST TURN

(11.9 DEGREES/SECOND)

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

35

33

31

29

  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    30,000 Feet

DATA BASIS FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MAX AB

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 150

GW = 28,000 POUNDS

TIGHTEST TURN

(RADIUS =

4569 FEET)

MAX AFT STICK

3
2

1

-1

-2
-3

10

20

-20

-10

Figure B860.

T.O. GR1F16CJ11

B878Change 3

1F-16CJ-1-1-4096A

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

(21.6 DEGREES/SECOND)

MAXIMUM AIRSPEED

TIGHTEST TURN

(RADIUS =

1450 FEET)

Turn Performance    Sea Level

DATA BASIS FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MAX AB

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 200

GW = 28,000 POUNDS

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

28

32

36

40

  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

3
2

1

-1

-2
-3

10

20

-20

-10

Figure B861.

T.O. GR1F16CJ11

Change 3B879

1F-16CJ-1-1-4097A

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 =

2112 FEET)

QUICKEST TURN

(18.2 DEGREES/SECOND)

Turn Performance    10,000 Feet

DATA BASIS FLIGHT TEST

CONFIGURATION:

CONDITIONS:

ENGINE F110-GE-129

STANDARD DAY

MAX AB

NOTE:  REFER TO SECTION V FOR AIRSPEED LIMITATIONS.

DRAG INDEX = 200

GW = 28,000 POUNDS

-4

-2

0

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

28

32

36

40

  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

3
2

1

-1

-2
-3

10

20

-20

-10

Figure B862.

 

 

 

 

 

 

 

Content      ..     75      76      77      78     ..