F16C/D. FLIGHT MANUAL (2002) - page 89

T.O. GR1F16CJ11

C878Change 7

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 = 50

GW = 26,000 POUNDS

1F-16CJ-1-1-1086X37

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW 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

(22.5 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

1469 FEET)

MAXIMUM AIRSPEED

-4

-2

0

26

28

30

2

1

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 C848.

T.O. GR1F16CJ11

Change 7C879

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 = 50

GW = 26,000 POUNDS

1F-16CJ-1-1-1087X37

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW 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

(18.7 DEGREES/SECOND)

MAXIMUM AIRSPEED

TIGHTEST TURN

(RADIUS =

2083 FEET)

-4

-2

0

26

28

30

32

34

1

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 C849.

T.O. GR1F16CJ11

C880Change 7

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 = 50

GW = 26,000 POUNDS

1F-16CJ-1-1-1088X37

24

20

16

12

8

4

0

0.1

0.3

0.5

0.7

0.9

1.1

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.3

1.5

TIGHTEST TURN

(RADIUS =

3001 FEET)

QUICKEST TURN

(15.8 DEGREES/SECOND)

MAXIMUM AIRSPEED

  TURN RA

TE

(DEGREE/SECOND)

GW   1000 POUNDS

GW EFFECT

-4

-2

0

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

1.7

Figure C850.

T.O. GR1F16CJ11

Change 7C881

1F-16CJ-1-1-1089X37

1.1

1.3

0

4

8

12

16

20

24

0.9

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.5

1.7

1.9

MAXIMUM AIRSPEED

TIGHTEST TURN

(RADIUS =

QUICKEST TURN

(12.7 DEGREES/SECOND)

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 = 50

GW = 26,000 POUNDS

4418 FEET)

MAX AFT STICK

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

-4

-2

0

26

28

30

32

34

0.7

0.5

0.3

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 C851.

T.O. GR1F16CJ11

C882Change 7

1F-16CJ-1-1-1090X37

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

(8.0 DEGREES/SECOND)

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 = 50

GW = 26,000 POUNDS

2.0

6668 FEET)

MAX AFT STICK

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

-4

-2

0

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 C852.

T.O. GR1F16CJ11

Change 7C883

1F-16CJ-1-1-1091X37

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

(22.5 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

1469 FEET)

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 = 100

GW = 26,000 POUNDS

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

-4

-2

0

26

30

34

38

42

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 C853.

T.O. GR1F16CJ11

C884Change 7

1F-16CJ-1-1-1092X37

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 = 100

GW = 26,000 POUNDS

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

(18.7 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

2083 FEET)

MAXIMUM AIRSPEED

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

-4

-2

0

26

30

34

38

42

2

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 C854.

T.O. GR1F16CJ11

Change 7C885

1F-16CJ-1-1-1093X37

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

QUICKEST TURN

(15.8 DEGREES/SECOND)

MAXIMUM AIRSPEED

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 = 100

GW = 26,000 POUNDS

TIGHTEST TURN

(RADIUS =

3001 FEET)

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

-4

-2

0

26

30

34

38

42

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 C855.

T.O. GR1F16CJ11

C886Change 7

1F-16CJ-1-1-1094X37

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

(12.7 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

4419 FEET)

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 = 100

GW = 26,000 POUNDS

MAX AFT STICK

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

-4

-2

0

26

30

34

38

42

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 C856.

T.O. GR1F16CJ11

Change 7C887

1F-16CJ-1-1-1095X37

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

(21.5 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

1606 FEET)

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 = 150

GW = 28,000 POUNDS

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

-4

-2

0

28

32

36

40

44

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 C857.

T.O. GR1F16CJ11

C888Change 7

1F-16CJ-1-1-1096X37

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

(18.0 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

2264 FEET)

MAXIMUM AIRSPEED

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 = 150

GW = 28,000 POUNDS

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

-4

-2

0

28

32

36

40

44

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 C858.

T.O. GR1F16CJ11

Change 7C889

1F-16CJ-1-1-1097X37

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 =

3249 FEET)

QUICKEST TURN

(15.1 DEGREES/SECOND)

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 = 150

GW = 28,000 POUNDS

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

-4

-2

0

28

32

36

40

44

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 C859.

T.O. GR1F16CJ11

C890Change 7

1F-16CJ-1-1-1098X37

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

(11.8 DEGREES/SECOND)

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 = 150

GW = 28,000 POUNDS

TIGHTEST TURN

(RADIUS =

4795 FEET)

MAX AFT STICK

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

-4

-2

0

28

32

36

40

44

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 C860.

T.O. GR1F16CJ11

Change 7C891

1F-16CJ-1-1-1099X37

0.8

1.0

0

4

8

12

16

20

0

0.2

0.4

0.6

MACH NUMBER

TURN RA

TE   DEGREES/SECOND

1.2

QUICKEST TURN

(21.5 DEGREES/SECOND)

TIGHTEST TURN

(RADIUS =

1606 FEET)

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 = 200

GW = 28,000 POUNDS

MAXIMUM AIRSPEED

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

-4

-2

0

28

32

36

40

44

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

24

Figure C861.

T.O. GR1F16CJ11

C892Change 7

1F-16CJ-1-1-1100X37

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 =

2264 FEET)

QUICKEST TURN

(18.0 DEGREES/SECOND)

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 = 200

GW = 28,000 POUNDS

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

-4

-2

0

28

32

36

40

44

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 C862.

T.O. GR1F16CJ11

Change 7C893

1F-16CJ-1-1-1101X37

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 =

3249 FEET)

MAXIMUM AIRSPEED

QUICKEST TURN

(15.1 DEGREES/SECOND)

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 = 200

GW = 28,000 POUNDS

1.4

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

-4

-2

0

28

32

36

40

44

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 C863.

T.O. GR1F16CJ11

C894Change 7

1F-16CJ-1-1-1102X37

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

TIGHTEST TURN

(RADIUS =

4795 FEET)

MAXIMUM AIRSPEED

QUICKEST TURN

(11.3 DEGREES/SECOND)

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 = 200

GW = 28,000 POUNDS

1.4

  TURN RA

TE

(DEGREES/SECOND)

GW   1000 POUNDS

GW EFFECT

-4

-2

0

28

32

36

40

44

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 C864.

T.O. GR1F16CJ11

Change 7C895

1F-16CJ-1-1-1103X_37

INITIAL MACH NUMBER

GW   1000 POUNDS

TIME   MINUTES

DIST

ANCE   NM

0.6

0.8

1.0

1.2

1.4

1.6 24

28

32

36

40

BASELINE

0

40

80

120

FUEL USED   POUNDS

0

5

10

15

20

25

0

0.5

1.0

1.5

2.0

2.5

3.0

0.6

0.8

1.0

1.2

1.4

1.6

0.6

0.8

1.0

1.2

1.4

1.6

BASELINE

BASELINE

Deceleration    20,000 Feet

DATA BASIS ESTIMATED

IDLE

WINGS LEVEL

STANDARD DAY

ENGINE F100-PW-229/CFT

CONDITIONS:

44

30

160

200

A

B

B

B

C

C

C

D

E

F

240

48

24

28

32

36

40

44

48

24

28

32

36

40

44

48

Figure C865.(Sheet 1)

T.O. GR1F16CJ11

C896Change 7

0.9

1.1

1.3

1.5

1.7

0

1.0

2.0

3.0

4.0

BASELINE

0

10

20

30

40

50

0.9

1.1

1.3

1.5

1.7

0.9

1.1

1.3

1.5

1.7

24

28

32

36

0

100

200

300

BASELINE

BASELINE

INITIAL MACH NUMBER

GW   1000 POUNDS

TIME   MINUTES

DIST

ANCE   NM

FUEL USED   POUNDS

1F-16CJ-1-1-1104X37

Deceleration    30,000 Feet

DATA BASIS ESTIMATED

IDLE

WINGS LEVEL

STANDARD DAY

ENGINE F100-PW-229/CFT

CONDITIONS:

40

0.7

0.7

0.7

400

5.0

44

48

24

28

32

36

40

44

48

24

28

32

36

40

44

48

Figure C865.(Sheet 2)

T.O. GR1F16CJ11

Change 7C897/(C898 blank)

1.0

1.2

1.4

1.6

1.8

0

1.0

2.0

3.0

4.0

BASELINE

0

10

20

30

40

50

24

28

32

36

0

100

200

300

BASELINE

BASELINE

INITIAL MACH NUMBER

GW   1000 POUNDS

TIME   MINUTES

DIST

ANCE   NM

FUEL USED   POUNDS

1F-16CJ-1-1-1105X37

Deceleration    40,000 Feet

DATA BASIS ESTIMATED

IDLE

WINGS LEVEL

STANDARD DAY

ENGINE F100-PW-229/CFT

CONDITIONS:

40

400

0.8

5.0

44

1.0

1.2

1.4

1.6

1.8

0.8

60

1.0

1.2

1.4

1.6

1.8

0.8

48

24

28

32

36

40

44

48

24

28

32

36

40

44

48

Figure C865.(Sheet 3)

T.O. GR1F16CJ11

Change 7C91/(C92 blank)

PART 9 - MISSION PLANNING

Refer to Appendix A, Part 9 - Mission Planning