F16C/D. FLIGHT MANUAL (2002) - page 56

T.O. GR1F16CJ11

Change 7A213

1F-16CJ-1-1-1018A

Refusal Speed (Non-AB)

DATA BASIS ESTIMATED

ENGINE F100-PW-229

CONFIGURATION:

CONDITIONS:

ALL DRAG INDEXES

SPEEDBRAKES   OPEN

IDLE SELECTED AT REFUSAL SPEED
MAX EFFORT BRAKING

SNOW (RCR=8)

NOTES:

REFUSAL SPEED BASED ON:

ZERO TAXI ENERGY.

NO BRAKING ABOVE MAX BRAKE APPLICATION SPEED (REFER TO FIGURE A2-12).
BRAKES APPLIED 3 SECONDS AFTER IDLE SELECTED.

ICY (RCR=4)

0

1

2

3

SLOPE   %

REFUSAL SPEED   KIAS

180

160

140

120

100

80

60

40

BASELINE

200

SNOW (RCR=8)

7

ICY (RCR=4)

BASELINE

0

20

40

WIND   KNOTS

NON-AB T

AKEOFF F

ACTOR

2

3

4

5

6

8

Figure A25.(Sheet 3)

T.O. GR1F16CJ11

A214Change 7

1F-16CJ-1-1-1019A

Refusal Speed (AB)

DATA BASIS ESTIMATED

ENGINE F100-PW-229

CONFIGURATION:

CONDITIONS:

ALL DRAG INDEXES
SPEEDBRAKES   OPEN

IDLE SELECTED AT REFUSAL SPEED
MAX EFFORT BRAKING
DRY CONCRETE (RCR=23)

NOTES:

REFUSAL SPEED BASED ON:

ZERO TAXI ENERGY.

NO BRAKING ABOVE MAX BRAKE APPLICATION SPEED (REFER TO FIGURE A2-12).
BRAKES APPLIED 3 SECONDS AFTER IDLE SELECTED.
FOR RCR=16 (DRY) DECREASE REFUSAL SPEED BY 5 KIAS FOR ALL GW'S.

1.0

1.5

2.0

2.5

AB T

AKEOFF F

ACTOR

0

1

2

3

SLOPE   %

REFUSAL SPEED   KIAS

180

160

140

120

100

80

60

40

BASELINE

200

3.0

F

0

20

40

WIND   KNOTS

BASELINE

A

3.5

4.0

B

E

D

C

Figure A26.(Sheet 1)

T.O. GR1F16CJ11

Change 7A215

1F-16CJ-1-1-1020A

Refusal Speed (AB)

DATA BASIS ESTIMATED

ENGINE F100-PW-229

CONFIGURATION:

CONDITIONS:

ALL DRAG INDEXES

SPEEDBRAKES   OPEN

IDLE SELECTED AT REFUSAL SPEED
MAX EFFORT BRAKING

WET CONCRETE (RCR=18)

NOTES:

REFUSAL SPEED BASED ON:

ZERO TAXI ENERGY.

NO BRAKING ABOVE MAX BRAKE APPLICATION SPEED (REFER TO FIGURE A2-12).
BRAKES APPLIED 3 SECONDS AFTER IDLE SELECTED.
FOR RCR=12 (WET) DECREASE REFUSAL SPEED BY 10 KIAS FOR ALL GW'S.

AB T

AKEOFF F

ACTOR

0

1

2

3

SLOPE   %

REFUSAL SPEED   KIAS

180

160

140

120

100

80

60

40

BASELINE

200

3.5

BASELINE

0

20

40

WIND   KNOTS

4.0

1.0

1.5

2.0

2.5

3.0

Figure A26.(Sheet 2)

T.O. GR1F16CJ11

A216Change 7

1F-16CJ-1-1-1021A

Refusal Speed (AB)

DATA BASIS ESTIMATED

ENGINE F100-PW-229

CONFIGURATION:

CONDITIONS:

ALL DRAG INDEXES

SPEEDBRAKES   OPEN

IDLE SELECTED AT REFUSAL SPEED
MAX EFFORT BRAKING

SNOW (RCR=8)

NOTES:

REFUSAL SPEED BASED ON:

ZERO TAXI ENERGY.

NO BRAKING ABOVE MAX BRAKE APPLICATION SPEED (REFER TO FIGURE A2-12).
BRAKES APPLIED 3 SECONDS AFTER IDLE SELECTED.

0

1

2

3

SLOPE   %

REFUSAL SPEED   KIAS

180

160

140

120

100

80

60

40

BASELINE

200

ICY (RCR=4)

SNOW (RCR=8)

BASELINE

0

20

40

WIND   KNOTS

1.0

1.5

2.0

2.5

AB T

AKEOFF F

ACTOR

3.0

ICY (RCR=4)

4.0

3.5

Figure A26.(Sheet 3)

T.O. GR1F16CJ11

Change 7A217

GR1F-16CJ-1-1-5022X37

190

DATA BASIS ESTIMATED

CONFIGURATION:

CONDITIONS:

Refusal Speed With Drag Chute (Non-AB)

ENGINE F100-PW-229

ALL DRAG INDEXES
SPEEDBRAKES   OPEN

IDLE SELECTED AND DRAG CHUTE

MAX EFFORT BRAKING
DRY CONCRETE (RCR=23)

NOTES:

REFUSAL SPEED BASED ON:

ZERO TAXI ENERGY.

NO BRAKING ABOVE MAX BRAKE APPLICATION SPEED (REFER TO FIGURE A2-12).
BRAKES APPLIED 3 SECONDS AFTER IDLE SELECTED.

DEPLOYED AT REFUSAL SPEED

FOR RCR=16 (DRY) DECREASE DRY RUNWAY REFUSAL SPEED BY 2.5 KIAS FOR ALL GW'S.

CHUTE SEPARATION SPEED

MAXIMUM RECOMMENDED CHUTE DEPLOYMENT SPEED

BASELINE

REFUSAL SPEED   KIAS

180

170

160

150

140

130

120

110

100

90

80

3

2

1

0

SLOPE   %

NON-AB T

AKEOFF F

ACTOR

7

5

4

3

2

6

DRAG CHUTE   DEPLOYED

BASELINE

40

20

0

WIND   KNOTS

8

Figure A27.(Sheet 1)

T.O. GR1F16CJ11

A218Change 7

GR1F-16CJ-1-1-5023X37

DATA BASIS ESTIMATED

CONFIGURATION:

CONDITIONS:

Refusal Speed With Drag Chute (Non-AB)

ENGINE F100-PW-229

ALL DRAG INDEXES
SPEEDBRAKES   OPEN

IDLE SELECTED AND DRAG CHUTE

MAX EFFORT BRAKING

WET CONCRETE (RCR=18)

NOTES:

REFUSAL SPEED BASED ON:

ZERO TAXI ENERGY.

NO BRAKING ABOVE MAX BRAKE APPLICATION SPEED (REFER TO FIGURE A2-12).
BRAKES APPLIED 3 SECONDS AFTER IDLE SELECTED.

DEPLOYED AT REFUSAL SPEED

FOR RCR=12 (WET) DECREASE WET RUNWAY REFUSAL SPEED BY 6 KIAS FOR ALL GW'S.

CHUTE SEPARATION SPEED

MAXIMUM RECOMMENDED CHUTE DEPLOYMENT SPEED

BASELINE

190

180

170

160

150

140

130

120

110

100

90

80

3

2

1

0

SLOPE   %

NON-AB T

AKEOFF F

ACTOR

7

5

4

3

2

6

REFUSAL SPEED   KIAS

DRAG CHUTE   DEPLOYED

BASELINE

40

20

0

WIND   KNOTS

8

Figure A27.(Sheet 2)

T.O. GR1F16CJ11

Change 7A219

CHUTE SEPARATION SPEED

MAXIMUM RECOMMENDED CHUTE DEPLOYMENT SPEED

GR1F-16CJ-1-1-5024X37

BASELINE

190

180

170

160

150

140

130

120

110

100

90

80

3

2

1

0

SLOPE   %

NON-AB T

AKEOFF F

ACTOR

7

5

4

3

2

DATA BASIS ESTIMATED

CONFIGURATION:

CONDITIONS:

Refusal Speed With Drag Chute (Non-AB)

ENGINE F100-PW-229

ALL DRAG INDEXES
SPEEDBRAKES   OPEN

IDLE SELECTED AND DRAG CHUTE

MAX EFFORT BRAKING

SNOW (RCR=8)

NOTES:

REFUSAL SPEED BASED ON:

ZERO TAXI ENERGY.

NO BRAKING ABOVE MAX BRAKE APPLICATION SPEED (REFER TO FIGURE A2-12).
BRAKES APPLIED 3 SECONDS AFTER IDLE SELECTED.

DEPLOYED AT REFUSAL SPEED

6

REFUSAL SPEED   KIAS

DRAG CHUTE   DEPLOYED

BASELINE

40

20

0

WIND   KNOTS

8

Figure A27.(Sheet 3)

T.O. GR1F16CJ11

A220Change 7

CHUTE SEPARATION SPEED

MAXIMUM RECOMMENDED CHUTE DEPLOYMENT SPEED

GR1F-16CJ-1-1-5125X37

BASELINE

BASELINE

190

180

170

160

150

140

130

120

110

100

90

80

3

2

1

0

SLOPE   %

NON-AB T

AKEOFF F

ACTOR

7

5

4

3

2

DATA BASIS ESTIMATED

CONFIGURATION:

CONDITIONS:

Refusal Speed With Drag Chute (Non-AB)

ENGINE F100-PW-229

ALL DRAG INDEXES
SPEEDBRAKES   OPEN

IDLE SELECTED AND DRAG CHUTE

MAX EFFORT BRAKING
ICY (RCR=4)

NOTES:

REFUSAL SPEED BASED ON:

ZERO TAXI ENERGY.

NO BRAKING ABOVE MAX BRAKE APPLICATION SPEED (REFER TO FIGURE A2-12).
BRAKES APPLIED 3 SECONDS AFTER IDLE SELECTED.

DEPLOYED AT REFUSAL SPEED

6

REFUSAL SPEED   KIAS

DRAG CHUTE   DEPLOYED

40

20

0

WIND   KNOTS

8

Figure A27.(Sheet 4)

T.O. GR1F16CJ11

Change 7A221

GR1F-16CJ-1-1-5126X37

DATA BASIS ESTIMATED

CONFIGURATION:

CONDITIONS:

Refusal Speed With Drag Chute (AB)

ENGINE F100-PW-229

ALL DRAG INDEXES
SPEEDBRAKES   OPEN

IDLE SELECTED AND DRAG CHUTE

MAX EFFORT BRAKING
DRY CONCRETE (RCR=23)

NOTES:

REFUSAL SPEED BASED ON:

ZERO TAXI ENERGY.

NO BRAKING ABOVE MAX BRAKE APPLICATION SPEED (REFER TO FIGURE A2-12).
BRAKES APPLIED 3 SECONDS AFTER IDLE SELECTED.

DEPLOYED AT REFUSAL SPEED

FOR RCR=16 (DRY) DECREASE DRY RUNWAY REFUSAL SPEED BY 3.5 KIAS FOR ALL GW'S.

CHUTE SEPARATION SPEED

MAXIMUM RECOMMENDED CHUTE DEPLOYMENT SPEED

BASELINE

190

180

170

160

150

140

130

120

110

100

90

80

3

2

1

0

SLOPE   %

AB T

AKEOFF F

ACTOR

3.5

2.5

2.0

1.5

1.0

3.0

REFUSAL SPEED   KIAS

DRAG CHUTE   DEPLOYED

4.0

BASELINE

40

20

0

WIND   KNOTS

Figure A28.(Sheet 1)

T.O. GR1F16CJ11

A222Change 7

GR1F-16CJ-1-1-5027X37

DATA BASIS ESTIMATED

CONFIGURATION:

CONDITIONS:

Refusal Speed With Drag Chute (AB)

ENGINE F100-PW-229

ALL DRAG INDEXES
SPEEDBRAKES   OPEN

IDLE SELECTED AND DRAG CHUTE

MAX EFFORT BRAKING

WET CONCRETE (RCR=18)

NOTES:

REFUSAL SPEED BASED ON:

ZERO TAXI ENERGY.

NO BRAKING ABOVE MAX BRAKE APPLICATION SPEED (REFER TO FIGURE A2-12).
BRAKES APPLIED 3 SECONDS AFTER IDLE SELECTED.

DEPLOYED AT REFUSAL SPEED

FOR RCR=12 (WET) DECREASE WET RUNWAY REFUSAL SPEED BY 8.5 KIAS FOR ALL GW'S.

CHUTE SEPARATION SPEED

MAXIMUM RECOMMENDED CHUTE DEPLOYMENT SPEED

BASELINE

190

180

170

160

150

140

130

120

110

100

90

80

3

2

1

0

SLOPE   %

AB T

AKEOFF F

ACTOR

3.5

2.5

2.0

1.5

1.0

3.0

REFUSAL SPEED   KIAS

DRAG CHUTE   DEPLOYED

4.0

BASELINE

40

20

0

WIND   KNOTS

Figure A28.(Sheet 2)

T.O. GR1F16CJ11

Change 7A223

CHUTE SEPARATION SPEED

MAXIMUM RECOMMENDED CHUTE DEPLOYMENT SPEED

GR1F-16CJ-1-1-5028X37

BASELINE

190

180

170

160

150

140

130

120

110

100

90

80

3

2

1

0

SLOPE   %

AB T

AKEOFF F

ACTOR

3.5

2.5

2.0

1.5

1.0

DATA BASIS ESTIMATED

CONFIGURATION:

CONDITIONS:

Refusal Speed With Drag Chute (AB)

ENGINE F100-PW-229

ALL DRAG INDEXES
SPEEDBRAKES   OPEN

IDLE SELECTED AND DRAG CHUTE

MAX EFFORT BRAKING

SNOW (RCR=8)

NOTES:

REFUSAL SPEED BASED ON:

ZERO TAXI ENERGY.

NO BRAKING ABOVE MAX BRAKE APPLICATION SPEED (REFER TO FIGURE A2-12).
BRAKES APPLIED 3 SECONDS AFTER IDLE SELECTED.

DEPLOYED AT REFUSAL SPEED

3.0

REFUSAL SPEED   KIAS

DRAG CHUTE   DEPLOYED

4.0

BASELINE

40

20

0

WIND   KNOTS

Figure A28.(Sheet 3)

T.O. GR1F16CJ11

A224Change 7

CHUTE SEPARATION SPEED

MAXIMUM RECOMMENDED CHUTE DEPLOYMENT SPEED

GR1F-16CJ-1-1-5029X37

BASELINE

190

180

170

160

150

140

130

120

110

100

90

80

3

2

1

0

SLOPE   %

AB T

AKEOFF F

ACTOR

3.5

2.5

2.0

1.5

1.0

DATA BASIS ESTIMATED

CONFIGURATION:

CONDITIONS:

Refusal Speed With Drag Chute (AB)

ENGINE F100-PW-229

ALL DRAG INDEXES
SPEEDBRAKES   OPEN

IDLE SELECTED AND DRAG CHUTE

MAX EFFORT BRAKING
ICY (RCR=4)

NOTES:

REFUSAL SPEED BASED ON:

ZERO TAXI ENERGY.

NO BRAKING ABOVE MAX BRAKE APPLICATION SPEED (REFER TO FIGURE A2-12).
BRAKES APPLIED 3 SECONDS AFTER IDLE SELECTED.

DEPLOYED AT REFUSAL SPEED

3.0

REFUSAL SPEED   KIAS

DRAG CHUTE   DEPLOYED

4.0

BASELINE

40

20

0

WIND   KNOTS

Figure A28.(Sheet 4)

T.O. GR1F16CJ11

Change 7A225

1F-16CJ-1-1-1022A

Minimum AB Blowout Speed

DATA BASIS FLIGHT TEST

ENGINE F100-PW-229

3.0

2.5

2.0

1.5

1.0

0

100
200
300
400

0

20

40

0

1

2
3

40

60

80

100

120

140

160

180

0

1

2

3

4

5

6

7

8

9

10

MAX AB T

AKEOFF F

ACTOR

INDEX

MINIMUM MAX AB BLOWOUT SPEED   KIAS

GW   1000 POUNDS

RUNWAY LENGTH   1000 FEET

A

G

BASELINE

BASELINE

BASELINE

BASELINE

BASELINE

WIND

%

KNOTS

SLOPE

28

33

38

43

48

18

23

3.5

4.0

B

C

D

E

F

DRAG

Figure A29.

T.O. GR1F16CJ11

A226Change 7

Takeoff Roll Trim With Asymmetric Stores

LEF'S SCHEDULED

TEF'S AT 20 DEGREES

CONFIGURATION:

DATA BASIS FLIGHT TEST

NOTES:

100

120

140

160

180

200

4/6

2/8

3/7

0

1

2

3

FULL

A

B

C

D

BASELINE

TAKEOFF SPEED   KIAS

STORE STATION

DOTS OF ROLL TRIM

1F-16X-1-1-0010X

INCREASE TAKEOFF SPEED 2 KNOTS FOR EACH DOT OF ROLL TRIM APPLIED TO COMPENSATE

FOR REDUCED LIFT. TAKEOFF DISTANCE INCREASES PROPORTIONATELY TO THE SPEED

IT IS POSSIBLE TO EXCEED THE LATERAL TRIM AUTHORITY OF THE AIRCRAFT FOR ONSPEED

TAKEOFF WITH A NET ASYMMETRIC (ROLLING) MOMENT LESS THAN AIRCRAFT TAKEOFF

LIMITS. REFER TO SECTION V FOR LIMITS.

INCREASE.

Figure A210.

T.O. GR1F16CJ11

Change 7A227

1F-16X-1-1-0011A

Takeoff and Landing Crosswind Limits

NOTES:

0

5

10

15

20

25

30

0

5

10

15

20

25

30

35

CROSSWIND COMPONENT   KNOTS

HEADWIND COMPONENT   KNOTS

A

B

C

CROSSWIND LIMITS FOR RCR VALUES 4-23 MAY BE OBTAINED BY INTERPOLATING BETWEEN

THE LIMITS SHOWN.

ENTER CHART WITH STEADY WIND TO DETERMINE HEADWIND COMPONENT AND MAXIMUM

GUST VELOCITY TO DETERMINE CROSSWIND COMPONENT.

Figure A211.

T.O. GR1F16CJ11

A228Change 8

GR1F-16CJ-1-1-1125A37

50

40

30

20

10

0

-10

-20

C

F

120

100

80

60

40

20

0

0 1 2 3 4 5

6

20 22 24 26 28 30 32 34 36 38 40 42 44

GW   1000 POUNDS

BRAKE ENERGY ABSORPTION   MILLION FOOT-POUNDS PER BRAKE

0

1

2

3

4

5

6

7

8

9

10

11

12

13

14

15

16

17

18

19

20

21

22

23

1

2

3

4

5

46 48

A

B

J

K

G

F

C

E

H

I

Brake Energy Limits    Max Effort Braking

DATA BASIS ESTIMATED

CONFIGURATION:

ALL DRAG INDEXES
SPEEDBRAKES   OPEN
TEF's DOWN

CONDITIONS:

NORMAL IDLE THRUST

ENGINE F100-PW-229

D

RUNWAY

TEMPERATURE

EXCEEDING 24.5 MILLION
FOOT-POUNDS PER BRAKE
CUMULATIVE TOTAL ENERGY
MAY RESULT IN LOSS OF
BRAKING.

NOTES:

ADD TAILWIND COMPONENT
OR SUBTRACT ONE-HALF

HEADWIND COMPONENT
FROM AIRSPEED WHEN
BRAKES ARE APPLIED.

FOR ABORTED TAKEOFF

AT AIRSPEED GREATER
THAN 100 KNOTS, ADD
2 MILLION FOOT-POUNDS

PER BRAKE IF BRAKES ARE

APPLIED SOONER THAN 4
SECONDS AFTER THROTTLE

IS RETARDED TO IDLE.

IF LANDING WITH ASYM-
METRICAL WING LOADING,

TAKE ACTION AS APPLIC-
ABLE FOR NEXT HIGHER

ENERGY ZONE TO ALLOW
FOR UNEQUAL BRAKE
ENERGY DISTRIBUTION.

24

Figure

 A212.(Sheet 1)