F16C/D. FLIGHT MANUAL (2002) - page 35

T.O. GR1F16CJ1CL2

N20

CONDITIONS

Takeoff and Landing Data Card

GW

. . . . . . . . . . . . . . . . . . . . . . . . . . . 

Runway Condition

. . . . . . . . . . . . . 

Runway Temp

. . . . . . . . . . . . . . . . . 

Pressure Altitude

. . . . . . . . . . . . . . 

Wind

. . . . . . . . . . . . . . . . . . . . . . . . . . 

Runway Length

. . . . . . . . . . . . . . . . 

Runway Slope

. . . . . . . . . . . . . . . . . 

TAKEOFF

LANDING

Rotation Speed

KIAS

. . . . . . 

Takeoff Speed/Dist

KIAS

FEET

. . 

Refusal Speed

KIAS

. . . . . . . 

Max Brake Speed

KIAS

. . . 

GW

GW

Approach Speed . . . . 

Touchdown Speed . . . 

Landing Distance . . . . 

Immediately

After Takeoff

Final Landing

LANDING

TAKEOFF

Figure N8.

T.O. GR1F16CJ1CL2

P1/PW

SECTION P/PW

PERFORMANCE DATA

F100PW229

TABLE OF CONTENTS

Page

TAKEOFF FACTOR

P2/PW

. . . . . . . . . . . . . . . . . . . . . . 

TAKEOFF SPEED AND DISTANCE

P4/PW

. . . . . . . 

ACCELERATION CHECK SPEED

P6/PW

. . . . . . . . . . 

GROUND VEHICLE FRICTION 

READINGTORCR 

CONVERSION

P7/PW

. . . . . . . . . . . . . . . . . . . . . . . 

REFUSAL SPEED

P8/PW

. . . . . . . . . . . . . . . . . . . . . . . 

REFUSAL SPEED WITH DRAG CHUTE

P12/PW

. . . . 

LANDING DENSITY FACTOR

P16/PW

. . . . . . . . . . . . 

APPROACH SPEEDS

P17/PW

. . . . . . . . . . . . . . . . . . . . 

SHORT FIELD LANDING DISTANCE

P18/PW

. . . . . 

SHORT FIELD LANDING

DISTANCE SEC

P20/PW

. . . . . . . . . . . . . . . . . . . . 

SHORT FIELD LANDING DISTANCE 

WITH DRAG CHUTE

P21/PW

. . . . . . . . . . . . . . . . . 

SHORT FIELD LANDING DISTANCE-

SEC WITH DRAG CHUTE

P23/PW

. . . . . . . . . . . . . 

CLIMB/OPTIMUM CRUISE

P25/PW

. . . . . . . . . . . . . . 

DIVERSION DECISION DIVERT

P29/PW

. . . . . . . 

DIVERSION DECISION LOITER

P32/PW

. . . . . . . 

BEST CRUISE ALTITUDE FOR SHORT

RANGE MISSION MAXIMUM

RANGE DESCENT

P35/PW

. . . . . . . . . . . . . . . . . . . . 

AMBIENT AIR TEMPERATURE

P37/PW

. . . . . . . . . . . 

T.O. GR1F16CJ1CL2

P2/PW

1F-16CJ-1CL-1-0003A

DATA BASIS FLT TEST

ENGINE F100-PW-229

Takeoff Factor

Figure P1.

T.O. GR1F16CJ1CL2

P4

1F-16CJ-1CL-1-0004A

Takeoff Speed and Distance

DATA BASIS FLT TEST

ENGINE F100-PW-229

CONFIGURATION:

CONDITIONS:

ALL DRAG INDEXES

TUDE

CG = 35% MAC

NOTES:

Refer to sheet 2.

ZERO ROLL TRIM

ALL TEMPERATURES

ALL ALTITUDES

10 DEGREES PITCH ATTI-

Figure P2.(Sheet 1)

(P3/PW blank)/P4/PW

T.O. GR1F16CJ1CL2

P5/PW

Takeoff Speed and Distance

DATA BASIS FLIGHT TEST

ENGINEF100PW229

CONFIGURATION:

CONDITIONS:

D

ALL DRAG INDEXES

D

CG=35% MAC

D

ZERO ROLL TRIM

D

ALL ALTITUDES

D

ALL TEMPERATURES

D

10 DEGREES PITCH ATTI

TUDE

NOTES:

D

ROTATE AT 10 KIAS (NONAB) OR 15 KIAS (AB) LESS THAN

TAKEOFF SPEED.

D

COMPUTE % INCREASE/DECREASE CHANGES INDIVIDUAL

LY.

D

INCREASE TAKEOFF SPEED 8% AND DISTANCE 18% FOR

AN 8

_

 PITCH ATTITUDE ROTATION.

D

INCREASE/DECREASE TAKEOFF SPEED 0.8 KIAS FOR EACH

1% FORWARD/AFT OF 35% MAC.

D

INCREASE/DECREASE DISTANCE 1% FOR EACH 1% FOR

WARD/AFT OF 35% MAC.

D

INCREASE DISTANCE 2% PER 100 DRAG INDEX.

D

INCREASE DISTANCE 4% PER 1% UPSLOPE.

D

DECREASE DISTANCE 3.5% PER 1% DOWNSLOPE.

D

INCREASE DISTANCE 11% PER 10 KTS TAILWIND.

D

DECREASE DISTANCE 10% PER 10 KTS HEADWIND.

D

FOR TAKEOFF SPEED CORRECTION WITH ROLL TRIM OTH

ER THAN ZERO, REFER TO TAKEOFF ROLL TRIM WITH

ASYMMETRIC STORES, FIGURE N1, PAGE N8.

Figure P2.(Sheet 2)

T.O. GR1F16CJ1CL2

P6/PW

1F-16CJ-1CL-1-0005B

DATA BASIS FLT TEST

ENGINE F100-PW-229

NOTES:

COMPUTE % INCREASE/DECREASE CHANGES

INDIVIDUALLY.

DECREASE SPEED 1% PER 100 DRAG INDEX.

INCREASE SPEED 7.6 KIAS PER 10 KTS HEADWIND.

DECREASE SPEED 7.7 KIAS PER 10 KTS TAILWIND.

INCREASE SPEED 3.4% PER 1% DOWNHILL SLOPE.

DECREASE SPEED 3.5% PER 1% UPHILL SLOPE.

Acceleration Check Speed

ACCELERA

TION CHECK SPEED   KIAS

6

5

4

3

2

1 50 45 40 35 30 25 20

TAKEOFF FACTOR

GW   1000 POUNDS

40

60

80

100

120

140

160

180

7

BASELINE

Figure P3.

T.O. GR1F16CJ1CL2

P7/PW

1F-16X-1CL-1-0005X

Ground Vehicle Friction Reading

Conversion

NOTES:

IN MANY AREAS, GROUND VEHICLE FRICTION READING

IS THE ONLY AVAILABLE MEASURE FOR RUNWAY

BRAKING ACTION.
NORMALLY THE GROUND VEHICLE FRICTION READING,

ALSO REFERRED TO AS BRAKING ACTION COEFFICIENT,

IS GIVEN AS WHOLE NUMBERS, NOT AS DECIMALS

(I.E., 40 INSTEAD OF 0.40).

GROUND VEHICLE FRICTION READING

RCR/BRAKING ACTION LEVEL

26

24

22

20

18

16

14

12

10

8

6

4

2

0

0.80

0.70

0.60

0.50

0.40

0.30

0.20

0.10

0

MEDIUM

MEDIUM TO POOR

MEDIUM TO GOOD

POOR

GOOD

RCR

To

Figure P4.

T.O. GR1F16CJ1CL2

P8/PW

Refusal Speed

DATA BASIS ESTIMATED

ENGINE F100-PW-229

CONFIGURATION:

CONDITIONS:

ALL DRAG INDEXES
SPEEDBRAKES   OPEN

GW = 32,000 LB

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

NOTES:

COMPUTE % INCREASE/DECREASE CHANGES INDIVIDUALLY.

FOR RCR = 16 (DRY) DECREASE NON-AB/AB REFUSAL SPEED

INCREASE/DECREASE REFUSAL SPEED 1.1%/0.9% WITH

1F-16CJ-1CL-1-0006A

INCREASE/DECREASE REFUSAL SPEED 5/5 KIAS WITH NON-AB

BY 4/5 KIAS.

NON-AB AND 0.7%/0.7% WITH AB PER 1000 LB LESS/

ADDITIONAL GW.

AND 6/6 KIAS WITH AB PER 5 KTS HEADWIND/TAILWIND.

INCREASE/DECREASE REFUSAL SPEED 0.5/1.0 KIAS WITH

NON-AB AND 1.5/2.0 KIAS WITH AB PER 1% UPSLOPE/

DOWNSLOPE.

Figure P5.(Sheet 1)

T.O. GR1F16CJ1CL2

P9/PW

Refusal Speed

DATA BASIS ESTIMATED

ENGINE F100-PW-229

CONFIGURATION:

CONDITIONS:

ALL DRAG INDEXES
SPEEDBRAKES   OPEN

GW = 32,000 LB

IDLE SELECTED AT
REFUSAL SPEED
MAX EFFORT BRAKING

WET CONCRETE (RCR = 18)

NOTES:

COMPUTE % INCREASE/DECREASE CHANGES INDIVIDUALLY.

FOR RCR = 12 (WET) DECREASE NON-AB/AB REFUSAL SPEED

INCREASE/DECREASE REFUSAL SPEED 0.6%/0.4% WITH

1F-16CJ-1CL-1-0007A

INCREASE/DECREASE REFUSAL SPEED 6/7 KIAS WITH NON-AB

BY 9/10 KIAS.

NON-AB AND 0.2%/0.2% WITH AB PER 1000 LB LESS/

ADDITIONAL GW.

AND 7/8 KIAS WITH AB PER 5 KTS HEADWIND/TAILWIND.

INCREASE/DECREASE REFUSAL SPEED 2.5/4.5 KIAS WITH

NON-AB AND 4.0/5.5 KIAS WITH AB PER 1% UPSLOPE/

DOWNSLOPE.

Figure P5.(Sheet 2)

T.O. GR1F16CJ1CL2

P10/PW

Refusal Speed

DATA BASIS ESTIMATED

ENGINE F100-PW-229

CONFIGURATION:

CONDITIONS:

ALL DRAG INDEXES
SPEEDBRAKES   OPEN

GW = 32,000 LB

IDLE SELECTED AT
REFUSAL SPEED
MAX EFFORT BRAKING

SNOW (RCR = 8)

NOTES:

COMPUTE % INCREASE/DECREASE CHANGES INDIVIDUALLY.

INCREASE/DECREASE REFUSAL SPEED 0.6%/0.5% WITH

1F-16CJ-1CL-1-0008A

INCREASE/DECREASE REFUSAL SPEED 6/7 KIAS WITH NON-AB

NON-AB AND 0.1%/0.2% WITH AB PER 1000 LB LESS/

ADDITIONAL GW.

AND 7/7 KIAS WITH AB PER 5 KTS HEADWIND/TAILWIND.

INCREASE/DECREASE REFUSAL SPEED 3/5 KIAS WITH

NON-AB AND 4/6 KIAS WITH AB PER 1% UPSLOPE/

DOWNSLOPE.

Figure P5.(Sheet 3)

T.O. GR1F16CJ1CL2

P11/PW

Refusal Speed

DATA BASIS ESTIMATED

ENGINE F100-PW-229

CONFIGURATION:

CONDITIONS:

ALL DRAG INDEXES
SPEEDBRAKES   OPEN

GW = 32,000 LB

IDLE SELECTED AT
REFUSAL SPEED
MAX EFFORT BRAKING
ICY (RCR = 4)

NOTES:

COMPUTE % INCREASE/DECREASE CHANGES INDIVIDUALLY.

DECREASE/INCREASE REFUSAL SPEED 0.0%/0.1% WITH

1F-16CJ-1CL-1-0009A

INCREASE/DECREASE REFUSAL SPEED 6/7 KIAS WITH NON-AB

NON-AB AND 0.7%/0.3% WITH AB PER 1000 LB LESS/

ADDITIONAL GW.

AND 7/7 KIAS WITH AB PER 5 KTS HEADWIND/TAILWIND.

INCREASE/DECREASE REFUSAL SPEED 3/5 KIAS WITH

NON-AB AND 4/6 KIAS WITH AB PER 1% UPSLOPE/

DOWNSLOPE.

Figure P5.(Sheet 4)

T.O. GR1F16CJ1CL2

P12/PW

Refusal Speed With Drag Chute

DRAG CHUTE DEPLOYED

GR1F-16CJ-1CL-1-1012X37

DATA BASIS ESTIMATED

ENGINE F100-PW-229

CONFIGURATION:

CONDITIONS:

ALL DRAG INDEXES
SPEEDBRAKES   OPEN

DRAG CHUTE   DEPLOYED

IDLE SELECTED AND

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

NOTES:

COMPUTE % INCREASE/DECREASE CHANGES INDIVIDUALLY.

FOR RCR = 16 (DRY) DECREASE NON-AB/AB DRY RUNWAY

INCREASE/DECREASE REFUSAL SPEED 1.8%/1.2% WITH 

INCREASE/DECREASE REFUSAL SPEED 6/6 KIAS WITH NONAB

REFUSAL SPEED BY 2.5/3.5 KIAS.

NON-AB AND 1.7%/1.1% WITH AB PER 1000 LB LESS/

ADDITIONAL GW.

AND 7/7 KIAS WITH AB PER 5 KTS HEADWIND/TAILWIND.

DECREASE/INCREASE REFUSAL SPEED 1/0.5 KIAS WITH

NON-AB AND INCREASE/DECREASE REFUSAL SPEED 0.5/0.5 KIAS

WITH AB PER 1% UPSLOPE/DOWNSLOPE.

GW = 32,000 LB

Figure P6. (Sheet 1)

T.O. GR1F16CJ1CL2

P13/PW

Refusal Speed With Drag Chute

GR1F-16CJ-1CL-1-1013X37

DRAG CHUTE DEPLOYED

DATA BASIS ESTIMATED

ENGINE F100-PW-229

CONFIGURATION:

CONDITIONS:

ALL DRAG INDEXES
SPEEDBRAKES   OPEN

DRAG CHUTE   DEPLOYED

IDLE SELECTED AND

AT REFUSAL SPEED
MAX EFFORT BRAKING
WET CONCRETE (RCR = 18)

NOTES:

COMPUTE % INCREASE/DECREASE CHANGES INDIVIDUALLY.

FOR RCR = 12 (WET) DECREASE NONAB/AB WET RUNWAY

INCREASE/DECREASE REFUSAL SPEED 2.1%/1.2% WITH

INCREASE/DECREASE REFUSAL SPEED 7/8 KIAS WITH NONAB

REFUSAL SPEED BY 6/8 KIAS.

NON-AB AND 2.1%/1.1% WITH AB PER 1000 LB LESS/

ADDITIONAL GW.

AND 9/9 KIAS WITH AB PER 5 KTS HEADWIND/TAILWIND.

INCREASE/DECREASE REFUSAL SPEED 0/0.5 KIAS WITH

NON-AB AND 1.5/2 KIAS WITH AB PER 1% UPSLOPE/

DOWNSLOPE.

GW = 32,000 LB

6.5

6.0

5.5

5.0

4.5

4.0

3.5

3.0

2.5

2.0

1.5

3

4

5

6

7

8

9

10

11

12

Figure P6.(Sheet 2)

T.O. GR1F16CJ1CL2

P14/PW

Refusal Speed With Drag Chute

GR1F-16CJ-1CL-1-1014X37

DRAG CHUTE DEPLOYED

DATA BASIS ESTIMATED

ENGINE F100-PW-229

CONFIGURATION:

CONDITIONS:

ALL DRAG INDEXES
SPEEDBRAKES   OPEN

DRAG CHUTE   DEPLOYED

IDLE SELECTED AND

AT REFUSAL SPEED
MAX EFFORT BRAKING
SNOW (RCR = 8)

NOTES:

COMPUTE % INCREASE/DECREASE CHANGES INDIVIDUALLY.

INCREASE/DECREASE REFUSAL SPEED 2.1%/1.2% WITH

INCREASE/DECREASE REFUSAL SPEED 8/8 KIAS WITH NONAB

NON-AB AND 2.0%/1.1% WITH AB PER 1000 LB LESS/

ADDITIONAL GW.

AND 9/10 KIAS WITH AB PER 5 KTS HEADWIND/TAILWIND.

INCREASE/DECREASE REFUSAL SPEED 0.5/1.5 KIAS WITH

NON-AB AND 2.5/3.5 KIAS WITH AB PER 1% UPSLOPE/

DOWNSLOPE.

GW = 32,000 LB

Figure P6.(Sheet 3)

T.O. GR1F16CJ1CL2

P15/PW

Refusal Speed With Drag Chute

GR1F-16CJ-1CL-1-1015X37

DRAG CHUTE DEPLOYED

DATA BASIS ESTIMATED

ENGINE F100-PW-229

CONFIGURATION:

CONDITIONS:

ALL DRAG INDEXES
SPEEDBRAKES   OPEN

DRAG CHUTE   DEPLOYED

IDLE SELECTED AND

AT REFUSAL SPEED
MAX EFFORT BRAKING
ICY (RCR = 4)

NOTES:

COMPUTE % INCREASE/DECREASE CHANGES INDIVIDUALLY.

DECREASE/INCREASE REFUSAL SPEED 2.2%/1.2% WITH 

INCREASE/DECREASE REFUSAL SPEED 10/12 KIAS WITH NONAB

NON-AB AND 2.0%/1.0% WITH AB PER 1000 LB LESS/

ADDITIONAL GW.

AND 13/14 KIAS WITH AB PER 5 KTS HEADWIND/TAILWIND.

INCREASE/DECREASE REFUSAL SPEED 3/8.5 KIAS WITH

NON-AB AND 5.5/11.5 KIAS WITH AB PER 1% UPSLOPE/

DOWNSLOPE.

GW = 32,000 LB

Figure P6.(Sheet 4)

T.O. GR1F16CJ1CL2

P16/PW

1F-16X-1CL-1-0001X

Landing Density Factor

Figure P7.