F16C/D. FLIGHT MANUAL (2002) - page 66

T.O. GR1F16CJ11

Change 1B19

Drag Indexes and Weights  

Individual Stores

DATA BASIS FLIGHT TEST

 NOTE:  WEIGHT AND DRAG INDEXES DO NOT

INCLUDE SUSPENSION EQUIPMENT.

REFER TO SHEET 2.

STORE

STATION

RACK

WEIGHT

LB

(EACH STORE)

DRAG

INDEX

(EACH STORE)

BDU33B/B, D/B

3,4,6, OR 7

TER

24

1

BDU50/B, A/B

3,4,6, OR 7

PYLON/TER

510

5/9

BL755 MK 2

3,4,6, OR 7

PYLON/TER

610

19/23

BLU107/B

3,4,6, OR 7

PYLON/TER

482

5/8

BLU109/B

3 OR 7

PYLON

2020

12

CATM88B (WITH WINGS AND

FINS)

3 OR 7

LAU118(V)4/A

795

8

CATM88B (WITHOUT WINGS

AND FINS)

3 OR 7

LAU118(V)4/A

733

8

CATM120A (107), B (106)

1 OR 9

LAUNCHER

345

0

CATM120A (107), B (106)

2,3,7, OR 8

LAUNCHER + ADAPTER

345

4

CBU52B/B

CBU58/B, A/B

CBU71/B

(SUU30 H/B)

3,4,6, OR 7

3,4,6, OR 7

3,4,6, OR 7

PYLON/TER

PYLON/TER

PYLON/TER

785

800

800

20/24

20/24

20/24

CBU87/B (SUU65/B)

3,4,6, OR 7

PYLON/TER

950

18/22

GBU10/B, A/B, C/B, D/B, E/B, F/B

3,4,6, OR 7

PYLON

2052

15

GBU10G/B, H/B, J/B

3,4,6, OR 7

PYLON

2135

17

GBU12/B, A/B, B/B, C/B, D/B, E/B

3,4,6, OR 7

PYLON

611

7

GBU12B/B, C/B, D/B, E/B

3 OR 7

TER

611

10

ITM88B

3 OR 7

LAU118(V)4/A

770

8

LANTIRN POD:

NAVIGATION

TARGETING

5L

5R

PYLON

PYLON

429*

553

32*

19

*

WITH PYLON.

Figure B11.(Sheet 4)

T.O. GR1F16CJ11

B110Change 3

Drag Indexes and Weights  

Individual Stores

DATA BASIS FLIGHT TEST

 NOTE:  WEIGHT AND DRAG INDEXES DO NOT

INCLUDE SUSPENSION EQUIPMENT.

REFER TO SHEET 2.

STORE

STATION

RACK

WEIGHT

LB

(EACH STORE)

DRAG

INDEX

(EACH STORE)

LAU3/A, B/A, C/A, D/A ROCKET

LAUNCHER WITH:

(19) M151

3,4,6, OR 7

PYLON/TER

496

14/20

(19) M156

3,4,6, OR 7

PYLON/TER

496

14/20

(19) MK 1

3,4,6, OR 7

PYLON/TER

418

14/20

(19) MK 5

3,4,6, OR 7

PYLON/TER

418

14/20

FIRED OUT (NO FWD FAIRING)

3,4,6, OR 7

PYLON/TER

76

26/39

EMPTY WITH FWD FAIRING

3,4,6, OR 7

PYLON/TER

78

14/20

LAU68A/A, B/A ROCKET

LAUNCHER WITH:

(7) M151

3 OR 7

TER

215

9

(7) M156

3 OR 7

TER

215

9

(7) MK 1

3 OR 7

TER

194

9

(7) MK 5

3 OR 7

TER

194

9

FIRED OUT (NO FWD FAIRING)

3 OR 7

TER

67

17

EMPTY WITH FWD FAIRING

3 OR 7

TER

68

9

LAU131/A ROCKET LAUNCHER

WITH:

(7) M151

3 OR 7

TER

223

9

(7) M156

3 OR 7

TER

223

9

(7) MK 1

3 OR 7

TER

195

9

(7) MK 5

3 OR 7

TER

195

9

FIRED OUT (NO FWD FAIRING)

3 OR 7

TER

68

18

EMPTY WITH FWD FAIRING

3 OR 7

TER

69

9

LAU5003/A ROCKET LAUNCHER

WITH:

(19) CM151 (CRV7)

(19) RA79 (CRV7)

FIRED OUT (NO FWD FAIRING)

EMPTY WITH FWD FAIRING

3 OR 7

3 OR 7

3 OR 7

3 OR 7

TER

TER

TER

TER

530

658

76

78

20

20

39

20

Figure B11.(Sheet 5)

T.O. GR1F16CJ11

Change 5B111

Drag Indexes and Weights  

Individual Stores

DATA BASIS FLIGHT TEST

 NOTE:  WEIGHT AND DRAG INDEXES DO NOT

INCLUDE SUSPENSION EQUIPMENT.

REFER TO SHEET 2.

STORE

STATION

RACK

WEIGHT

LB

(EACH STORE)

DRAG

INDEX

(EACH STORE)

M129E2

3,4,6, OR 7

PYLON

229

16

MK 20 MOD 3,4

3,4,6, OR 7

PYLON/TER

490

11/14

MK 82 AIR

3,4,6, OR 7

PYLON/TER

540

7/11

MK 82  LDGP

3,4,6, OR 7

PYLON/TER

510

5/9

MK 82 (SNAKEYE)

3,4,6, OR 7

PYLON/TER

550

7/11

MK 84 AIR

3,4,6, OR 7

PYLON

2010

10

MK 84  LDGP

3,4,6, OR 7

PYLON

1970

9

MXU648A/A, C/A (TRAVEL POD)

(MAX CARGO WT IS 300 LB)

3,4,5,6, OR 7

PYLON/TER

108

(EMPTY)

10/10

SUU20A/A, B/A WITH:

(A/A) (B/A)

(6) BDU33B/B, D/B

3,4,6, OR 7

PYLON

474420

14

(6) MK 106

3,4,6, OR 7

PYLON

360306

14

(4) M151

3,4,6, OR 7

PYLON

414360

14

(6) BDU33B/B, D/B+(4) M151

3,4,6, OR 7

PYLON

558504

14

(6) MK 106+(4) M151

3,4,6, OR 7

PYLON

444390

14

EMPTY

3,4,6, OR 7

PYLON

330276

12

SUU5003A/A, B/A WITH:

(6) BDU33B/B, D/B

(6) MK 106

(4) CM151 (CRV7)

(6) BDU33B/B, D/B+(4) CM151

(6) MK 106+(4) CM151

(4) RA79T (RA82) (CRV7)

EMPTY

3,4,6, OR 7

3,4,6, OR 7

3,4,6, OR 7

3,4,6, OR 7

3,4,6, OR 7

3,4,6, OR 7

3,4,6, OR 7

PYLON

PYLON

PYLON

PYLON

PYLON

PYLON

PYLON

(A/A) (B/A)

583546

469432

561524

705668

591554

547510

439402

14

14

14

14

14

14

12

Figure B11.(Sheet 6)

T.O. GR1F16CJ11

B112Change 5

Drag Indexes and Weights  

Individual Stores 

DATA BASIS FLIGHT TEST

 NOTE:  WEIGHT AND DRAG INDEXES DO NOT

INCLUDE SUSPENSION EQUIPMENT.

REFER TO SHEET 2.

STORE

STATION

RACK

WEIGHT

LB

(EACH STORE)

DRAG

INDEX

(EACH STORE)

TGM65A, B

3 OR 7

LAU88/A, A/A, 117/A,

A(V)1A, A(V)3/A

447

13/8

TGM65D, G

3 OR 7

LAU88/A, A/A, 117/A,

A(V)1A, A(V)3/A

474

13/8

300GALLON TANK (EMPTY/FULL):

NO STORES AT 4 OR 6

5

PYLON

392*/2432

15

STORES AT 4 AND 6

5

PYLON

392*/2432

18

370GALLON TANK (EMPTY/FULL):

NO STORES AT 3 OR 7

4 OR 6

NONE

490*/3006

27

AIM9'S AT 3 OR 7

4 OR 6

NONE

490*/3006

27

SINGLE RACKS OR STORES

  AT 3 OR 7

4 OR 6

NONE

490*/3006

35

MULTIPLE STORES AT 3 OR 7

4 OR 6

NONE

490*/3006

39

600GALLON TANK (EMPTY/FULL):

NO STORES AT 3 OR 7

4 OR 6

PYLON (NJETT)

399*/4360

20

AIM9'S AT 3 OR 7

4 OR 6

PYLON (NJETT)

399*/4360

20

SINGLE RACKS OR STORES

  AT 3 OR 7

4 OR 6

PYLON (NJETT)

399*/4360

30

MULTIPLE STORES AT 3 OR 7

4 OR 6

PYLON (NJETT)

399*/4360

32

300/370/600GALLON TANK WEIGHTS BASED ON JP8.

*

INCLUDES UNUSABLE FUEL.

Figure B11.(Sheet 7)

T.O. GR1F16CJ11

B113

1F-16X-1-1-0002A

DATA BASIS FLIGHT TEST

Position Error Correction    Airspeed

and Altitude

800

700

600

500

400

300

200

100

-1000

-500

0

500

1000

-10

-5

0

5

10

AL

TITUDE CORRECTION   FEET

AIRSPEED CORRECTION   KNOTS

CALIBRATED AIRSPEED   KNOTS

PRESSURE ALTITUDE   FEET

NOTE: USE ALTITUDE CORRECTION ONLY WHEN THE ALTIMETER MODE

SELECTOR IS IN THE PNEU (SECONDARY) OPERATIONS MODE.

PRESSURE ALTITUDE   FEET

NOTE: SUBTRACT CORRECTION FROM DESIRED CONDITION TO OBTAIN INDICATOR READING.

D

B

B

C

A

Figure B12.(Sheet 1)

T.O. GR1F16CJ11

B114

1F-16X-1-1-0003X

DATA BASIS FLIGHT TEST

Position Error Correction    Mach Number

NOTE:  SUBTRACT FROM THE TRUE MACH TO OBTAIN MACH INDICATOR READING.

-0.04

-0.03

-0.02

-0.01

0

0.01

0.02

0.03

0.04

0.4

0.6

0.8

1.0

1.2

1.4

1.6

TRUE MACH NUMBER

MACH CORRECTION

Figure B12.(Sheet 2)

T.

O

. GR1F

16CJ

11

B115

Figure B13.   (Sheet 1)

Airspeed Conversion

1F-16X-1-1-0004X

STD TEMP

C

ALTITUDE

1000 FT

SL

5

10
15
20
25
30
35
40
45
50
55
60

-56

-56

-56

-56

-56

-54

-44

-35

-25

-15

-5

5

15

0.4

0.5

0.6

0.7

0.8

0.9

1.0

200

300

400

500

600

100

200

300

400

500

600

CALIBRATED AIRSPEED   KNOTS

TRUE AIRSPEED   KNOTS

MACH NUMBER

A

B

D

C

E

-80

-70

-60

-50

-40

-30

-20

-10

0

10

20

30

40

50

60

140

120

100

80

60

40

20

0

-20

-40

-60

-80

-100

FAHRENHEIT

CENTIGRADE

= (

)

9/ 5

32

+

-

F

F

C

C

=

(

)

9

5/

32

T.

O

. GR1F

16CJ

11

B116

Airspeed Conversion

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

1.0

1.2

1.4

1.6

1.8

2.0

600

700

800

900

1000

1100

1200

200

300

400

500

600

700

800

MACH NUMBER

TRUE AIRSPEED   KNOTS

CALIBRATED AIRSPEED   KNOTS

Figure B13.   (Sheet 2)

T.O. GR1F16CJ11

B117

1F-16X-1-1-0006X

Compressibility Correction to Airspeed

NOTE:  EQUIVALENT AIRSPEED = CALIBRATED AIRSPEED   CORRECTION.

100

200

300

400

500

600

700

800

0

10

20

30

40

50

60

70

80

90

COMPRESSIBILITY CORRECTION   KNOTS

CALIBRATED AIRSPEED   KNOTS

A

B

C

Figure B14.

T.O. GR1F16CJ11

B118

Standard Atmosphere

DATA BASIS US STANDARD ATMOSPHERE, 1966

STANDARD SEA LEVEL AIR:

D

T  = 59

_

F (15

_

C)

D

P

o

 = 29.921 IN. OF HG

D

W  = 0.076475 LB/CU FT

D

ρ

o

= 0.0023769 SLUG/CU FT

D

1 IN. OF HG = 70.726 LB/SQ FT

D

1 IN. OF HG = 0.4912 LB/SQ IN.

D

a

o

 = 1116.4 FT/SEC

D

a

o

 = 661.48 KTS

ALTITUDE

DENSITY

AIR TEMPERATURE

SPEED OF

PRESSURE

ALTITUDE

FEET

DENSITY

RATIO

ρ/ρ

o

 

+

 

s

1

ń

s

Ǹ

DEG F

DEG C

SPEED OF

SOUND

KNOTS

IN. OF

HG

RATIO

P/P

o

 

+

 

d

-2000

-1000

1.0598

1.0296

0.9714

0.9855

66.132

62.566

18.962

16.981

665.98

663.73

32.15

31.02

1.0745

1.0368

0

1000

2000

3000

4000

1.0000

0.9711

0.9428

0.9151

0.8881

1.0000

1.0148

1.0299

1.0454

1.0611

59.000

55.434

51.868

48.302

44.735

15.000

13.019

11.038

9.057

7.075

661.48

659.23

656.92

654.60

652.35

29.92

28.86

27.82

26.82

25.84

1.0000

0.9644

0.9298

0.8962

0.8637

5000

6000

7000

8000

9000

0.8617

0.8359

0.8106

0.7860

0.7620

1.0773

1.0938

1.1107

1.1279

1.1456

41.169

37.603

34.037

30.471

26.905

5.094

3.113

1.132

-0.849

-2.831

650.04

647.72

645.34

643.02

640.71

24.90

23.98

23.09

22.22

21.39

0.8320

0.8014

0.7716

0.7428

0.7148

10,000

11,000

12,000

13,000

14,000

0.7385

0.7156

0.6932

0.6713

0.6500

1.1637

1.1822

1.2011

1.2205

1.2403

23.338

19.772

16.206

12.640

9.074

-4.812

-6.793

-8.774

-10.756

-12.737

638.33

635.95

633.63

631.25

628.87

20.58

19.79

19.03

18.29

17.58

0.6877

0.6614

0.6360

0.6113

0.5875

15,000

16,000

17,000

18,000

19,000

0.6292

0.6090

0.5892

0.5699

0.5511

1.2606

1.2815

1.3028

1.3246

1.3470

5.508

1.941

-1.625

-5.191

-8.757

-14.718

-16.699

-18.681

-20.662

-22.643

626.42

624.04

621.59

619.21

616.76

16.89

16.22

15.57

14.94

14.34

0.5643

0.5420

0.5203

0.4994

0.4791

20,000

21,000

22,000

23,000

24,000

0.5328

0.5150

0.4976

0.4807

0.4642

1.3700

1.3935

1.4176

1.4424

1.4678

-12.323

-15.889

-19.456

-23.022

-26.588

-24.624

-26.605

-28.587

-30.568

-32.549

614.32

611.87

609.42

606.91

604.46

13.75

13.18

12.64

12.11

11.60

0.4595

0.4406

0.4223

0.4046

0.3876

25,000

26,000

27,000

28,000

29,000

0.4481

0.4325

0.4173

0.4025

0.3881

1.4938

1.5206

1.5480

1.5762

1.6052

-30.154

-33.720

-37.286

-40.852

-44.419

-34.530

-36.511

-38.492

-40.473

-42.455

601.95

599.43

596.92

594.41

591.89

11.10

10.63

10.17

9.725

9.297

0.3711

0.3552

0.3398

0.3250

0.3107

Figure B15.(Sheet 1)

T.O. GR1F16CJ11

B119

Standard Atmosphere

DATA BASIS US STANDARD ATMOSPHERE, 1966

STANDARD SEA LEVEL AIR:

D

T  = 59

_

F (15

_

C)

D

P

o

 = 29.921 IN. OF HG

D

W  = 0.076475 LB/CU FT

D

ρ

o

 = 0.0023769 SLUG/CU FT

D

1 IN. OF HG = 70.726 LB/SQ FT

D

1 IN. OF HG = 0.4912 LB/SQ IN.

D

a

o

 = 1116.4 FT/SEC

D

a

o = 

 661.48 KTS

ALTITUDE

DENSITY

AIR TEMPERATURE

SPEED OF

PRESSURE

ALTITUDE

FEET

DENSITY

RATIO

ρ/ρ

o

 

+

 

s

1

ń

s

Ǹ

DEG F

DEG C

SPEED OF

SOUND

KNOTS

IN. OF

HG

RATIO

P/P

o

 

+

 

d

30,000

31,000

32,000

33,000

34,000

0.3741

0.3605

0.3473

0.3345

0.3220

1.6349

1.6654

1.6968

1.7291

1.7623

-47.985

-51.551

-55.117

-58.683

-62.249

-44.436

-46.417

-48.398

-50.379

-52.361

589.31

586.80

584.22

581.64

579.06

8.885

8.488

8.106

7.737

7.382

0.2970

0.2837

0.2709

0.2586

0.2467

35,000

36,089*

37,000

38,000

39,000

0.3099

0.2971

0.2844

0.2710

0.2583

1.7964

1.8347

1.8753

1.9209

1.9677

-65.816

-69.700

-69.700

-69.700

-69.700

-54.342

-56.500

-56.500

-56.500

-56.500

576.41

573.57

573.57

573.57

573.57

7.041

6.683

6.397

6.097

5.811

0.2353

0.2234

0.2138

0.2038

0.1942

40,000

41,000

42,000

43,000

44,000

0.2462

0.2346

0.2236

0.2131

0.2031

2.0155

2.0645

2.1148

2.1662

2.2189

-69.700

-69.700

-69.700

-69.700

-69.700

-56.500

-56.500

-56.500

-56.500

-56.500

573.57

573.57

573.57

573.57

573.57

5.538

5.278

5.030

4.794

4.569

0.1851

0.1764

0.1681

0.1602

0.1527

45,000

46,000

47,000

48,000

49,000

0.1936

0.1845

0.1758

0.1676

0.1597

2.2728

2.3281

2.3848

2.4428

2.5022

-69.700

-69.700

-69.700

-69.700

-69.700

-56.500

-56.500

-56.500

-56.500

-56.500

573.57

573.57

573.57

573.57

573.57

4.355

4.151

3.956

3.770

3.563

0.1455

0.1387

0.1322

0.1260

0.1201

50,000

51,000

52,000

53,000

54,000

0.1522

0.1451

0.1383

0.1318

0.1256

2.5630

2.6254

2.6892

2.7546

2.8216

-69.700

-69.700

-69.700

-69.700

-69.700

-56.500

-56.500

-56.500

-56.500

-56.500

573.57

573.57

573.57

573.57

573.57

3.425

3.264

3.111

2.965

2.826

0.1145

0.1091

0.1040

0.09909

0.09444

55,000

56,000

57,000

58,000

59,000

0.1197

0.1141

0.1087

0.1036

0.09877

2.8903

2.9606

3.0326

3.1063

3.1819

-69.700

-69.700

-69.700

-69.700

-69.700

-56.500

-56.500

-56.500

-56.500

-56.500

573.57

573.57

573.57

573.57

573.57

2.693

2.567

2.446

2.331

2.222

0.09001

0.08578

0.08176

0.07792

0.07426

60,000

61,000

62,000

63,000

64,000

65,000

0.09414

0.08972

0.08551

0.08150

0.07767

0.07403

3.2593

3.3386

3.4198

3.5029

3.5881

3.6754

-69.700

-69.700

-69.700

-69.700

-69.700

-69.700

-56.500

-56.500

-56.500

-56.500

-56.500

-56.500

573.57

573.57

573.57

573.57

573.57

573.57

2.118

2.018

1.924

1.833

1.747

1.665

0.07078

0.06746

0.06429

0.06127

0.05840

0.05566

*

Tropopause

Figure B15.(Sheet 2)

T.O. GR1F16CJ11

B120

Temperature Correction for Compressibility

1F-16X-1-1-0007A

-80

-60

-40

-20

0

20

40

60

0.2

0.4

0.6

0.8

1.0

1.2

1.4

1.6

1.8

2.0

AMBIENT TEMPERATURE    C

MACH NUMBER

TOTAL TEMPERATURE     C

TEMPERATURE RECOVERY

COEFFICIENT = 1.00

NOTE:

Figure B16.

T.O. GR1F16CJ11

Change 3B121

1F-16X-1-1-0008A

Angle of Attack

DATA BASIS FLIGHT TEST

LG   UP

ALL DRAG INDEXES

1G LEVEL FLIGHT

NO THRUST EFFECTS INCLUDED

CONFIGURATION:

CONDITIONS:

0

4

8

12

16

20

24

28

20

30

40

AOA   DEGREES

GW   1000 POUNDS

48

A

B

C

D

Figure B17.

T.O. GR1F16CJ11

B122Change 3

1F-16CJ-1-1-4009A

9

8

7

6

5

4

3

2

1

18

28

38

0.4

0.8

1.2

A

V

AILABLE LOAD F

ACTOR   G

GW   1000 LB

BASELINE

1.6

2.0

MACH NUMBER

9

8

7

6

5

4

3

2

1

18

28

38

A

V

AILABLE LOAD F

ACTOR   G

GW   1000 LB

BASELINE

0.0

0.4

0.8

1.2

1.6

2.0

0.0

CAT III

CAT I

MACH NUMBER

48

48

Available Load Factor

DATA BASIS FLIGHT TEST

ALL DRAG INDEXES

LG   UP

ENGINE F110-GE-129

CONDITIONS:

CONFIGURATION:

NOTES:

ALL TEMPERATURES
ALL THROTTLE SETTING

REFER TO SECTION V FOR G LIMITATIONS.

KCAS ON 9.0G LIMITER IS INACCURATE. (REFER TO FIGURE B1-3.)

2.4

2.4

Figure B18.

0

30

40

50

55

60

65

70

71

72

73

74

75

76

77

78

79

80

81

82

83

84

1

2

3

4

5

6

7

8

9

0

10

20

30

40

TURN RADIUS   1000 FEET

LOAD F

ACTOR   G

1F-16X-1-1-0009A

BANK ANGLE   DEGREES

TURN RATE   DEGREES/SECOND

Turn Conversion

T.

O

. GR1F

16CJ

11

B123

Figure B19.

T.O. GR1F16CJ11

B124

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

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

GROUND

VEHICLE

FRICTION

READING

RCR/

BRAKING

ACTION

LEVEL

Ground Vehicle Friction Reading-To-RCR

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).

MEDIUM TO GOOD

POOR

GOOD

Figure 

B110.