JEPPESEN GENERAL AIRWAY MANUAL (Issue Date 1 JUL 21) - page 51

Aircraft Type

All-up Mass

1

(Maximum

Apron Mass)

(Operating

Mass Empty)

Load

on

one

main

gear

leg

(%)

Standard Aircraft

Tire Pressure

ACN relative to

Rigid Pavement Subgrades

Flexible Pavement Subgrades

High K

= 150

MN/m

3

Medi-

um K

= 80

MN/m

3

Low

K =

40

MN/

m

3

Ultra-
low K

= 20

MN/m

3

High

CBR =

15%

Medi-

um

CBR =

10%

Low

CBR =

6%

Very

low

CBR =

3%

 

lbs

kgs

psi

kg/c

m

2

mPa

A

B

C

D

A

B

C

D

1

2

3

4

5

6

7

8

9

10

11

12

13

14

15

MD-87

141000

73300

63957
33248

47.4

170 11.95 1.17

40
18

42
20

44
21

46
22

36
17

38
17

42
19

46
22

MD-90-30ER

168500

89100

76430
40415

47.0

193 13.57 1.33

51
24

54
25

56
26

57
28

44
21

48
22

52
24

55
27

DASH7

43800
26000

19867
11793

46.75

107

7.55

0.74

11

6

12

6

13

7

13

7

10

5

11

6

12

6

14

8

DASH8 Ser-

ies 100

Standard

Tires

34700
22000

15740

9979

47.1

131

9.21

0.90

9
5

9
5

10

6

10

6

8
4

8
5

9
5

11

6

DASH8 Ser-

ies 100

Optional Tires

34700
22000

15740

9979

47.1

77

5.41

0.53

8
4

8
5

9
5

10

6

6
3

7
4

9
5

10

6

AIRPORT DATA - GENERAL

1601

ACN TABLES

Aircraft Type

All-up Mass

1

(Maximum

Apron Mass)

(Operating

Mass Empty)

Load

on

one

main

gear

leg

(%)

Standard Aircraft

Tire Pressure

ACN relative to

Rigid Pavement Subgrades

Flexible Pavement Subgrades

High K

= 150

MN/m

3

Medi-

um K

= 80

MN/m

3

Low

K =

40

MN/

m

3

Ultra-
low K

= 20

MN/m

3

High

CBR =

15%

Medi-

um

CBR =

10%

Low

CBR =

6%

Very

low

CBR =

3%

 

lbs

kgs

psi

kg/c

m

2

mPa

A

B

C

D

A

B

C

D

1

2

3

4

5

6

7

8

9

10

11

12

13

14

15

DASH8 Ser-

ies 400

Standard

Tires

64700
37886

29347
17185

 

227 15.95 1.56

19

9

20
10

21
10

21
11

16

8

17

8

18

9

20
10

DASH8 Ser-

ies 400

Optional Tires

64700
37886

29347
17185

 

141

9.91

0.97

18

8

18

9

19
10

20
10

15

7

16

8

19

9

20
10

Dornier

228-101/201

13250

8224

6010
3730

44.2

70

4.9

0.48

3.8
2.4

4.0
2.5

4.1
2.6

4.2
2.6

3.1
1.9

3.8
2.4

4.6
2.8

4.9
3.0

Dornier

228-202

13734

8354

6230
3789

45.1

74

5.1

0.50

4.1
2.5

4.3
2.6

4.4
2.7

4.5
2.8

3.4
2.1

4.1
2.5

4.9
3.0

5.1
3.1

Dornier

228-212

14175

8398

6430
3809

45.1

75

5.2

0.51

4.3
2.6

4.4
2.7

4.6
2.7

4.7
2.8

3.6
2.1

4.3
2.6

5.1
3.0

5.3
3.1

AIRPORT DATA - GENERAL

1602

ACN TABLES

Aircraft Type

All-up Mass

1

(Maximum

Apron Mass)

(Operating

Mass Empty)

Load

on

one

main

gear

leg

(%)

Standard Aircraft

Tire Pressure

ACN relative to

Rigid Pavement Subgrades

Flexible Pavement Subgrades

High K

= 150

MN/m

3

Medi-

um K

= 80

MN/m

3

Low

K =

40

MN/

m

3

Ultra-
low K

= 20

MN/m

3

High

CBR =

15%

Medi-

um

CBR =

10%

Low

CBR =

6%

Very

low

CBR =

3%

 

lbs

kgs

psi

kg/c

m

2

mPa

A

B

C

D

A

B

C

D

1

2

3

4

5

6

7

8

9

10

11

12

13

14

15

Dornier

328-100

30247
19423

13720

8810

46.2

116

8.15

0.80

7.6
4.5

8.1
4.8

8.5
5.1

8.9
5.4

6.3
3.8

7.0
4.1

8.1
4.5

9.1
5.5

Embraer EMB

120 RT

25529
17066

11580

7750

47.4

115

8.09

0.80

6.4
3.9

6.8
4.2

7.2
4.5

7.5
4.7

5.3
3.3

5.8
3.6

6.6
4.0

7.7
4.8

Embraer EMB

120 ER

26609
17213

12070

7808

47.4

127

8.93

0.88

6.9
4.1

7.3
4.4

7.7
4.6

8.0
4.9

5.8
3.4

6.1
3.7

7.0
4.1

8.0
4.8

Embraer ERJ

135 ER

42108
25353

19100
11500

92.42

134

9.42

0.92

10.7

5.7

11.3

6.0

12.0

6.3

13.0

7.0

9.2
4.8

9.8
5.1

11.2

5.6

13.0

7.0

Embraer ERJ

135 LR

44313
25353

20100
11500

93.42

148 10.41 1.02

11.7

5.7

12.3

6.1

12.9

6.5

14.0

7.0

10.0

5.0

10.5

5.2

12.0

5.7

14.0

7.0

Embraer ERJ

140 ER

44533
26455

20200
12000

93.7

145 10.19 1.00

11.7

6.2

12.4

6.5

13.0

7.0

14.0

7.0

10.0

5.1

10.5

5.3

12.0

6.2

14.0

7.0

AIRPORT DATA - GENERAL

1603

ACN TABLES

Aircraft Type

All-up Mass

1

(Maximum

Apron Mass)

(Operating

Mass Empty)

Load

on

one

main

gear

leg

(%)

Standard Aircraft

Tire Pressure

ACN relative to

Rigid Pavement Subgrades

Flexible Pavement Subgrades

High K

= 150

MN/m

3

Medi-

um K

= 80

MN/m

3

Low

K =

40

MN/

m

3

Ultra-
low K

= 20

MN/m

3

High

CBR =

15%

Medi-

um

CBR =

10%

Low

CBR =

6%

Very

low

CBR =

3%

 

lbs

kgs

psi

kg/c

m

2

mPa

A

B

C

D

A

B

C

D

1

2

3

4

5

6

7

8

9

10

11

12

13

14

15

Embraer ERJ

140 LR

46738
26455

21200
12000

93.7

148 10.41 1.02

12.6

6.3

13.1

6.7

13.7

7.0

14.0

7.0

10.7

5.1

11.1

5.3

12.6

6.2

14.0

7.0

Embraer ERJ

145 EP

46495
25772

21090
11690

94.4

142

9.98

0.98

12.5

6.2

13.3

6.6

13.8

7.0

15.0

7.0

10.8

5.3

11.4

5.7

13.1

6.2

15.0

7.0

Embraer ERJ

145 ER

45635
25573

20700
11600

47.2

139

9.77

0.95

12.2

6.1

12.9

6.5

13.6

6.9

14.0

7.0

10.5

5.3

11.1

5.6

12.7

6.1

14.0

7.0

Embraer ERJ

145 EU

44291
25772

20090
11690

94.4

139

9.77

0.95

11.8

6.1

12.5

6.5

13.1

6.9

14.0

7.0

10.2

5.3

10.7

5.6

12.3

6.1

13.0

7.0

Embraer ERJ

145 LR/LU

48722
27227

22100
12350

93.8

150 10.55 1.03

13.4

6.7

14.2

7.0

14.8

7.5

15.0

8.0

11.6

3.5

12.2

3.7

13.8

4.0

16.0

5.0

Embraer ERJ

145 MK

44291
29321

20090
13300

93.8

150 10.55 1.03

10.2

5.7

10.7

5.9

12.2

6.6

14.0

8.0

10.2

5.7

10.7

5.9

12.2

6.5

14.0

8.0

AIRPORT DATA - GENERAL

1604

ACN TABLES

Aircraft Type

All-up Mass

1

(Maximum

Apron Mass)

(Operating

Mass Empty)

Load

on

one

main

gear

leg

(%)

Standard Aircraft

Tire Pressure

ACN relative to

Rigid Pavement Subgrades

Flexible Pavement Subgrades

High K

= 150

MN/m

3

Medi-

um K

= 80

MN/m

3

Low

K =

40

MN/

m

3

Ultra-
low K

= 20

MN/m

3

High

CBR =

15%

Medi-

um

CBR =

10%

Low

CBR =

6%

Very

low

CBR =

3%

 

lbs

kgs

psi

kg/c

m

2

mPa

A

B

C

D

A

B

C

D

1

2

3

4

5

6

7

8

9

10

11

12

13

14

15

Embraer ERJ

145 MP

46495
28219

21090
12800

93.8

147 10.34 1.01

12.1

6.3

12.8

6.7

13.5

7.2

14.0

8.0

10.5

5.4

11.1

5.7

12.6

6.3

14.0

7.0

Embraer ERJ

145 XR

53131
28219

24100
12800

93.47

175 12.30 1.21

15.0

7.1

15.7

7.6

16.4

7.9

17.0

8.0

12.8

6.1

13.2

6.2

15.1

6.9

17.0

8.0

Embraer E

170 AR

85451
48061

38760
21800

45.55

136

9.56

0.94

19.7

9.7

21.2
10.5

22.6
11.2

24.0
12.0

17.8

8.9

18.8

9.4

21.3
10.2

25.0
12.0

44.47

Embraer E

170 LR

82365
48061

37360
21800

45.8

131

9.21

0.90

18.7

9.2

20.2

9.9

21.6
10.7

23.0
11.0

17.1

8.4

18.0

8.9

20.4

9.7

24.0
11.0

42.75

Embraer E

170 STD

79697
48061

36150
21800

45.8

131

9.21

0.90

18.0

9.2

19.4

9.9

20.8
10.7

22.0
11.0

16.5

8.4

17.3

8.9

19.5

9.7

23.0
11.0

42.75

Embraer E

175 AR

89353
49604

40530
22500

46.01

141

9.91

0.97

21.2

9.9

22.8
10.6

24.3
11.4

26.0
12.0

19.3

9.1

20.2

9.4

22.8
10.3

26.0
12.0

43.21

AIRPORT DATA - GENERAL

1605

ACN TABLES

Aircraft Type

All-up Mass

1

(Maximum

Apron Mass)

(Operating

Mass Empty)

Load

on

one

main

gear

leg

(%)

Standard Aircraft

Tire Pressure

ACN relative to

Rigid Pavement Subgrades

Flexible Pavement Subgrades

High K

= 150

MN/m

3

Medi-

um K

= 80

MN/m

3

Low

K =

40

MN/

m

3

Ultra-
low K

= 20

MN/m

3

High

CBR =

15%

Medi-

um

CBR =

10%

Low

CBR =

6%

Very

low

CBR =

3%

 

lbs

kgs

psi

kg/c

m

2

mPa

A

B

C

D

A

B

C

D

1

2

3

4

5

6

7

8

9

10

11

12

13

14

15

Embraer E

175 LR

85870
49604

38950
22500

45.8

136

9.56

0.94

19.9

9.8

21.5
10.5

22.9
11.3

24.0
12.0

18.0

9.0

19.1

9.4

21.6
10.3

25.0
12.0

43.25

Embraer E

175 STD

83026
49604

37660
22500

45.94

136

9.56

0.94

19.2

9.8

20.7
10.5

22.0
11.3

23.0
12.0

17.3

9.0

18.4

9.4

20.7
10.3

24.0
12.0

43.25

Embraer E

175 E2

98767
57761

44800
26200

45.37

150 10.55 1.03

23.2
12.3

25.0
13.2

26.6
14.1

28.0
15.0

21.3
11.4

22.1
11.7

24.9
12.8

29.0
15.0

44.99

Embraer E

190 AR

114552

65036

51960
29500

46.1

151 10.62 1.04

26.4
13.2

28.4
14.2

30.3
15.3

32.0
16.0

24.5
12.3

25.4
12.5

28.2
13.6

33.0
15.0

44.9

Embraer E

190 LR

111245

65036

50460
29500

46.2

151 10.62 1.04

25.5
13.2

27.5
14.2

29.4
15.3

31.0
16.0

23.7
12.3

24.6
12.5

27.2
13.6

32.0
15.0

44.9

Embraer E

190 STD

105712

65037

47950
29500

46.3

151 10.62 1.04

24.1
13.2

26.0
14.2

27.7
15.3

29.0
16.0

22.4
12.3

23.1
12.5

25.5
13.6

30.0
15.0

44.9

AIRPORT DATA - GENERAL

1606

ACN TABLES

Aircraft Type

All-up Mass

1

(Maximum

Apron Mass)

(Operating

Mass Empty)

Load

on

one

main

gear

leg

(%)

Standard Aircraft

Tire Pressure

ACN relative to

Rigid Pavement Subgrades

Flexible Pavement Subgrades

High K

= 150

MN/m

3

Medi-

um K

= 80

MN/m

3

Low

K =

40

MN/

m

3

Ultra-
low K

= 20

MN/m

3

High

CBR =

15%

Medi-

um

CBR =

10%

Low

CBR =

6%

Very

low

CBR =

3%

 

lbs

kgs

psi

kg/c

m

2

mPa

A

B

C

D

A

B

C

D

1

2

3

4

5

6

7

8

9

10

11

12

13

14

15

Embraer E

190 E2

124782

72091

56600
32700

 

152 10.69 1.05

29.2
15.0

31.4
16.1

33.5
17.3

35.0
18.0

27.1
14.3

28.1
14.6

31.4
15.8

37.0
18.0

Embraer E

195 AR

115632

65037

52450
29500

46.8

154 10.83 1.06

27.4
13.4

29.4
14.4

31.4
15.4

33.0
16.0

25.3
12.7

26.2
13.0

29.2
14.0

34.0
16.0

45.2

Embraer E

195 LR

112326

65037

50950
29500

46.8

154 10.83 1.06

26.5
13.4

28.4
14.4

30.3
15.4

32.0
16.0

24.5
12.7

25.4
13.0

28.2
14.0

33.0
16.0

45.2

Embraer E

195 E2

136025

76500

61700
34700

46.45

170 11.95 1.17

34.0
17.1

36.3
18.3

38.4
19.4

40.0
21.0

31.1
16.1

32.0
16.1

35.8
17.5

41.0
20.0

46.0

Embraer ERJ

195 STD

107916

65037

48950
29500

46.8

154 10.82 1.06

25.2
13.4

27.1
14.4

28.9
15.4

31.0
16.0

23.4
12.7

24.2
13.0

26.8
14.0

31.0
16.0

45.2

AIRPORT DATA - GENERAL

1607

ACN TABLES

Aircraft Type

All-up Mass

1

(Maximum

Apron Mass)

(Operating

Mass Empty)

Load

on

one

main

gear

leg

(%)

Standard Aircraft

Tire Pressure

ACN relative to

Rigid Pavement Subgrades

Flexible Pavement Subgrades

High K

= 150

MN/m

3

Medi-

um K

= 80

MN/m

3

Low

K =

40

MN/

m

3

Ultra-
low K

= 20

MN/m

3

High

CBR =

15%

Medi-

um

CBR =

10%

Low

CBR =

6%

Very

low

CBR =

3%

 

lbs

kgs

psi

kg/c

m

2

mPa

A

B

C

D

A

B

C

D

1

2

3

4

5

6

7

8

9

10

11

12

13

14

15

Fokker 27

Standard

Mk

200/400/500/

600

45000
25000

20412
11340

47.35

80

5.62

0.55

10

5

11

5

12

6

13

6

8
4

10

5

12

6

14

7

Fokker 27

RFV

Mk

200/400/500/

600

45000
25000

20412
11340

47.3

58

4.08

0.40

8
4

9
5

10

5

11

6

6
3

8
4

11

5

13

6

Fokker 28

Mk 1000 High

Tire Pressure

66500
35000

30164
15876

46.4

100

7.03

0.69

15

7

16

8

17

8

18

9

12

6

15

7

17

8

20
10

Fokker 28

Mk 1000 Low
Tire Pressure

66500
33500

30164
15876

46.4

70

4.92

0.48

13

6

14

7

16

7

17

8

10

5

13

6

16

7

19

9

AIRPORT DATA - GENERAL

1608

ACN TABLES

Aircraft Type

All-up Mass

1

(Maximum

Apron Mass)

(Operating

Mass Empty)

Load

on

one

main

gear

leg

(%)

Standard Aircraft

Tire Pressure

ACN relative to

Rigid Pavement Subgrades

Flexible Pavement Subgrades

High K

= 150

MN/m

3

Medi-

um K

= 80

MN/m

3

Low

K =

40

MN/

m

3

Ultra-
low K

= 20

MN/m

3

High

CBR =

15%

Medi-

um

CBR =

10%

Low

CBR =

6%

Very

low

CBR =

3%

 

lbs

kgs

psi

kg/c

m

2

mPa

A

B

C

D

A

B

C

D

1

2

3

4

5

6

7

8

9

10

11

12

13

14

15

Fokker 28

Mk 2000 High

Tire Pressure

65000
35000

29484
15876

46.9

102

7.17

0.70

15

7

17

7

17

8

19

9

13

6

15

7

18

8

20

9

Fokker 28

Mk 2000 Low
Tire Pressure

65000
35000

29484
15876

46.9

71

5.00

0.49

13

6

15

7

16

8

17

8

10

5

13

6

17

7

20

9

Fokker 28

Mk

3000/4000

High Tire
Pressure

73000
38000

33113
17240

46.5

101

7.10

0.70

17

8

18

8

19

9

20
10

14

7

17

8

19

9

22
10

Fokker 28

Mk

3000/4000

Low Tire

Pressure

73000
38000

33113
17240

46.5

78

5.48

0.54

15

7

17

8

18

8

19

9

13

6

16

7

19

8

22
10

AIRPORT DATA - GENERAL

1609

ACN TABLES

Aircraft Type

All-up Mass

1

(Maximum

Apron Mass)

(Operating

Mass Empty)

Load

on

one

main

gear

leg

(%)

Standard Aircraft

Tire Pressure

ACN relative to

Rigid Pavement Subgrades

Flexible Pavement Subgrades

High K

= 150

MN/m

3

Medi-

um K

= 80

MN/m

3

Low

K =

40

MN/

m

3

Ultra-
low K

= 20

MN/m

3

High

CBR =

15%

Medi-

um

CBR =

10%

Low

CBR =

6%

Very

low

CBR =

3%

 

lbs

kgs

psi

kg/c

m

2

mPa

A

B

C

D

A

B

C

D

1

2

3

4

5

6

7

8

9

10

11

12

13

14

15

Fokker 50

High Tire
Pressure

45900
27886

20820
12649

47.8

{85

80

5.98
5.62

0.59}

0.55

10

6

11

6

12

7

13

7

8
5

10

5

12

6

14

8

Fokker 50

Low Tire

Pressure

45900
27886

20820
12649

47.8

60

4.22

0.41

9
5

10

5

11

6

12

7

6
4

9
5

11

6

14

8

Fokker 100

98500
53736

44680
24375

47.8

142

9.98

0.98

28
13

29
14

31
15

32
16

25
12

27
13

30
14

32
16

Lockheed

L-100-20

155800

75409

70670
34205

24.1

105

7.38

0.72

30
14

33
15

36
16

38
17

27
12

31
14

33
15

38
16

Lockheed

L-100-30

155800

76502

70670
34701

24.2

105

7.38

0.72

30
14

33
15

36
16

38
17

27
12

31
14

33
15

39
17

AIRPORT DATA - GENERAL

1610

ACN TABLES

Aircraft Type

All-up Mass

1

(Maximum

Apron Mass)

(Operating

Mass Empty)

Load

on

one

main

gear

leg

(%)

Standard Aircraft

Tire Pressure

ACN relative to

Rigid Pavement Subgrades

Flexible Pavement Subgrades

High K

= 150

MN/m

3

Medi-

um K

= 80

MN/m

3

Low

K =

40

MN/

m

3

Ultra-
low K

= 20

MN/m

3

High

CBR =

15%

Medi-

um

CBR =

10%

Low

CBR =

6%

Very

low

CBR =

3%

 

lbs

kgs

psi

kg/c

m

2

mPa

A

B

C

D

A

B

C

D

1

2

3

4

5

6

7

8

9

10

11

12

13

14

15

Lockheed

L-1011-1

432000
240000

19595

2

10886

2

47.4

193 13.56 1.33

45
24

52
25

62
28

73
33

52
25

56
27

66
29

91
38

Lockheed

L-1011-100/2

00

468000
244682

21228

1

11098

6

46.8

175 12.34 1.21

46
23

55
24

66
28

78
32

56
25

61
26

73
30

100

38

Lockheed

L-1011-500

498000
240136

22588

9

10892

4

46.2

184 12.95 1.27

50
23

59
24

72
27

84
31

60
25

65
26

79
28

107

36

YS-11A

51800
34170

23500
15500

45.11

77

5.40

0.53

9
5

10

5

11

6

12

6

8
6

10

7

11

8

13

9

AIRPORT DATA - GENERAL

1611

ACN TABLES

Aircraft Type

All-up Mass

1

(Maximum

Apron Mass)

(Operating

Mass Empty)

Load

on

one

main

gear

leg

(%)

Standard Aircraft

Tire Pressure

ACN relative to

Rigid Pavement Subgrades

Flexible Pavement Subgrades

High K

= 150

MN/m

3

Medi-

um K

= 80

MN/m

3

Low

K =

40

MN/

m

3

Ultra-
low K

= 20

MN/m

3

High

CBR =

15%

Medi-

um

CBR =

10%

Low

CBR =

6%

Very

low

CBR =

3%

 

lbs

kgs

psi

kg/c

m

2

mPa

A

B

C

D

A

B

C

D

1

2

3

4

5

6

7

8

9

10

11

12

13

14

15

Ilyushin

IL-18

142197

73854

64500
33500

47.0

133

9.38

0.92

16

7

20

8

24
10

27
11

18

8

19

8

24

9

31
13

Ilyushin

IL-62M

370373
157408

16800

0

71400

47.0

157 11.01 1.08

43
16

52
17

62
19

71
22

50
17

57
18

67
20

83
26

Ilyushin

IL-62

358468
146387

16260

0

66400

47.0

157 11.01 1.08

42
14

50
15

60
18

69
20

47
16

54
16

64
18

79
24

Ilyushin

IL-76T

376986
184745

17100

0

83800

23.5

86

6.02

0.59

29
10

29
13

32
13

33
14

24

9

27
10

34
12

45
16

Ilyushin

IL-76TD

421078
192241

19100

0

87200

23.5

100

7.03

0.69

35
12

35
14

36
15

40
16

29
10

32
11

40
13

53
17

AIRPORT DATA - GENERAL

1612

ACN TABLES

Aircraft Type

All-up Mass

1

(Maximum

Apron Mass)

(Operating

Mass Empty)

Load

on

one

main

gear

leg

(%)

Standard Aircraft

Tire Pressure

ACN relative to

Rigid Pavement Subgrades

Flexible Pavement Subgrades

High K

= 150

MN/m

3

Medi-

um K

= 80

MN/m

3

Low

K =

40

MN/

m

3

Ultra-
low K

= 20

MN/m

3

High

CBR =

15%

Medi-

um

CBR =

10%

Low

CBR =

6%

Very

low

CBR =

3%

 

lbs

kgs

psi

kg/c

m

2

mPa

A

B

C

D

A

B

C

D

1

2

3

4

5

6

7

8

9

10

11

12

13

14

15

Ilyushin

IL-86

477295
244094

21650

0

11070

0

31.2

135

9.48

0.93

26
14

31
15

38
17

45
20

34
16

36
17

44
19

61
23

Ilyushin

IL-96

509355
245858

23100

0

11150

0

31.7

157 11.00 1.08

35
15

43
16

52
19

61
23

42
17

46
18

57
20

76
26

Ilyushin

IL-114

50164
31973

22750
14500

47.5

86

6.02

0.59

11

6

12

7

13

8

14

8

9
5

11

6

13

7

15

9

Saab 340B

28800
17715

13065

8035

46.5

115

8.09

0.79

7.4
4.6

7.9
4.8

8.3
5.1

8.6
5.3

6.1
3.8

6.8
4.2

7.8
4.8

9.0
5.5

Saab 2000

50706
30203

23000
13700

47.5

165 11.62 1.14

14.5

7.8

15.2

8.2

15.8

8.7

16.2

9.1

12.5

6.8

13.1

7.1

14.8

7.8

16.2

9.0

AIRPORT DATA - GENERAL

1613

ACN TABLES

Aircraft Type

All-up Mass

1

(Maximum

Apron Mass)

(Operating

Mass Empty)

Load

on

one

main

gear

leg

(%)

Standard Aircraft

Tire Pressure

ACN relative to

Rigid Pavement Subgrades

Flexible Pavement Subgrades

High K

= 150

MN/m

3

Medi-

um K

= 80

MN/m

3

Low

K =

40

MN/

m

3

Ultra-
low K

= 20

MN/m

3

High

CBR =

15%

Medi-

um

CBR =

10%

Low

CBR =

6%

Very

low

CBR =

3%

 

lbs

kgs

psi

kg/c

m

2

mPa

A

B

C

D

A

B

C

D

1

2

3

4

5

6

7

8

9

10

11

12

13

14

15

Sukhoi SSJ

100-95

101413

60627

46000
27500

 

161 11.32 1.11

27.0
13.5

28.6
14.5

30.1
15.4

31.3
16.2

23.8
12.2

24.8
12.5

28.0
13.7

31.5
16.0

Sukhoi SSJ

100-75

88185
60627

40000
27500

 

161 11.32 1.11

22.1
13.5

23.5
14.5

24.8
15.4

26.0
16.2

19.8
12.2

20.4
12.5

22.9
13.7

26.3
16.0

Tupolev

TU-134A

104940

64705

47600
29350

45.6

120

8.50

0.83

11

7

13

8

16

9

19
10

12

7

13

8

16

9

21
12

Tupolev

TU-154B

216050
117946

98000
53500

45.1

135

9.50

0.93

19

8

25
10

32
13

38
17

20
10

24
11

30
13

38
18

Tupolev

TU-204

206130
121187

93500
54970

45.4

199 13.97 1.37

23
12

27
14

32
16

37
18

25
13

28
14

33
15

43
20

Yakovlev

YAK-40

35274
21385

16000

9700

44.0

56

3.97

0.39

9
6

9
6

10

6

10

6

7
4

9
5

11

7

13

8

AIRPORT DATA - GENERAL

1614

ACN TABLES

Aircraft Type

All-up Mass

1

(Maximum

Apron Mass)

(Operating

Mass Empty)

Load

on

one

main

gear

leg

(%)

Standard Aircraft

Tire Pressure

ACN relative to

Rigid Pavement Subgrades

Flexible Pavement Subgrades

High K

= 150

MN/m

3

Medi-

um K

= 80

MN/m

3

Low

K =

40

MN/

m

3

Ultra-
low K

= 20

MN/m

3

High

CBR =

15%

Medi-

um

CBR =

10%

Low

CBR =

6%

Very

low

CBR =

3%

 

lbs

kgs

psi

kg/c

m

2

mPa

A

B

C

D

A

B

C

D

1

2

3

4

5

6

7

8

9

10

11

12

13

14

15

Yakovlev

YAK-42

124560

70106

56500
31800

47.0

127

8.97

0.88

13

6

16

7

20

9

23
10

15

7

16

8

20

9

26
11

1

 The two all-up masses shown in columns 2 and 3 for each aircraft type are respectively the Maximum Apron (ramp) Mass and a

representative Operating Mass Empty. To compute the ACN for any intermediate value, proceed on the assumption that the ACN
varies linearly between the Operating Mass Empty and the Maximum Apron Mass.

2

 Values reflect tire speeds up to 160 MPH (257 KMH). Higher tire pressure and higher speeds result in greater ACN.

3

 The tire pressure used are for tires with a maximum allowable ground speed of 160 MPH (257 KMH). Tires available for ground

speeds over 160 MPH (257 KHM) require tire pressure about 10.5% higher for standard tires and 17% higher for low pressure tires.

4

 Maximim Zero Fuel Weight. Operating Mass Empty not defined yet.

5

 Minimum weight used solely as a baseline for ACN curve generation. Operating Mass Empty not defined yet.

AIRPORT DATA - GENERAL

1615

ACN TABLES

Terminal

Terminal

Terminal Procedures - General

Information

VERTICAL DESCENT PLANNING

Vertical descent planning is a key component of the Constant Descent Final Approach (CDFA)
concept. When not otherwise included on an instrument approach chart, this reference table pro-
vides a method to easily determine a vertical descent angle with respect to a defined Height at the
FAF (

Above Ground Level – AGL) and the Distance to the Runway Threshold (Nautical Miles –

NM). The table includes a range of angles between 2.5 and 3.8 degrees.
To determine a vertical descent angle based upon a pre-defined combination of FAF Height
(AGL) and Distance to Runway Threshold, match the FAF height (AGL) value in the left column to
the corresponding Distance to Runway Threshold value in the top row. The value shown in the
box where the two lines cross represents the vertical descent angle (

in Degrees).

EXAMPLE:

TERMINAL PROCEDURES - GENERAL

INFORMATION

1618

VERTICAL DESCENT ANGLE REFERENCE TABLE

The table may also be used to determine a Height (AGL) at the FAF that would provide an opti-
mum descent angle of 3.0 degrees. First, determine the Distance FAF to Runway Threshold (NM)
in the top row, and then move down the table to the 3.0 degree value. Finally, move to the left to
determine the optimum FAF Height (AGL). (Refer to Note 4 below).
IMPORTANT NOTES:
NOTE 1: Angles are predicated on an assumed Threshold Crossing Height (TCH) of 50 feet.
NOTE 2: To determine the FAF Altitude as an Above Mean Sea Level value (AMSL), add the FAF
Height (AGL value) and the Touchdown Zone Elevation (TDZE).
NOTE 3: Vertical descent angle information obtained from this table is for REFERENCE USE
ONLY.
NOTE 4: ANY USE OF A HIGHER-THAN-PUBLISHED HEIGHT/ALTITUDE AT THE FINAL
APPROACH FIX (FAF) IS CONTINGENT UPON PRIOR APPROVAL BY AIR TRAFFIC CON-
TROL AND/OR CONFORMANCE WITH APPLICABLE OPERATING PROCEDURES.

TERMINAL PROCEDURES - GENERAL

INFORMATION

1619

VERTICAL DESCENT ANGLE REFERENCE TABLE

GROUNDSPEED IN KNOTS TO FEET PER NAUTICAL MILE

This table provides a rate of climb or descent in feet per minute below the GROUNDSPEED IN
KNOTS for the gradient shown in FEET PER NAUTICAL MILE at the left. Table accuracy is within
one foot per nautical mile. This table is for use in climbs, descents from altitude and non-precision
instrument approach procedures. This table does not consider the earth’s curvature as a factor.
The earth’s curvature is considered when using fixed glide slope (ILS/PAR). Procedures utilizing a
fixed glide slope have slightly higher figures to reflect the earth’s curvature.

GRADIENT

GROUNDSPEED IN KNOTS

FEET PER NM

70

75

90

100

120

140

150

160

180

200

250

300

152

177 190

228

253

304

355

380

405

456

507

633

760

160

187 200

240

267

320

373

400

427

480

533

667

800

170

198 213

255

283

340

397

425

453

510

567

708

850

180

210 225

270

300

360

420

450

480

540

600

750

900

190

222 238

285

317

380

443

475

507

570

633

792

950

200

233 250

300

333

400

467

500

533

600

667

833 1000

210

245 263

315

350

420

490

525

560

630

700

875 1050

220

257 275

330

367

440

513

550

587

660

733

917 1100

230

268 288

345

383

460

537

575

613

690

767

958 1150

240

280 300

360

400

480

560

600

640

720

800 1000 1200

250

292 313

375

417

500

583

625

667

750

833 1042 1250

260

303 325

390

433

520

607

650

693

780

867 1083 1300

270

315 338

405

450

540

630

675

720

810

900 1125 1350

280

327 350

420

467

560

653

700

747

840

933 1167 1400

290

338 363

435

483

580

677

725

773

870

967 1208 1450

300

350 375

450

500

600

700

750

800

900 1000 1250 1500

310

362 388

465

517

620

723

775

827

930 1033 1292 1550

320

373 400

480

533

640

747

800

853

960 1067 1333 1600

330

385 413

495

550

660

770

825

880

990 1100 1375 1650

340

397 425

510

567

680

793

850

907 1020 1133 1417 1700

350

408 438

525

583

700

817

875

933 1050 1167 1458 1750

360

420 450

540

600

720

840

900

960 1080 1200 1500 1800

370

432 463

555

617

740

863

925

987 1110 1233 1542 1850

TERMINAL PROCEDURES - GENERAL

INFORMATION

1620

GRADIENT TO RATE TABLE

GRADIENT

GROUNDSPEED IN KNOTS

FEET PER NM

70

75

90

100

120

140

150

160

180

200

250

300

380

443 475

570

633

760

887

950 1013 1140 1267 1583 1900

390

455 488

585

650

780

910

975 1040 1170 1300 1625 1950

400

467 500

600

667

800

933 1000 1067 1200 1333 1667 2000

410

478 513

615

683

820

957 1025 1093 1230 1367 1708 2050

420

490 525

630

700

840

980 1050 1120 1260 1400 1750 2100

430

502 538

645

717

860 1003 1075 1147 1290 1433 1792 2150

440

513 550

660

733

880 1027 1100 1173 1320 1467 1833 2200

450

525 563

675

750

900 1050 1125 1200 1350 1500 1875 2250

460

537 575

690

767

920 1073 1150 1227 1380 1533 1917 2300

470

548 588

705

783

940 1097 1175 1253 1410 1567 1958 2350

480

560 600

720

800

960 1120 1200 1280 1440 1600 2000 2400

490

572 613

735

817

980 1143 1225 1307 1470 1633 2042 2450

500

583 625

750

833 1000 1167 1250 1333 1500 1667 2083 2500

510

595 638

765

850 1020 1190 1275 1360 1530 1700 2125 2550

520

607 650

780

867 1040 1213 1300 1387 1560 1733 2167 2600

530

618 663

795

883 1060 1237 1325 1413 1590 1767 2208 2650

540

630 675

810

900 1080 1260 1350 1440 1620 1800 2250 2700

550

642 688

825

917 1100 1283 1375 1467 1650 1833 2292 2750

560

653 700

840

933 1120 1307 1400 1493 1680 1867 2333 2800

570

665 713

855

950 1140 1330 1425 1520 1710 1900 2375 2850

580

677 725

870

967 1160 1353 1450 1547 1740 1933 2417 2900

590

688 738

885

983 1180 1377 1475 1573 1770 1967 2458 2950

600

700 750

900 1000 1200 1400 1500 1600 1800 2000 2500 3000

610

712 763

915 1017 1220 1423 1525 1627 1830 2033 2542 3050

620

723 775

930 1033 1240 1447 1550 1653 1860 2067 2583 3100

630

735 788

945 1050 1260 1470 1575 1680 1890 2100 2625 3150

640

747 800

960 1067 1280 1493 1600 1707 1920 2133 2667 3200

650

758 813

975 1083 1300 1517 1625 1733 1950 2167 2708 3250

660

770 825

990 1100 1320 1540 1650 1760 1980 2200 2750 3300

TERMINAL PROCEDURES - GENERAL

INFORMATION

1621

GRADIENT TO RATE TABLE

GRADIENT

GROUNDSPEED IN KNOTS

FEET PER NM

70

75

90

100

120

140

150

160

180

200

250

300

670

782 838 1005 1117 1340 1563 1675 1787 2010 2233 2792 3350

680

793 850 1020 1133 1360 1587 1700 1813 2040 2267 2833 3400

690

805 863 1035 1150 1380 1610 1725 1840 2070 2300 2875 3450

700

817 875 1050 1167 1400 1633 1750 1867 2100 2333 2917 3500

710

828 888 1065 1183 1420 1657 1775 1893 2130 2367 2958 3550

720

840 900 1080 1200 1440 1680 1800 1920 2160 2400 3000 3600

GROUNDSPEED IN KNOTS TO GRADIENT IN PERCENTAGE

This table provides a rate of climb or descent in feet per minute below the GROUNDSPEED IN
KNOTS for the gradient shown in PERCENT (%) at the left. This table is for use in climbs,
descents from altitude and non-precision instrument approach procedures. Table accuracy is
within four feet per nautical mile. This table does not consider the earth’s curvature as a factor.
The earth’s curvature is considered when using fixed glide slopes (ILS/PAR). Procedures utilizing
a fixed glide slope have slightly higher figures to reflect the earth’s curvature.

GRADI-

ENT

GROUNDSPEED IN KNOTS

%

70

75

90

100

120

140

150

160

180

200

250

300

2.5

177

190

228

253

304

354

380

405

456

506

633

760

2.6

184

197

237

263

316

369

395

421

474

527

658

790

2.7

191

205

246

273

328

383

410

437

492

547

684

820

2.8

198

213

255

284

340

397

425

454

510

567

709

851

2.9

206

220

264

294

352

411

441

470

529

587

734

881

3.0

213

228

273

304

365

425

456

486

547

608

760

911

3.1

220

235

283

314

377

440

471

502

565

628

785

942

3.2

227

243

292

324

389

454

486

519

583

648

810

972

3.3

234

251

301

334

401

468

501

535

602

668

835 1003

3.4

241

258

310

344

413

482

516

551

620

689

861 1033

3.5

248

266

319

354

425

496

532

567

638

709

886 1063

3.6

255

273

328

365

437

510

547

583

656

729

911 1094

3.7

262

281

337

375

450

525

562

600

674

749

937 1124

3.8

269

289

346

385

462

539

577

616

693

770

962 1155

TERMINAL PROCEDURES - GENERAL

INFORMATION

1622

GRADIENT TO RATE TABLE

GRADI-

ENT

GROUNDSPEED IN KNOTS

%

70

75

90

100

120

140

150

160

180

200

250

300

3.9

276

296

355

395

474

553

592

632

711

790

987 1185

4.0

284

304

365

405

486

567

608

648

729

810

1013 1215

4.1

291

311

374

415

498

581

623

664

747

830

1038 1246

4.2

298

319

383

425

510

595

638

681

766

851

1063 1276

4.3

305

327

392

435

523

610

653

697

784

871

1089 1306

4.4

312

334

401

446

535

624

668

713

802

891

1114 1337

4.5

319

342

410

456

547

638

684

729

820

911

1139 1367

4.6

326

349

419

466

559

652

699

745

839

932

1165 1398

4.7

333

357

428

476

571

666

714

762

857

952

1190 1428

4.8

340

365

437

486

583

681

729

778

875

972

1215 1458

4.9

347

372

447

496

595

695

744

794

893

992

1241 1489

5.0

354

380

456

506

608

709

760

810

911

1013 1266 1519

5.1

362

387

465

516

620

723

775

826

930

1033 1291 1549

5.2

369

395

474

527

632

737

790

843

948

1053 1317 1580

5.3

376

403

483

537

644

751

805

859

966

1073 1342 1610

5.4

383

410

492

547

656

766

820

875

984

1094 1367 1641

5.5

390

418

501

557

668

780

835

891

1003

1114 1392 1671

5.6

397

425

510

567

681

794

851

907

1021

1134 1418 1701

5.7

404

433

520

577

693

808

866

924

1039

1155 1443 1732

5.8

411

441

529

587

705

822

881

940

1057

1175 1468 1762

5.9

418

448

538

597

717

836

896

956

1075

1195 1494 1792

6.0

425

456

547

608

729

851

911

972

1094

1215 1519 1823

6.1

432

463

556

618

741

865

927

988

1112

1235 1544 1853

6.2

440

471

565

628

753

879

942

1005

1130

1256 1570 1884

6.3

447

479

574

638

766

893

957

1021

1148

1276 1595 1914

6.4

454

486

583

648

778

907

972

1037

1167

1296 1620 1944

6.5

461

494

592

658

790

922

987

1053

1185

1317 1646 1975

6.6

468

501

602

668

802

936

1003

1069

1203

1337 1671 2005

TERMINAL PROCEDURES - GENERAL

INFORMATION

1623

GRADIENT TO RATE TABLE

GRADI-

ENT

GROUNDSPEED IN KNOTS

%

70

75

90

100

120

140

150

160

180

200

250

300

6.7

475

509

611

679

814

950

1018

1086

1221

1357 1696 2036

6.8

482

516

620

689

826

964

1033

1102

1240

1377 1722 2066

6.9

489

524

629

699

839

978

1048

1118

1258

1398 1747 2096

7.0

496

532

638

709

851

992

1063

1134

1276

1418 1772 2127

7.1

503

539

647

719

863

1007

1079

1150

1294

1438 1798 2157

7.2

510

547

656

729

875

1021

1094

1167

1312

1458 1823 2187

7.3

517

554

665

739

887

1035

1109

1183

1331

1479 1848 2218

7.4

525

562

674

749

899

1049

1124

1199

1349

1499 1873 2248

7.5

532

570

684

760

911

1063

1139

1215

1367

1519 1899 2279

7.6

539

577

693

770

924

1078

1154

1231

1385

1539 1924 2309

7.7

546

585

702

780

936

1092

1170

1248

1404

1560 1949 2339

7.8

553

592

711

790

948

1106

1185

1264

1422

1580 1975 2370

7.9

560

600

720

800

960

1120

1200

1280

1440

1600 2000 2400

8.0

567

608

729

810

972

1134

1215

1296

1458

1620 2025 2430

8.1

574

615

738

820

984

1148

1230

1312

1477

1641 2051 2461

8.2

581

623

747

830

996

1163

1246

1329

1495

1661 2076 2491

8.3

588

630

756

841 1009 1177

1261

1345

1513

1681 2101 2522

8.4

595

638

766

851 1021 1191

1276

1361

1531

1701 2127 2552

8.5

603

646

775

861 1033 1205

1291

1377

1549

1722 2152 2582

8.6

610

653

784

871 1045 1219

1306

1393

1568

1742 2177 2613

8.7

617

661

793

881 1057 1233

1322

1410

1586

1762 2203 2643

8.8

624

668

802

891 1069 1248

1337

1426

1604

1782 2228 2674

8.9

631

676

811

901 1082 1262

1352

1442

1622

1803 2253 2704

9.0

638

684

820

911 1094 1276

1367

1458

1641

1823 2279 2734

9.1

645

691

829

922 1106 1290

1382

1474

1659

1843 2304 2765

9.2

652

699

839

932 1118 1304

1398

1491

1677

1863 2329 2795

9.3

659

706

848

942 1130 1319

1413

1507

1695

1884 2355 2825

9.4

666

714

857

952 1142 1333

1428

1523

1713

1904 2380 2856

TERMINAL PROCEDURES - GENERAL

INFORMATION

1624

GRADIENT TO RATE TABLE

GRADI-

ENT

GROUNDSPEED IN KNOTS

%

70

75

90

100

120

140

150

160

180

200

250

300

9.5

673

722

866

962 1154 1347

1443

1539

1732

1924 2405 2886

9.6

681

729

875

972 1167 1361

1458

1556

1750

1944 2430 2917

9.7

688

737

884

982 1179 1375

1473

1572

1768

1965 2456 2947

9.8

695

744

893

992 1191 1389

1489

1588

1786

1985 2481 2977

9.9

702

752

902 1003 1203 1404

1504

1604

1805

2005 2506 3008

10.0

709

760

911 1013 1215 1418

1519

1620

1823

2025 2532 3038

10.1

716

767

921 1023 1227 1432

1534

1637

1841

2046 2557 3068

10.2

723

775

930 1033 1240 1446

1549

1653

1859

2066 2582 3099

10.3

730

782

939 1043 1252 1460

1565

1669

1878

2086 2608 3129

10.4

737

790

948 1053 1264 1474

1580

1685

1896

2106 2633 3160

10.5

744

798

957 1063 1276 1489

1595

1701

1914

2127 2658 3190

10.6

751

805

966 1073 1288 1503

1610

1718

1932

2147 2684 3220

10.7

759

813

975 1084 1300 1517

1625

1734

1950

2167 2709 3251

10.8

766

820

984 1094 1312 1531

1641

1750

1969

2187 2734 3281

10.9

773

828

993 1104 1325 1545

1656

1766

1987

2208 2760 3312

11.0

780

835 1003 1114 1337 1560

1671

1782

2005

2228 2785 3342

11.1

787

843 1012 1124 1349 1574

1686

1799

2023

2248 2810 3372

11.2

794

851 1021 1134 1361 1588

1701

1815

2042

2268 2836 3403

11.3

801

858 1030 1144 1373 1602

1717

1831

2060

2289 2861 3433

11.4

808

866 1039 1154 1385 1616

1732

1847

2078

2309 2886 3463

11.5

815

873 1048 1165 1398 1630

1747

1863

2096

2329 2912 3494

11.6

822

881 1057 1175 1410 1645

1762

1880

2115

2349 2937 3524

11.7

829

889 1066 1185 1422 1659

1777

1896

2133

2370 2962 3555

11.8

836

896 1075 1195 1434 1673

1792

1912

2151

2390 2987 3585

11.9

844

904 1085 1205 1446 1687

1808

1928

2169

2410 3013 3615

12.0

851

911 1094 1215 1458 1701

1823

1944

2187

2430 3038 3646

12.1

858

919 1103 1225 1470 1716

1838

1961

2206

2451 3063 3676

12.2

865

927 1112 1235 1483 1730

1853

1977

2224

2471 3089 3706

TERMINAL PROCEDURES - GENERAL

INFORMATION

1625

GRADIENT TO RATE TABLE

GRADI-

ENT

GROUNDSPEED IN KNOTS

%

70

75

90

100

120

140

150

160

180

200

250

300

12.3

872

934 1121 1246 1495 1744

1868

1993

2242

2491 3114 3737

12.4

879

942 1130 1256 1507 1758

1884

2009

2260

2511 3139 3767

12.5

886

949 1139 1266 1519 1772

1899

2025

2279

2532 3165 3798

12.6

893

957 1148 1276 1531 1786

1914

2042

2297

2552 3190 3828

12.7

900

965 1158 1286 1543 1801

1929

2058

2315

2572 3215 3858

12.8

907

972 1167 1296 1556 1815

1944

2074

2333

2593 3241 3889

12.9

914

980 1176 1306 1568 1829

1960

2090

2351

2613 3266 3919

13.0

922

987 1185 1317 1580 1843

1975

2106

2370

2633 3291 3950

13.1

929

995 1194 1327 1592 1857

1990

2123

2388

2653 3317 3980

13.2

936 1003 1203 1337 1604 1871

2005

2139

2406

2674 3342 4010

13.3

943 1010 1212 1347 1616 1886

2020

2155

2424

2694 3367 4041

13.4

950 1018 1221 1357 1628 1900

2036

2171

2443

2714 3393 4071

13.5

957 1025 1230 1367 1641 1914

2051

2187

2461

2734 3418 4101

13.6

964 1033 1240 1377 1653 1928

2066

2204

2479

2754 3443 4132

13.8

978 1048 1258 1397 1677 1956

2096

2236

2515

2795 3494 4192

14.0

992 1063 1276 1418 1701 1985

2127

2268

2552

2835 3544 4253

14.2

1007 1078 1294 1438 1726 2013

2157

2301

2588

2876 3595 4314

14.4

1021 1094 1312 1458 1750 2042

2187

2333

2625

2916 3646 4375

14.6

1035 1109 1331 1478 1774 2070

2218

2366

2661

2957 3696 4435

14.8

1049 1124 1349 1499 1798 2098

2248

2398

2698

2997 3747 4496

15.0

1063 1139 1367 1519 1823 2127

2279

2430

2734

3038 3798 4557

15.2

1007 1154 1385 1539 1847 2155

2309

2463

2771

3079 3848 4618

15.4

1092 1170 1404 1560 1871 2183

2339

2495

2807

3119 3899 4679

15.6

1106 1185 1422 1580 1896 2212

2370

2528

2844

3160 3949 4739

15.8

1120 1200 1440 1600 1920 2240

2400

2560

2880

3200 4000 4800

16.0

1134 1215 1458 1620 1944 2268

2430

2592

2916

3241 4051 4861

16.2

1148 1230 1476 1641 1969 2297

2461

2625

2953

3281 4101 4922

16.4

1163 1246 1495 1661 1993 2325

2491

2657

2989

3322 4152 4982

TERMINAL PROCEDURES - GENERAL

INFORMATION

1626

GRADIENT TO RATE TABLE

GRADI-

ENT

GROUNDSPEED IN KNOTS

%

70

75

90

100

120

140

150

160

180

200

250

300

16.6

1177 1261 1513 1681 2017 2353

2522

2690

3026

3362 4203 5043

16.8

1191 1276 1531 1701 2042 2382

2552

2722

3062

3403 4253 5104

17.0

1205 1291 1549 1722 2066 2410

2582

2754

3099

3443 4304 5165

17.2

1219 1306 1568 1742 2090 2439

2613

2787

3135

3484 4354 5225

17.4

1233 1322 1586 1762 2114 2467

2643

2819

3172

3524 4405 5286

17.6

1248 1337 1604 1782 2139 2495

2673

2852

3208

3565 4456 5347

17.8

1262 1352 1622 1803 2163 2524

2704

2884

3245

3605 4506 5408

18.0

1276 1367 1641 1823 2187 2552

2734

2916

3281

3646 4557 5468

18.2

1290 1382 1659 1843 2212 2580

2765

2949

3317

3686 4608 5529

18.4

1304 1397 1677 1863 2236 2609

2795

2981

3354

3727 4658 5590

18.6

1318 1413 1695 1884 2260 2637

2825

3014

3390

3767 4709 5651

18.8

1333 1428 1713 1904 2285 2665

2856

3046

3427

3808 4760 5711

19.0

1347 1443 1732 1924 2309 2694

2886

3079

3463

3848 4810 5772

TERMINAL PROCEDURES - GENERAL

INFORMATION

1627

GRADIENT TO RATE TABLE

CORRECTION FACTOR

This table provides a correction factor in Hectopascals or Millibars for elevations on an airport.
Application of the factor in this table will provide a QFE altimeter setting. To use the table, deter-
mine the correction factor by finding the elevation in hundreds of feet in the left column and read-
ing across to the nearest ten feet. For example 1220 feet equals -43.9. Subtract 43.9 from your
current Hectopascal or Millibar altimeter setting and your altimeter shall read “zero” on the sur-
face.

Elev

-200

-190

-180

-170

-160

-150

-140

-130

-120

-110

7.3

7.0

6.6

6.2

5.9

5.5

5.1

4.8

4.4

4.0

Elev

-100

-90

-80

-70

-60

-50

-40

-30

-20

-10

3.7

3.3

2.9

2.6

2.2

1.8

1.5

1.1

0.7

0.4

Elev

+00

+10

+20

+30

+40

+50

+60

+70

+80

+90

0

0.0

-0.4

-0.7

-1.1

-1.5

-1.8

-2.2

-2.6

-2.9

-3.3

100

-3.7

-4.0

-4.4

-4.8

-5.1

-5.5

-5.8

-6.2

-6.6

-6.9

200

-7.3

-7.7

-8.0

-8.4

-8.8

-9.1

-9.5

-9.8

-10.2

-10.6

300

-10.9

-11.3

-11.7

-12.0

-12.4

-12.8

-13.1

-13.5

-13.8

-14.2

400

-14.6

-14.9

-15.3

-15.6

-16.0

-16.4

-16.7

-17.1

-17.5

-17.8

500

-18.2

-18.5

-18.9

-19.3

-19.6

-20.0

-20.3

-20.7

-21.1

-21.4

600

-21.8

-22.1

-22.5

-22.9

-23.2

-23.6

-23.9

-24.3

-24.7

-25.0

700

-25.4

-25.7

-26.1

-26.4

-26.8

-27.2

-27.5

-27.9

-28.2

-28.6

800

-29.0

-29.3

-29.7

-30.0

-30.4

-30.7

-31.1

-31.5

-31.8

-32.2

900

-32.5

-32.9

-33.2

-33.6

-33.9

-34.3

-34.7

-35.0

-35.4

-35.7

1000

-36.1

-36.4

-36.8

-37.2

-37.5

37.9

-38.2

-38.6

-38.9

-39.3

1100

-39.6

-40.0

-40.3

-40.7

-41.1

-41.4

-41.8

-42.1

-42.5

-42.8

1200

-43.2

-43.5

-43.9

-44.2

-44.6

-44.9

-45.3

-45.6

-46.0

-46.4

1300

-46.7

-47.1

-47.4

-47.8

-48.1

-48.5

-48.8

-49.2

-49.5

-49.9

1400

-50.2

-50.6

-50.9

-51.3

-51.6

-52.0

-52.3

-52.7

-53.0

-53.4

1500

-53.7

-54.1

-54.4

-54.8

-55.1

-55.5

-55.8

-56.2

-56.5

-56.9

1600

-57.2

-57.6

-57.9

-58.3

-58.6

-59.0

-59.3

-59.7

-60.0

-60.4

1700

-60.7

-61.1

-61.4

-61.8

-62.1

-62.5

-62.8

-63.2

-63.5

-63.8

1800

-64.2

-64.5

-64.9

-65.2

-65.6

-65.9

-66.3

-66.6

-67.0

-67.3

1900

-67.7

-68.0

-68.4

-68.7

-69.0

-69.4

-69.7

-70.1

-70.4

70.8

TERMINAL PROCEDURES - GENERAL

INFORMATION

1628

HECTOPASCAL/MILLIBAR EQUIVALENT FOR AIRPORT ELEVATION

Elev

-200

-190

-180

-170

-160

-150

-140

-130

-120

-110

7.3

7.0

6.6

6.2

5.9

5.5

5.1

4.8

4.4

4.0

Elev

-100

-90

-80

-70

-60

-50

-40

-30

-20

-10

3.7

3.3

2.9

2.6

2.2

1.8

1.5

1.1

0.7

0.4

Elev

+00

+10

+20

+30

+40

+50

+60

+70

+80

+90

2000

-71.1

-71.5

-71.8

-72.2

-72.5

-72.8

-73.2

-73.5

-73.9

-74.2

2100

-74.6

-74.9

-75.3

-75.6

-75.9

-76.3

-76.6

-77.0

-77.3

-77.7

2200

-78.0

-78.3

-78.7

-79.0

-79.4

-79.7

-80.1

-80.4

-80.7

-81.1

2300

-81.4

-81.8

-82.1

-82.5

-82.8

-83.1

-83.5

-83.8

-84.2

-84.5

2400

-84.8

-85.2

-85.5

-85.9

-86.2

-86.6

-86.9

-87.2

-87.6

-87.9

2500

-88.3

-88.6

-88.9

-89.3

-89.6

-90.0

-90.3

-90.6

-91.0

-91.3

2600

-91.6

-92.0

-92.3

-92.7

-93.0

-93.3

-93.7

-94.0

-94.4

-94.7

2700

-95.0

-95.4

-95.7

-96.0

-96.4

-96.7

-97.1

-97.4

-97.7

-98.1

2800

-98.4

-98.7

-99.1

-99.4

-99.8 -100.1 -100.4

-100.8 -101.1 -101.4

2900

-101.8 -102.1 -102.4 -102.8 -103.1 -103.5 -103.8

-104.1 -104.5 -104.8

3000

-105.1 -105.5 -105.8 -106.1 -106.5 -106.8 -107.1

-107.5 -107.8 -108.1

3100

-108.5 -108.8 -109.1 -109.5 -109.8 -110.1 -110.5

-110.8 -111.1 -111.5

3200

-111.8 -112.1 -112.5 -112.8 -113.1 -113.5 -113.8

-114.1 -114.5 -114.8

3300

-115.1 -115.5 -115.8 -116.1 -116.5 -116.8 -117.1

-117.5 -117.8 -118.1

3400

-118.5 -118.8 -119.1 -119.4 -119.8 -120.1 -120.4

-120.8 -121.1 -121.4

3500

-121.8 -122.1 -122.4 -122.8 -123.1 -123.4 -123.7

-124.1 -124.4 -124.7

3600

-125.1 -125.4 -125.7 -126.0 -126.4 -126.7 -127.0

-127.4 -127.7 -128.0

3700

-128.3 -128.7 -129.0 -129.3 -129.7 -130.0 -130.3

-130.6 -131.0 -131.3

3800

-131.6 -131.9 -132.3 -132.6 -132.9 -133.3 -133.6

-133.9 -134.2 -134.5

3900

-134.9 -135.2 -135.5 -135.9 -136.2 -136.5 -136.8

-137.2 -137.5 -137.8

4000

-138.1 -138.5 -138.8 -139.1 -139.4 -139.8 -140.1

-140.4 -140.7 -141.1

4100

-141.4 -141.7 -142.0 -142.4 -142.7 -143.0 -143.3

-143.7 -144.0 -144.3

4200

-144.6 -145.0 -145.3 -145.6 -145.9 -146.2 -146.6

-146.9 -147.2 -147.5

4300

-147.9 -148.2 -148.5 -148.8 -149.1 -149.5 -149.8

-150.1 -150.4 -150.8

4400

-151.1 -151.4 -151.7 -152.0 -152.4 -152.7 -153.0

-153.3 -153.6 -154.0

4500

-154.3 -154.6 -154.9 -155.2 -155.6 -155.9 -156.2

-156.5 -156.8 -157.2

TERMINAL PROCEDURES - GENERAL

INFORMATION

1629

HECTOPASCAL/MILLIBAR EQUIVALENT FOR AIRPORT ELEVATION

Elev

-200

-190

-180

-170

-160

-150

-140

-130

-120

-110

7.3

7.0

6.6

6.2

5.9

5.5

5.1

4.8

4.4

4.0

Elev

-100

-90

-80

-70

-60

-50

-40

-30

-20

-10

3.7

3.3

2.9

2.6

2.2

1.8

1.5

1.1

0.7

0.4

Elev

+00

+10

+20

+30

+40

+50

+60

+70

+80

+90

4600

-157.5 -157.8 -158.1 -158.4 -158.8 -159.1 -159.4

-159.7 -160.0 -160.4

4700

-160.7 -161.0 -161.3 -161.6 -161.9 -162.3 -162.6

-162.9 -163.2 -163.5

4800

-163.8 -164.2 -164.5 -164.8 -165.1 -165.4 -165.8

-166.1 -166.4 -166.7

4900

-167.0 -167.3 -167.7 -168.0 -168.3 -168.6 -168.9

-169.2 -169.5 -169.9

5000

-170.2 -170.5 -170.8 -171.1 -171.4 -171.8 -172.1

-172.4 -172.7 -173.0

5100

-173.3 -173.6 -174.0 -174.3 -174.6 -174.9 -175.2

-175.5 -175.8 -176.2

5200

-176.5 -176.8 -177.1 -177.4 -177.7 -178.0 -178.3

-178.7 -179.0 -179.3

5300

-179.6 -179.9 -180.2 -180.5 -180.8 -181.2 -181.5

-181.8 -182.1 -182.4

5400

-182.7 -183.0 -183.3 -183.7 -184.0 -184.3 -184.6

-184.9 -185.2 -185.5

5500

-185.8 -186.1 -186.5 -186.8 -187.1 -187.4 -187.7

-188.0 -188.3 -188.6

5600

-188.9 -189.2 -189.6 -189.9 -190.2 -190.5 -190.8

-191.1 -191.4 -191.7

5700

-192,0 -192.3 -192.6 -193.0 -193.3 -193.6 -193.9

-194.2 -194.5 -194.8

5800

-195.1 -195.4 -195.7 -196.0 -196.3 -196.7 -197.0

-197.3 -197.6 -197.9

5900

-198.2 -198.5 -198.8 -199.1 -199.4 -199.7 -200.0

-200.3 -200.6 -200.9

6000

-201.3 -201.6 -201.9 -202.2 -202.5 -202.8 -203.1

-203.4 -203.7 -204.0

6100

-204.3 -204.6 -204.9 -205.2 -205.5 -205.8 -206.1

-206.4 -206.7 -207.1

6200

-207.4 -207.7 -208.0 -208.3 -208.6 -208.9 -209.2

-209.5 -209.8 -210.1

6300

-210.4 -210.7 -211.0 -211.3 -211.6 -211.9 -212.2

-212.5 -212.8 -213.1

6400

-213.4 -213.7 -214.0 -214.3 -214.6 -214.9 -215.2

-215.5 -215.8 -216.1

6500

-216.4 -216.7 -217.0 -217.3 -217.6 -217.9 -218.2

-218.5 -218.8 -219.1

6600

-219.5 -219.8 -220.1 -220.4 -220.7 -221.0 -221.3

-221.6 -221.9 -222.2

6700

-222.5 -222.7 -223.0 -223.3 -223.6 -223.9 -224.2

-224.5 -224.8 -225.1

6800

-225.4 -225.7 -226.0 -226.3 -226.6 -226.9 -227.2

-227.5 -227.8 -228.1

6900

-228.4 -228.7 -229.0 -229.3 -229.6 -229.9 -230.2

-230.5 -230.8 -231.1

7000

-231.4 -231.7 -232.0 -232.3 -232.6 -232.9 -233.2

-233.5 -233.8 -234.1

7100

-234.4 -234.7 -235.0 -235.2 -235.5 -235.8 -236.1

-236.4 -236.7 -237.0

TERMINAL PROCEDURES - GENERAL

INFORMATION

1630

HECTOPASCAL/MILLIBAR EQUIVALENT FOR AIRPORT ELEVATION

Elev

-200

-190

-180

-170

-160

-150

-140

-130

-120

-110

7.3

7.0

6.6

6.2

5.9

5.5

5.1

4.8

4.4

4.0

Elev

-100

-90

-80

-70

-60

-50

-40

-30

-20

-10

3.7

3.3

2.9

2.6

2.2

1.8

1.5

1.1

0.7

0.4

Elev

+00

+10

+20

+30

+40

+50

+60

+70

+80

+90

7200

-237.3 -237.6 -237.9 -238.2 -238.5 -238.8 -239.1

-239.4 -239.7 -240.0

7300

-240.3 -240.6 -240.8 -241.1 -241.4 -241.7 -242.0

-242.3 -242.6 -242.9

7400

-243.2 -243.5 -243.8 -244.1 -244.4 -244.7 -245.0

-245.2 -245.5 -245.8

7500

-246.1 -246.4 -246.7 -247.0 -247.3 -247.6 -247.9

-248.2 -248.5 -248.8

7600

-249.0 -249.3 -249.6 -249.9 -250.2 -250.5 -250.8

-251.1 -251.4 -251.7

7700

-252.0 -252.2 -252.5 -252.8 -253.1 -253.4 -253.7

-254.0 -254.3 -254.6

7800

-254.9 -255.1 -255.4 -255.7 -256.0 -256.3 -256.6

-256.9 -257.2 -257.5

7900

-257.7 -258.0 -258.3 -258.6 -258.9 -259.2 -259.5

-259.8 -260.1 -260.3

8000

-260.6 -260.9 -261.2 -261.5 -261.8 -262.1 -262.4

-262.6 -262.9 -263.2

8100

-263.5 -263.8 -264.1 -264.4 -264.6 -264.9 -265.2

-265.5 -265.8 -266.1

8200

-266.4 -266.7 -266.9 -267.2 -267.5 -267.8 -268.1

-268.4 -268.7 -268.9

8300

-269.2 -269.5 -269.8 -270.1 -270.4 -270.6 -270.9

-271.2 -271.5 -271.8

8400

-272.1 -272.4 -272.6 -272.9 -273.2 -273.5 -273.8

-274.1 -274.3 -274.6

8500

-274.9 -275.2 -275.5 -275.8 -276.0 -276.3 -276.6

-276.9 -277.2 -277.5

8600

-277.7 -278.0 -278.3 -278.6 -278.9 -279.1 -279.4

-279.7 -280.0 -280.3

8700

-280.6 -280.8 -281.1 -281.4 -281.7 -282.0 -282.2

-282.5 -282.8 -283.1

8800

-283.4 -283.6 -283.9 -284.2 -284.5 -284.8 -285.1

-285.3 -285.6 -285.9

8900

-286.2 -286.5 -286.7 -287.0 -287.3 -287.6 -287.8

-288.1 -288.4 -288.7

9000

-289.0 -289.2 -289.5 -289.8 -290.1 -290.4 -290.6

-290.9 -291.2 -291.5

9100

-291.8 -292.0 -292.3 -292.6 -292.9 -293.1 -293.4

-293.7 -294.0 -294.3

9200

-294.5 -294.8 -295.1 -295.4 -295.6 -295.9 -296.2

-296.5 -296.7 -297.0

9300

-297.3 -297.6 -297.8 -298.1 -298.4 -298.7 -299.0

-299.2 -299.5 -299.8

9400

-300.1 -300.3 -300.6 -300.9 -301.2 -301.4 -301.7

-302.0 -302.3 -302.5

9500

-302.8 -303.1 -303.4 -303.6 -303.9 -304.2 -304.5

-304.7 -305.0 -305.3

9600

-305.5 -305.8 -306.1 -306.4 -306.6 -306.9 -307.2

-307.5 -307.7 -308.0

9700

-308.3 -308.6 -308.8 -309.1 -309.4 -309.6 -309.9

-310.2 -310.5 -310.7

TERMINAL PROCEDURES - GENERAL

INFORMATION

1631

HECTOPASCAL/MILLIBAR EQUIVALENT FOR AIRPORT ELEVATION

Elev

-200

-190

-180

-170

-160

-150

-140

-130

-120

-110

7.3

7.0

6.6

6.2

5.9

5.5

5.1

4.8

4.4

4.0

Elev

-100

-90

-80

-70

-60

-50

-40

-30

-20

-10

3.7

3.3

2.9

2.6

2.2

1.8

1.5

1.1

0.7

0.4

Elev

+00

+10

+20

+30

+40

+50

+60

+70

+80

+90

9800

-311.0 -311.3 -311.6 -311.8 -312.1 -312.4 -312.6

-312.9 -313.2 -313.5

9900

-313.7 -314.0 -314.3 -314.5 -314.8 -315.1 -315.4

-315.6 -315.9 -316.2

10000

-316.4 -316.7 -317.0 -317.2 -317.5 -317.8 -318.1

-318.3 -318.6 -318.9

10100

-319.1 -319.4 -319.7 -319.9 -320.2 -320.5 -320.7

-321.0 -321.3 -321.6

10200

-321.8 -322.1 -322.4 -322.6 -322.9 -323.2 -323.4

-323.7 -324.0 -324.2

10300

-324.5 -324.8 -325.0 -325.3 -325.6 -325.8 -326.1

-326.4 -326.6 -326.9

10400

-327.2 -327.4 -327.7 -328.0 -328.2 -328.5 -328.8

-329.0 -329.3 -329.6

10500

-329.8 -330.1 -330.4 -330.6 -330.9 -331.2 -331.4

-331.7 -332.0 -332.2

10600

-332.5 -332.8 -333.0 -333.3 -333.6 -333.8 -334.1

-334.4 -334.6 -334.9

10700

-335.2 -335.4 -335.7 -335.9 -336.2 -336.5 -336.7

-337.0 -337.3 -337.5

10800

-337.8 -338.1 -338.3 -338.6 -338.8 -339.1 -339.4

-339.6 -339.9 -340.2

10900

-340.4 -340.7 -341.0 -341.2 -341.5 -341.7 -342.0

-342.3 -342.5 -342.8

11000

-343.1 -343.3 -343.6 -343.8 -344.1 -344.4 -344.6

-344.9 -345.1 -345.4

11100

-345.7 -345.9 -346.2 -346.5 -346.7 -347.0 -347.2

-347.5 -347.8 -348.0

11200

-348.3 -348.5 -348.8 -349.1 -349.3 -349.6 -349.8

-350.1 -350.4 -350.6

11300

-350.9 -351.1 -351.4 -351.7 -351.9 -352.2 -352.4

-352.7 -352.9 -353.2

11400

-353.5 -353.7 -354.0 -354.2 -354.5 -354.8 -355.0

-355.3 -355.5 -355.8

11500

-356.0 -356.3 -356.6 -356.8 -357.1 -357.3 -357.6

-357.9 -358.1 -358.4

11600

-358.6 -358.9 -359.1 -359.4 -359.7 -359.9 -360.2

-360.4 -360.7 -360.9

11700

-361.2 -361.4 -361.7 -362.0 -362.2 -362.5 -362.7

-363.0 -363.2 -363.5

11800

-363.7 -364.0 -364.3 -364.5 -364.8 -365.0 -365.3

-365.5 -365.8 -366.0

11900

-366.3 -366.6 -366.8 -367.1 -367.3 -367.6 -367.8

-368.1 -368.3 -368.6

12000

-368.8 -369.1 -369.3 -369.6 -369.9 -370.1 -370.4

-370.6 -370.9 -371.1

12100

-371.4 -371.6 -371.9 -372.1 -372.4 -372.6 -372.9

-373.1 -373.4 -373.6

12200

-373.9 -374.2 -374.4 -374.7 -374.9 -375.2 -375.4

-375.7 -375.9 -376.2

12300

-376.4 -376.7 -376.9 -377.2 -377.4 -377.7 -377.9

-378.2 -378.4 -378.7

TERMINAL PROCEDURES - GENERAL

INFORMATION

1632

HECTOPASCAL/MILLIBAR EQUIVALENT FOR AIRPORT ELEVATION

Elev

-200

-190

-180

-170

-160

-150

-140

-130

-120

-110

7.3

7.0

6.6

6.2

5.9

5.5

5.1

4.8

4.4

4.0

Elev

-100

-90

-80

-70

-60

-50

-40

-30

-20

-10

3.7

3.3

2.9

2.6

2.2

1.8

1.5

1.1

0.7

0.4

Elev

+00

+10

+20

+30

+40

+50

+60

+70

+80

+90

12400

-378.9 -379.2 -379.4 -379.7 -379.9 -380.2 -380.4

-380.7 -380.9 -381.2

12500

-381.4 -381.7 -381.9 -382.2 -382.4 -382.7 -382.9

-383.2 -383.4 -383.7

12600

-383.9 -384.2 -384.4 -384.7 -384.9 -385.2 -385.4

-385.7 -385.9 -386.2

12700

-386.4 -386.7 -386.9 -387.2 -387.4 -387.7 -387.9

-388.1 -388.4 -388.6

12800

-388.9 -389.1 -389.4 -389.6 -389.9 -390.1 -390.4

-390.6 -390.9 -391.1

12900

-391.4 -391.6 -391.9 -392.1 -392.3 -392.6 -392.8

-393.1 -393.3 -393.6

13000

-393.8 -394.1 -394.3 -394.6 -394.8 -395.0 -395.3

-395.5 -395.8 -396.0

13100

-396.3 -396.5 -396.8 -397.0 -397.3

397.5 -397.7

-398.0 -398.2 -398.5

13200

-398.7 -399.0 -399.2 -399.5 -399.7 -399.9 -400.2

-400.4 -400.7 -400.9

13300

-401.2 -401.4 -401.6 -401.9 -402.1 -402.4 -402.6

-402.9 -403.1 -403.3

13400

-403.6 -403.8 -404.1 -404.3 -404.6 -404.8 -405.0

-405.3 -405.5 -405.8

13500

-406.0 -406.3 -406.5 -406.7 -407.0 -407.2 -407.5

-407.7 -407.9 -408.2

TERMINAL PROCEDURES - GENERAL

INFORMATION

1633

HECTOPASCAL/MILLIBAR EQUIVALENT FOR AIRPORT ELEVATION