INSTRUMENT NUMBER:  CASA 390/04

 

 

CIVIL AVIATION ACT 1988

 

CIVIL AVIATION SAFETY REGULATIONS 1998

 

MANUAL OF STANDARDS (MOS) PART 139 — AERODROMES

 

AMENDMENT

 

 

I, WILLIAM BRUCE BYRON, Director of Aviation Safety, on behalf of CASA, publish the following amendment of the Manual of Standards (MOS) Part 139 — Aerodromes:

 (a) under and in accordance with paragraph 9 (1) (c) of the Civil Aviation Act 1988 (the Act); and

 (b) for the purposes of Part 139 of the Civil Aviation Safety Regulations 1998 (CASR 1998).

 

 

[Signed Bruce Byron]

 

 

Bruce Byron

Director of Aviation Safety and

   Chief Executive Officer

 

7 September 2004

 

1 Name of Instrument

 

1.1 This instrument is the Manual of Standards (MOS) Part 139 — Aerodromes (Amendment) (MOS Part 139 Amendment).

2 Commencement

 

2.1 This MOS Part 139 Amendment starts having effect on 1 September 2004.

3 Amendment of Manual of Standards (MOS) Part 139 — Aerodromes

 

3.1 Schedule 1 amends Manual of Standards (MOS) Part 139 — Aerodromes.

 

 

SCHEDULE 1

 

 

AMENDMENT OF MANUAL OF STANDARDS (MOS) PART 139 — AERODROMES

1 Subsection 1.1.1, the heading

 omit

Background

 insert

Commencement and Background

2 Paragraph 1.1.1.2

 before

Note

 insert

1.1.1.2A The Standards for aerodromes used in air transport operations, as set out in this MOS (except Chapter 13), come into effect when CASR Part 121A comes into effect. However, to avoid doubt, until CASR Part 121A comes into effect, the Standards set out in this MOS (except Chapter 13) continue to be the Standards in effect for aerodromes with respect to regular public transport operations by aeroplanes with a maximum take-off weight in excess of 5700kg. The operators of aerodromes for charter aeroplanes with a maximum take-off weight in excess of 5700kg are expected to plan for, and be ready to implement, the Standards in this MOS (except Chapter 13) when CASR Part 121A comes into effect.

1.1.1.2B The Standards for aerodromes used in air transport operations, as set out in Chapter 13 of this MOS, come into effect when CASR Part 121B comes into effect. However, to avoid doubt, until CASR Part 121B comes into effect, the Standards set out in section 82.3 of the Civil Aviation Orders continue to be the minimum Standards in effect for aerodromes with respect to regular public transport operations by aeroplanes with a maximum take-off weight not exceeding 5700kg. Aerodrome operators to whom CASR Part 121B will apply are expected to plan for, and be ready to implement, the Standards in Chapter 13 when CASR Part 121B comes into effect.

3 After paragraph 1.1.1.10

 insert

1.1.1.11 Where there is flexibility in compliance with a specification, words like “should” or “may” are used.  This does not mean that the specification can be ignored, but it means that there is no need to seek CASA approval if an aerodrome operator chooses to adopt alternate means to achieve similar outcomes.

1.1.1.12 Where it is necessary to provide factual or background information, explanation or references, or to provide a means of achieving compliance, the information is provided in the form of a “Note”.  A Note does not constitute part of the standard.

4 Paragraphs 1.1.2.1 and 1.1.2.2

 substitute

1.1.2.1 The document hierarchy consists of:

(a) the Civil Aviation Act 1988 (the Act);

(b) relevant Civil Aviation Safety Regulations 1998 (CASRs);

(c) the Manual of Standards (MOS);

(d) Advisory Circulars (ACs).

1.1.2.2 The Act establishes the Civil Aviation Safety Authority (CASA) with functions relating to civil aviation, in particular the safety of civil aviation and for related purposes.

5 Subsection 1.1.5

 substitute

1.1.5 MOS Documentation Change Management

1.1.5.1 Responsibility for the technical content in the MOS resides with the relevant technical area within the Aviation Safety Standards Division of CASA.

1.1.5.2 This MOS is issued and amended under the authority of the Director of Aviation Safety and Chief Executive Officer.

1.1.5.3 Suggested changes to this MOS must be directed to the Head, Standards Administration and Support Branch, Aviation Safety Standards Division.

1.1.5.4 Requests for any change to the content of the MOS may be initiated from:

(a) technical areas within CASA;

(b) aviation industry service providers or operators;

(c) individuals and authorisation holders.

1.1.5.5 The need to change standards in the MOS may be generated by a number of causes.  These may be to:

(a) ensure safety;

(b) ensure standardisation;

(c) respond to changed CASA standards;

(d) respond to ICAO prescription;

(e) accommodate new initiatives or technologies.

6 Paragraph 2.1.2.3

 substitute

2.1.2.3 At a certified aerodrome, an existing aerodrome facility that does not comply with this MOS must be identified and recorded in the Aerodrome Manual.  Information must include the date or period when that facility was first introduced or last upgraded and an indication from the aerodrome operator of a plan or timescale to bring the facility into compliance with the MOS.  As part of the CASA audit, evidence to demonstrate efforts to implement the plan or timescale may be required.

7 Sub-subparagraph 5.1.3.8 (c) (iii), Low tyre pressure category, the table

 substitute

 

Maximum allowable tyre pressure category

Code

Low: pressure limited to 1.00MPa

Low: pressure limited to 0.80MPa

Y1

Y2

8 Paragraph 5.1.3.9

 substitute

5.1.3.9 The Aircraft Classification Number (ACN) values for various aircraft types operating on flexible and rigid pavements are provided in Table 5.1-1.  The aircraft weight limits are defined by maximum take-off weight (MTOW) (kg) and operating weight empty (OWE) (kg).  The operating tyre pressure is defined by TP (kPa).  The main wheel under-carriage configurations are: single (S), dual (D), dual tandem (DT) and triple-tandem (TT).

Note: Specific ACN values for a particular aircraft should be obtained from the aircraft operator or the aircraft manufacturer.

 


Table 5.1-1:  ACN values for various aircraft types operating on flexible

and rigid pavements

 

 

ACN

Aircraft Type /Main wheel configuration

MTOW
OWE
TP

Flexible Pavement
Subgrade
CBR%

Rigid Pavement
Subgrade
k in MN/m3

 

 

A
15

B
10

C
6

D
3

A
k150

B
k80

C
k40

D
k20

A300-B4
DT
 

165900
88505
1240

47
21

52
22

63
26

82
34

42
19

50
21

60
25

69
29

A320-200
D

72000
40800
1360

36
19

37
19

41
20

46
23

40
21

42
22

44
23

46
24

A310-200
DT

132900
76890
1080

36
18

39
19

48
22

63
29

31
16

38
18

46
21

53
25

A330-300
DT

212000
121870
580

55
29

60
30

69
33

94
41

47
28

54
27

64
31

75
36

A340-300
DT

271000
129300
1380

59
24

64
25

74
28

100
34

50
25

58
24

69
26

80
30

Argosy
D

42276
22150
620

17
8

20
9

23
10

28
13

19
9

21
10

23
11

25
12

ATR 42
-200
D

15770
9609
744

7.1
3.9

8
4.4

9.3
4.8

10
5.9

8.6
4.7

9.1
5.1

9.6
5.4

10
5.7

BAC 1-11
-500
D

47400
24900
1103

27
12

29
13

31
14

33
16

30
14

32
15

33
15.5

34
16

BAe 146
-200
D

40030
22000
972

19.5
9.8

20.5
10

23
11

27
13

21
10.5

23
11

24
12

25
13

Jetstream
31

 

6950
4900
450

3.4
2.4

4.4
3

5.3
3.7

5.7
4

4.3
3.1

4.5
3.2

4.7
3.3

4.8
3.4

B707-320C
DT

152407

67495

1240

44

16

50

17

60

19

76

25

41

25

49

16

58

19

66

22


 

ACN

Aircraft Type /Main wheel configuration

MTOW
OWE
TP

Flexible Pavement
Subgrade
CBR%

Rigid Pavement
Subgrade
k in MN/m3

 

 

A
15

B
10

C
6

D
3

A
k150

B
k80

C
k40

D
k20

B717

D

54885

32110

1048

31

16

33

17

37

19

40

22

35

18

37

19

38

20

40

21

B727-200
D

95300
45735
1035

52
22

55
22.4

62
25

67
29

56
23

59
25

63
27

65
28

B737-200
D

53410
27290
1145

27
12.6

28
12.7

32
13.8

36
16

30
14

32
15

34
15.5

35
16

B737-300
D

61460
32900
1164

32
15.6

33
15.7

37
17

42
20

35
17

38
18

40
19

41
20

B737-400
D

68260
33640
1327

37
16

39
17

44
18

48
21

43
18

45
20

47
21

49
22

B737-700

D

60330

38147

1300

31

19

32

19

36

21

41

24

35

21

37

22

39

23

41

24

B737-800

D

70535

41145

1413

38

20

40

21

44

23

49

26

44

23

46

24

48

26

50

27

B747-SP
DT

302727
140000
1139

38
15

42
15.5

51
17

69
22

32
13.5

38
14

46
16

53
19

B747-200B
DT

364200
173320
1400

51
20

57
22

69
24

91
31

47
19

56
21

66
24

76
28

B747-300
DT

379100
174820
1296

53
20

60
22

74
24

95
31

48
18

57
20

68
24

79
28

B747-400
DT

386800
176860
1400

56
21

62
22

77
25

99
32

51
19

61
22

73
25

83
29

B747-SP
DT

302727
140000
1139

38
15

42
15.5

51
17

69
22

32
13.5

38
14

46
16

53
19

B747-200B
DT

 

364200
173320
1400

51
20

57
22

69
24

91
31

47
19

56
21

66
24

76
28

B747-300
DT

379100
174820
1296

53
20

60
22

74
24

95
31

48
18

57
20

68
24

79
28


 

 

ACN

Aircraft Type /Main wheel configuration

MTOW
OWE
TP

Flexible Pavement
Subgrade
CBR%

Rigid Pavement
Subgrade
k in MN/m3

 

 

A
15

B
10

C
6

D
3

A
k150

B
k80

C
k40

D
k20

B747-400
DT

386800
176860
1400

56
21

62
22

77
25

99
32

51
19

61
22

73
25

83
29

B757-200
DT

100200
56900
1116

27
13.5

30
14

36
16

49
22

25
12

30
14

36
16

41
19

B767-200
DT

141520
80890
1172

37
18.7

40
19

48
22

66
28

32
16

38
18

45
21

53
25

B767-200ER
DT

157400
80890
1260

42
19

46
20

55
22

75
28

37
17

44
19

53
22

61
25

B767-300ER
DT

172820
88000
1260

48
21

53
22

65
25

86
32

41
18

50
20

60
24

70
28

B777-200
TT

286897

142430

1255

62

24

71

27

90

31

121

43

47

22

61

22

80

27

99

34

Canadair
CL-600
D

19590
10000
1316

10.6
4.8

11.4
4.9

12.5
5.4

13
6.3

12.8
5.8

13.3
6.1

13.7
6.3

14.1
6.6

Cessna
550 S2
S

6940
4146
830

5.3
3.2

5.8
3.4

5.8
3.5

6.1
3.6

5.5
3.3

5.6
3.3

5.6
3.4

5.7
3.4

Cessna
Citation 3
D

9525
5670
1013

5.5
2.8

5.9
3.0

6.3
3.4

6.6
3.8

6.5
3.5

6.7
3.6

6.9
3.8

7
3.9

Dash 7
D

19867
11793
750

10
5

11
6

12
6

14
8

11
6

12
6

13
7

13
7

Dash 8-100
D

15785
9790
805

7.4
4

8
4.5

9
5

10.6
6

8.5
5

9.1
5

9.7
5.5

10.2
6

DC-8-63F
DT

162389
64107
1350

52
16

59
17

71
19

87
24

49
15

60
17

70
20

78
23

DC-9-32
D

49442
25597
1048

26
12

28
12.4

31
14

34
16

30
13

31
14

33
15

34
16


 

 

ACN

Aircraft Type /Main wheel configuration

MTOW
OWE
TP

Flexible Pavement
Subgrade
CBR%

Rigid Pavement
Subgrade
k in MN/m3

 

 

A
15

B
10

C
6

D
3

A
k150

B
k80

C
k40

D
k20

DC-9-82
D

68000
35000
1173

39
18

41
18

46
20

49
24

43
20

46
21

48
22

49
23

DC-10-10
DT

207746
108940
1345

55
26

60
27

72
30

98
38

48
23

56
25

67
29

78
33

DC-10-30
DT

260818
120742
1170

55
22

61
23

73
25

101
32

46
20

55
21

66
24

78
27

Brasilia
EMB 120
D

11600
7150
830

5.4
3.1

5.9
3.5

6.7
3.8

7.8
4.6

7.2
4.1

7.5
4.5

7.8
4.7

8.1
4.9

F/A-18
S

23542
10523
1723

22.5
10

21.6
9.7

21.5
9.6

21
9.5

23.4
10.4

23.2
10.3

23
10.2

22.8
10.2

Falcon-20
D

14000
8500
1020

8.1
4.3

8.6
4.5

9.3
5.2

9.8
5.7

9.4
5.2

9.7
5.4

10
5.6

10.2
5.8

Falcon-50
D

17600
9600
1400

9.3
4.6

9.9
4.8

11
5.1

12
6

11.4
5.6

11.8
5.8

12.2
6.1

12.5
6.3

Falcon-900
D

20635
10614
1330

12
5

13
6

14
6

15
7

14
7

15
7

15
7

16
7

F27-500
D

20412
11789
552

8.2
4.2

10
5.1

12
6

14
7.3

10.3
5.3

11
5.8

12
6.3

13
6.8

F28-1000
D

29484
15660
580

12
5.5

14
6.5

17
7.4

19
9.1

14
6.5

15
7.2

17
8

18
8.5

F28-4000
D

33110
16068
696

15
6.1

17
7

19
7.7

22
9.2

17
7

19
7.7

20
8.3

21
8.9

Fokker-50
D

20820
12383
552

8
4.3

10
5.2

11
6

14
7.4

10
5.3

11
5.8

12
6.4

13
6.9

Fokker-100D

41730
23200
920

23
11

24
12

27
13

30
15

24
12

25
12.5

26
13.3

27
14


 

 

ACN

Aircraft Type /Main wheel configuration

MTOW
OWE
TP

Flexible Pavement
Subgrade
CBR%

Rigid Pavement
Subgrade
k in MN/m3

 

 

A
15

B
10

C
6

D
3

A
k150

B
k80

C
k40

D
k20

GG II
D

28100
16000
930

15.4
7.7

16.6
8

18.3
9.3

19
10.5

17.6
9.0

18.4
9.5

19
10

19.7
10.4

GG III
D

31162
17372
1200

18
8.6

19
9

21
10.3

22
11.5

20
10

21
10.6

22
11

23
11.5

HS-748
D

20183
11786
550

7.7
4

9.5
4.8

11.1
5.6

13
7

9.6
5

10.5
5.5

11.3
6

12
6.4

Lear 35A
D

7824
4132
1080

3.9
1.9

4
1.9

4.6
2.1

5.1
2.4

4.7
2.2

4.9
2.3

5.1
2.5

5.3
2.6

Lockheed
L1011
DT

225889
108925
1269

60
25

66
26

79
29

105
36

50
23

59
24

72
27

84
31

Lockheed
C141
DT

145150
60100
1192

42
12.6

48
13

59
15

73
20

43
14

52
16

61
18

69
21

Lockheed
C130-H
D

70300
35000
550

23
10

28
13

32
15

37
16

26
13

29
14

32
15

35
16

Lockheed
C130-H
D

70300
35000
725

27
12

30
14

33
15

38
17

30
14

33
15

35
16

38
17

Orion
P3A
D

61235
27000
1310

35
13

38
14

42
15

44
17

41
15

43
16

44
17

46
18

SF-340
D

11794
7194
655

4.9
2.7

5.7
3.2

6.5
3.5

7.7
4.3

6.1
3.4

6.5
3.6

6.9
3.9

7.3
4.1

Shorts-330
S

10250
6690
540

5.8
3.8

7
4.6

8.1
5.3

8.5
5.6

6.8
4.5

7.1
4.7

7.3
4.8

7.5
4.9

Shorts-360
S

11818
7480
760

8.5
5.4

9.5
6

9.8
6.2

10
6.5

9
5.7

9.2
5.8

9.3
5.9

9.4
6

Westwind I
S

10660
6066
1050

9
5.1

9.3
5.3

9.2
5.3

9.4
5.4

9.1
5.2

9.1
5.2

9.2
5.2

9.2
5.3


9 Paragraph 5.1.3.23

 substitute

5.1.3.23 Aerodrome obstacles.  Local data may include obstacles in the circuit area.

5.1.3.24 Additional information.  Significant local data may include the following:

(a) animal or bird hazard;

(b) aircraft parking restriction;

(c) aircraft to avoid overflying certain areas such as mine blasting areas;

(d) other aviation activities such as ultralight or glider operations in the vicinity.

10 Paragraph 5.2.2.2, the diagrams

 substitute

 

11 Paragraph 5.2.5.1

 substitute

5.2.5.1 The following diagrams illustrate the method of calculating the take-off distance available or take-off run available where departures are allowed from taxiway intersections.

 

 

 

12 Paragraph 6.2.5.1

 substitute

6.2.5.1 Where parallel runways are to be provided, the aerodrome operator should consult with CASA and Airservices Australia on airspace and air traffic control procedures associated with the operation of the multiple runways. Where parallel, non-instrument runways are provided for simultaneous use, the minimum separation distance between the runway centrelines must not be less than:

(a) where General Aviation Aerodrome Procedures (GAAP) are in place — 213m.  If this distance is not provided, dependent parallel procedures may need to be introduced;

(b) where the higher code number of the two runways is 3 or 4 — 210m;

(c) where the higher code number of the two runways is 2 — 150m;

(d) where the code number of the two runways is 1 — 120m.

13 Paragraph 6.2.9.1

 substitute

6.2.9.1 The surface of a bitumen seal, asphalt or concrete runway must not have irregularities that would result in the loss of frictional characteristics or otherwise adversely affect the take-off or landing of an aircraft.

Note: The finish of the surface of a runway should be such that, when tested with a 3m straight-edge placed anywhere on the surface, there is no deviation greater than 3mm between the bottom of the straight-edge and the surface of the runway pavement anywhere along the straightedge.

6.2.9.1A The surface of a bitumen seal, asphalt or concrete runway must have an average surface texture depth of not less than 1mm over the full runway width and runway length.

Note: A runway surface meeting the ICAO minimum design objective for new surfaces specified in Annex 14, Volume 1, derived using a continuous friction-measuring device, is acceptable.

14 Paragraph 6.2.10.2

 substitute

6.2.10.2 CASA does not specify a standard for runway bearing strength, however, the bearing strength must be such that it will not cause any safety problems to aircraft.  The published PCN value should be suitable for the aircraft that regularly use the runway.

15 Paragraph 6.2.29.1, the Note

 substitute

Note: To reduce the risk of damage to an aeroplane undershooting the runway and to prevent jet blast erosion from jet aircraft turning and taking off at the end of the runway, it is recommended that areas abutting the runway should be provided with a compacted gravel pavement with a depth at the runway end equal to half the depth of the runway pavement, tapering to natural surface, the length of the taper being adjusted according to the bearing capacity of the natural surface.  For areas beyond the gravel surface and outside the runway strip, graded but non-compacted natural surface with a grass cover is preferred.  Hard pans should be broken up.

16 Paragraph 6.2.39.2

 omit

accelerated (wherever occurring)

 insert

accelerate

17 Paragraph 6.3.14.3

 substitute

6.3.14.3 No portion of the taxiway strip beyond the graded portion, nor objects thereon, must project upwards through a plane surface, originating from the outer edge of the graded taxiway strip, sloping upwards and outwards at a slope of 5% measured with reference to the horizontal. 

Note: The presence of drains and ditches in this part of the taxiway strip is acceptable.

18 Paragraph 6.4.4.2, contents of Table 6.4-1

 substitute

 

Code number

Type of runway

Non-instrument

Non-precision approach

Precision category I

Precision category
II or III

Take–off

1

30m

40m

60m

30m

2

40m

40m

60m

40m

3

75ma

75ma

90mb

105mc

75ma

4

75m

75m

90md

105mc d

75m

a if the runway’s code is 3A, 3B or 3C, the minimum distance is 45m.

b if the runway’s code is 3A, 3B or 3C, the minimum distance is 75m.

c may be reduced to 90m up to 300 m from the runway end.

d if the runway code letter is F, this distance should be 107.5m.

19 Paragraph 7.1.8.1

 omit

Table 10.15-1

 insert

Table 7.1-1

20 Paragraph 7.1.8.5

 omit

Table 10.15-1

 insert

Table 7.1-1

21 After subparagraph 7.3.2.5 (f)

 insert

(g) The above surfaces are to be varied when lateral offset, offset or curved approaches are utilised, specifically, two sides originating at the ends of the inner edge and diverging uniformly at a specified rate from the extended centreline of the lateral offset, offset or curved ground track.

22 Paragraph 8.1.2.1, at the end

 insert

Note: A closed aerodrome or aerodrome facility means one which has been withdrawn or decommissioned, not one which is temporarily unserviceable.

23 Paragraph 8.2.1.4, at the bottom of Figure 8.2-1

 insert

For cones used as runway edge markers h = 0.3m, w = 0.4m

24 Paragraph 8.3.9.5

 after

comprising white lines 1m wide.

 insert

The number of 10m long arrowhead markings used should be commensurate with the width of the runway.

25 Paragraph 8.3.9.9, the diagram in Figure 8.3-15

 substitute

 

26 Paragraph 8.3.9.9, the diagram in Figure 8.3-16

 substitute

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

27 Paragraph 8.4.3.4, diagram in Figure 8.4-2

 substitute

 

 

28 Paragraph 8.4.3.5, diagram in Figure 8.4-3

 substitute

 

 

 

 

 

 

 

 

29 After paragraph 8.5.2.4

 insert

8.5.2.5  Where an aircraft designator marking is required to cover a multiple number of aircraft types, and there is insufficient space for the marking, an abbreviated version of the designator may be used e.g. an A330-200 may be abbreviated to A332, a BAe 146200 to B462 and a B737-800 to B738.  A list of typical aircraft designators is published by Airservices Australia on their web page: http://www.airservicesaustralia.com/pilotcentre/SpecialpilotOps/acft.pdf.

30 Paragraph 8.6.6.4

 substitute

8.6.6.4 The average luminance of the sign must be calculated in accordance with ICAO Annex 14, Volume 1, Appendix 4, Figure 4.1.

31 Paragraph 8.7.1.2

 substitute

8.7.1.2 CASR Part 139 also requires that non-precision approach runways be provided with a wind direction indicator at the threshold of the runway.  However, subject to paragraph 8.7.1.3, for runways 1200m or less in length one centrally located wind direction indicator visible from both approaches and the aircraft parking area is acceptable.

 

32 Paragraph 8.10.2.4, diagram in Figure 8.10-2

 substitute

 

 

 

 

 

 

 

 

33 Paragraph 8.10.4.1

 substitute

8.10.4.1 A vehicle used regularly on the manoeuvring area by day should be painted a single conspicuous colour, preferably yellow or orange.  Where so painted, it does not require additional marking.

34 Paragraph 8.10.4.2

 substitute

8.10.4.2 Vehicles not painted yellow or orange must be marked, by using either:

(a) flags; or

(b) vehicle warning lights, in accordance with paragraph 9.19.1.

35 Paragraph 9.1.15.6

 omit all words from and including

  “Information” to and including “NOTAM”

 insert

Information to be supplied by aerodrome operator for inclusion in the permanent NOTAM

36 Subparagraph 9.9.1.4 (c)

 substitute

Double-sided PAPI; and

37 Paragraph 9.9.1.5

 omit

double sided (wherever occurring)

 insert

double-sided

38 Paragraph 9.9.2.1

 omit all words up to and including

provided.

 insert

An obstacle assessment surface (OAS) must be surveyed and assessed for obstacles for each end of the runway where a T-VASIS, AT-VASIS, doublesided PAPI or PAPI is to be provided.

39 Paragraph 9.9.4.4

 substitute

9.9.4.4 A double-sided PAPI system must consist of eight light units symmetrically disposed about the runway centre line in the form of two wing bars of four light units each.  The indications seen by the pilot must be symmetrical, so that when on or close to the approach slope, the two light units nearest the runway, in both wing bars, show red.

40 Paragraph 9.9.4.5

 after

Siting a PAPI

 insert

or a Double-sided PAPI

41 After subparagraph 9.10.17.1 (b)

 insert

(c) with respect to taxiways intended for exiting the runway, be located such that an aircraft exiting the runway will not be required to cross the row of red lights comprising the runway end lights.

Note: The universally accepted convention in aerodrome lighting is that a pilot is never required to cross a row of red lights.

42 Paragraph 9.11.1.4, title to Figure 9.11-12

 substitute

Figure 9.11-12: Method of Establishing Grid Points to be used for the Calculation of Average Intensity of Runway Lights specified by Figure 9.11-3 to Figure 9.11-10

43 After paragraph 9.13.13.3

 insert

9.13.13.4 Where a taxiway intersects with a runway, the last taxiway edge lights should preferably line-up with the line of runway edge lights, and must not encroach beyond the line of runway edge lights into the area outlined by the runway edge lights.

44 Paragraph 9.13.18.1, paragraph (a) of the Note

 substitute

(a) the centreline of lights in each pair should be separated by a horizontal distance that is not less than 2.5 times, and not more than 4 times, the radius of the individual lantern lens;

45 Paragraph 9.19.1.1

 substitute

9.19.1.1 Vehicle warning lights, as required by subsection 10.9.2, are provided to indicate to pilots and others the presence of vehicles or mobile plant on the movement area.

46 Paragraph 9.20.1.1

 omit

are to be (wherever occurring)

 insert

must be

47 Paragraph 9.20.2.1

 substitute

9.20.2.1 Any aerodrome light outage detected must be fixed as soon as is practicable.  The specifications listed below are intended to define the maintenance performance level objectives.  They are not intended to define whether the lighting system is operationally out of service.  Nor are they meant to condone outage, but are intended to indicate when lighting outage must be notified to the NOTAM office.  The specifications must be used as triggers for NOTAM action, to advise pilots of actual outage, unless the outage can be rectified before the next period of use.

48 Paragraph 9.20.2.5

 substitute

9.20.2.5 A lighting system is deemed to be on outage when:

(a) in the case of a lighting system comprising less than 4 lights (e.g. intermediate holding position lights or runway threshold identification lights), any of the lights are on outage;

(b) in the case of a lighting system comprising 4 or 5 lights (e.g. wind direction indicator lights or runway guard lights), more than 1 light is on outage;

(c) in the case of a lighting system comprising 6 to 13 lights (e.g. threshold lights or LAHSO lights), more than 2 lights are on outage, or 2 adjacent lights are on outage;

(d) in the case of a lighting system comprising more than 13 lights, more than 15% of the lights are on outage, or two adjacent lights are on outage.

Note: A lighting system here means lights used to illuminate a particular facility e.g. all the lights used to mark a threshold or runway end, runway edge lights on a runway, taxiway lights on a length of taxiway between intersections a T–VASIS or a PAPI system.

49 Subparagraph 9.20.2.6 (d)

 substitute

(d) Whenever a red filter has deteriorated such that it does not produce the correct colour light beam, is missing, or is damaged, all the lamps within the affected light unit must be extinguished until the red filter is rectified.  The affected light unit is included as an outage light unit when applying (b) or (c) above.

50 Paragraph 9.20.2.7

 substitute

9.20.2.7 For a PAPI, the outage standards take into account both the number of lamps on outage within a light unit and also the number of light units within the PAPI system.  The standards are:

(a) a PAPI light unit is deemed on outage when more than one lamp in a 3 or more lamp light unit is on outage, or any lamp in a less-than-3-lamp light unit is on outage;

(b) whenever a red filter has deteriorated such that it does not produce the correct colour light beam, is missing, or is damaged, all the lamps associated with that filter must be extinguished until the red filter is rectified.  The affected lamp/s are included as outage lamps when determining (a) above.

(c) a double-sided PAPI system (i.e. 8 light units) is:

(i) deemed to be on outage but useable when all light units in one wing bar are fully functioning, and any light units in the other wing bar are on outage.  The system may remain in use but a NOTAM must be issued detailing the number of light units on outage, and on which side of the runway they are; and

(ii) deemed on outage when one or more light units in each wing bar is on outage.  The double-sided PAPI system must be extinguished until the system is rectified;

(d) a single-sided PAPI system (i.e. 4 light units) is deemed to be on outage when any light unit  is on outage. The PAPI system must be extinguished until the system is rectified.

51 After paragraph 10.8.1.4

 insert

10.8.1.4A Where a rescue and fire fighting service (RFFS) is established at an aerodrome, the aerodrome operator and the rescue and fire fighting service provider must work together to ensure that they achieve the required outcome identified in MOS Part 139H – Standards Applicable to the Provision of Aerodrome Rescue and Fire Fighting Services.

52 Paragraph 10.8.7.1

 substitute

10.8.7.1 The person who initially assumes co-ordination of the situation should hand over the role when police arrive.

53 Paragraph 10.9.2.5

 substitute

10.9.2.5 Vehicles operating on the manoeuvring area by day must be marked in accordance with paragraph 8.10.4.

54 Paragraph 10.9.2.6

 substitute

10.9.2.6 Vehicles operating on the movement area must:

(a) be lit with vehicle warning lights in accordance with paragraph 9.19.1, unless accompanied by a vehicle that is so equipped; and

(b) display dipped headlights at night or in conditions of poor visibility.

55 After paragraph 10.9.2.6

 insert

10.9.2.7 Aircraft servicing equipment used only on aprons need not comply with paragraph 10.9.2.6.  In this case, equipment is deemed to be mobile objects that do not have their own motive power.

56 Paragraph 10.10.4.2

 substitute

10.10.4.2 Paragraph 10.10.4.1 does not apply at a controlled aerodrome or in other cases if the area can be restored to the required safety standards so as to allow aircraft operations to take place without delay.

57 Paragraph 10.10.7.4

 substitute

10.10.7.4 A works safety officer must be present at all times if aerodrome works are being carried out and the aerodrome is open to aircraft operations.

58 After paragraph 10.10.7.4

 insert

10.10.7.4A For time-limited works, a dedicated works safety officer is not required if one of the persons carrying out the time-limited work has been trained to perform the function of the works safety officer.

59 After paragraph 10.10.11.4

 insert

10.10.11.5 Before a runway being overlaid is returned to a temporary operational status, a runway centreline marking conforming to the specifications in Chapter 8, Section 8.3, Subsection 8.3.3 must be provided.

60 Paragraph 10.11.9.1

 substitute

10.11.9.1 When personnel and equipment are required to vacate the movement area for certain operations, specific mention of this fact must be made, e.g. “All personnel and equipment will clear runway strip 11/29 for air transport operations”.

61 Subparagraph 10.13.3.2 (b), at the end

 insert

Note: Advice is given in the USA National Fire Protection Association (NFPA) standards on the requirements for fire extinguishers at aircraft parking positions.  The NFPA web page is: http://www.nfpa.org/catalog/home/index.asp.

62 Paragraph 11.1.21

 substitute

11.1.21 Automatic Weather Information Stations

11.1.21.1 The location and configuration of the Bureau of Meteorology (BoM) provided weather information station sites and their dialup phone numbers, and, as relevant, the VHF broadcast frequencies, are set out in the MET section of ERSA.

11.1.21.2 Current weather information from the site is also available by accessing the BoM internet site at: www.bom.gov.au.

63 Subparagraph 12.1.3.2 (d)

 substitute

(d) any obstacles which may infringe the approach, take-off, transitional, inner horizontal or other surfaces nominated by the procedure designer;

64 Paragraph 12.1.6.1, Note

 substitute

Note: A copy of Notification of Changes to Serviceability of a Registered Aerodrome to the NOTAM Office is shown in Section 12.2.

65 Paragraph 12.1.7.3

 substitute

12.1.7.3 Where aerodrome works are carried out without closing the aerodrome, the aerodrome works safety procedures specified in Chapter 10: Section 10.10 for certified aerodromes are equally applicable to registered aerodromes.

66 Paragraph 12.1.8.3

 omit

taker-of

 insert

take-off

67 After subsection 12.1.8

 insert

12.1.9 Reporting of Obstacles

12.1.9.1 If the aerodrome is served by an instrument approach procedure, any obstacles, or proposed construction, that may infringe the obstacle limitation surface of the aerodrome, or other areas nominated by the designer of the instrument approach procedure, are to be reported to the designer.

68 Section 12.2, Form title

 substitute

Notification of Changes to Serviceability of a Registered Aerodrome

69 Subsection 13.1.1, the heading

 omit

Introduction

 insert

Commencement and Introduction

70 Paragraph 13.1.1.1

 substitute

13.1.1.1          The Standards set out in this Chapter come into effect in accordance with paragraph 1.1.1.2B.

13.1.1.1A This Chapter sets out the minimum Standards for aerodromes used in CASR Part 121B operations, that is air transport operations in aeroplanes with a maximum take-off weight not exceeding 5,700kg. Although these smaller aircraft may use aerodromes which meet the Standards applicable to aerodromes with respect to regular public transport operations by aeroplanes with a maximum take-off weight in excess of 5700kg, the minimum aerodrome standards for operations by such smaller aircraft are those set out in this Chapter.

71 Paragraph 13.1.1.2

 omit

CASR 121B

 insert

CASR Part 121B

72 Paragraph 13.1.2.1, Table 13.1-1, the headings in columns 1 to 4

 substitute

 

Runway and obstacle surfaces

Aeroplanes not exceeding 5,700kg by night

Aeroplanes not exceeding 5,700kg by day

Aeroplanes not exceeding 2,000kg by day

73 Paragraph 13.1.2.1, Table 13.1-1, Runway strip width — graded

 substitute

 

Runway strip width:

 – preferred graded

 

 – minimum acceptable graded

 

 – graded plus ungraded

 

80m

 

45m

 

80m

 

60m

 

45m

 

60m

 

30 m

 

 

60m

Runway strip transverse slope

3.0%

3.0%

3.0%

74 Paragraph 13.1.2.1, after Table 13.1-1

 insert

 Note:  At aerodromes with 10m wide runways, the aircraft operator or pilot in command should take into account the effects of crosswind.

75 After paragraph 13.1.2.3

 insert

13.1.2.3A Runway strip.  The runway strip may consist of a graded portion and an ungraded portion in cases where it is impractical to grade the entire runway strip. The impracticability of complying with specified runway graded width requirements will depend on the circumstances of each individual case.  Aerodrome operators should direct any questions about this issue to their nearest CASA area office.

76 Paragraph 13.1.3.3

 substitute

13.1.3.3 On unsealed runways, where the runway strip is not maintained to the normal runway grading standards, the runway must be marked using cone markers.   Where both the runway and the runway strip are prepared suitable for aircraft operations, either the runway or the runway strip may be marked.  Where the runway is not marked using cone markers, the threshold locations should be marked using white cones appropriately positioned in the shape of a             .

Note: Where cone markers are used they may be held down using tent pegs or similar, provided the pegs do not pose a hazard to aircraft or compromise the frangibility of the marker.

77 After paragraph 13.1.3.5

 insert

13.1.3.6 Where the edges of unsealed taxiways or aprons might not be visually clear to pilots, markers may be provided in accordance with Section 8.2.

78 Paragraph 13.1.4.1

 substitute

13.1.4.1 Where a runway is intended for night operations, the runway must be provided with runway edge lighting, spaced laterally at 30 – 31m apart, and longitudinally at approximately 90m apart.  The edge lights on each side must present two parallel straight rows equidistant from the runway centreline.  The lights indicating both ends of the runway must be at right angles to the runway centreline.  See Figure 13.1-4 for a typical layout of runway lights.

79 Paragraph 13.1.4.2

 substitute

13.1.4.2 Where there is no permanent electricity supply, the following may be used:

(a) lights producing white light and powered by portable generators, batteries, or similar power sources; or

(b) flares.