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19 Aerodromes - Physical Characteristics

19.45 Radio Altimeter Operating Area. The radio altimeter operating area should be established in the pre-threshold area of a precision approach runway. For CAT II/III operations the use of rad alt is mandatory to determine DH. For CAT II the minimum DH is 100 ft (system minima) and for a 300 ft/NM glide path this point would be at 600 m (1/3 NM) from the aiming point. Usually the aiming point is 300 m down the runway beyond the threshold; therefore the DH point would be 300 m before the threshold. For CAT III the DH is less than 50 ft, so a rad alt operating area for CAT II would be suitable for CAT III also. The area should extend before the threshold for a distance of at least 300 m. The area should extend laterally, on each side of the extended centre line of the runway, to a distance of 60 m, except that when special circumstances so warrant, the distance may be reduced to no less than 30 m if an aeronautical study indicates that such reduction would not affect the safety of operations of aircraft. The surface of the rad alt operating area should be level with no undulations of more than 7%.

Taxiways

19.46 Introduction. A major limitation to the use of an aerodrome is the capability of the taxiways to accommodate different sizes of aeroplanes. Clearly, a narrow taxiway cannot cope with a large aeroplane. However, width is not the only consideration. The strength of a taxiway needs to be equal to that of the runway and the surface of taxiways is more vulnerable to damage than a runway (constant loading and unloading, turning and stopping). Taxiways may include turns especially close to runways. Taxiways may cross, join, intersect and require signs and markings to enable pilots to reach their destination on the aerodrome. Taxiways, especially parallel to runways, must not be confused with runways. At some aerodromes, Gatwick for example, the parallel taxiway is also the secondary runway! Considerations have to be given to the points on taxiways where aeroplanes are held prior to entering the runway for take-off, and also portions of taxiways close to the runway where the presence of a large aeroplane (a large lump of electromagnetically friendly metal) may interfere with ILS or MLS transmissions, or more fundamentally, is an obstacle to operations. In basic terms according to Annex 14, taxiways should be provided to permit the safe and expeditious surface movement of aircraft.

 

19.47 General Layout. Sufficient entrance and exit taxiways for a runway are to be provided

19

to expedite movement of aeroplanes to and from the runway including the provision of rapid

 

-Aerodromes

exit taxiways (fast turn-off lanes) where traffic volumes are high. Where the end of a runway

is not served by a taxiway, it may be necessary to provide additional pavement at the end of

 

 

the runway for turning aeroplanes. Such areas may be usefully situated along the runway to

Physical

reduce taxi times.

19.48 Taxiing of Aeroplanes. Taxiways are required to have a painted centre line which may

Characteristics

be lit if the aerodrome is to be used at night. When taxiing an aeroplane it is vitally important

Concorde where the nose wheel was so far aft of the nose of the aeroplane that pilots used

 

that the nose wheel of the aeroplane is kept on the centre line especially during turns. Pilots

 

usually gain this skill by experience but special procedures may be used in extreme cases e.g.

 

marks on the windscreens to ‘fix’ the taxiway edge thus keeping the nose wheel in position on

 

the centre line.

380

Aerodromes - Physical Characteristics 19

19.49Rapid Exit Taxiways. Rapid exit taxiways, commonly called ‘fast turn-off lanes’, are provided where traffic density is high. They are used to allow aeroplanes to turn off of the duty runway at a speed higher than would be permitted at a right angle turn on to a normal taxiway. They are located along runways and are designed and constructed to cater for turnoff speeds of 93 km/h (50 kt) for code 3 or 4 runways and 65 km/h (35 kt) on code 1 and 2 runways, in wet conditions. Operators will specify the maximum speed for dry runway/taxiway operations. The taxiway is to include a straight section after the turn-off curve to allow an exiting aircraft to come to a full stop clear of the intersecting taxiway. The intersecting angle with the runway should not be greater than 45°, not less than 25°, and preferably 30°.

19.50Minimum Requirements. As previously mentioned, width is the most important factor in taxiway design and construction. The table below specifies the minimum requirements for clearance of the outermost main wheels when the nose wheel is on the centre line of the taxiway. The shoulders of taxiways which are used by turbine aeroplanes are to be prepared to prevent erosion by jet blast, and the ingestion of surface material into the jet engines. Taxiway strips, similar to runway strips, are provided primarily to delineate the area to be cleared of objects which may be obstacles. In the table, wheel base refers to the distance from the front of the nose wheel to the trailing edge of the main gear. Wheel to edge clearance refers to the distance from the outer edge of the main gear tyres to the defined edge of the taxiway.

 

Wheel to Taxiway Edge Clearance

 

 

Code Letter

Clearance

 

 

A

1.5 m

 

 

B

2.25 m

 

 

C

3 m if the taxiway is intended to be used by aeroplanes

with wheel base less than 18 m; otherwise 4.5 m

 

 

 

D

4.5 m

 

 

E

4.5 m

 

 

F

4.5 m

 

 

 

Figure 19.7 Wheel to edge clearance

Aerodromes - Physical Characteristics 19

381

19 Aerodromes - Physical Characteristics

19.51 Width of Taxiways. The straight portion of a taxiway should have a width of not less than that specified in the table below.

Taxiway Width

Code Letter

 

 

 

A

7.5 m

 

 

B

10.5 m

 

 

C

15 m if the taxiway is intended to be used by aeroplanes with

a wheel base less than 18 m; otherwise 18 m

 

 

 

D

18 m if the taxiway is intended to be used by aeroplanes with

an outer main gear span of less than 9 m; otherwise 23 m

 

 

 

E

23 m

 

 

F

25 m

 

 

Figure 19.8 Width of taxiways

Characteristics Physical - Aerodromes 19

Code C = 15 m if a/c has a wheel base less than

18 m otherwise width =

18 m

Code D = 18 m if a/c has outer main gear span less than 9 m otherwise

D/E/F = 23 m

Taxiways

Wheel to taxiway edge clearance = Code D/E/F 4.5 m

Rapid exit taxiways/fast turn-off lanes: may be used at max speed determined by operator (not more than 50 kt in wet conditions – code 3 or 4)

Figure 19.9: Taxiways

382

Aerodromes - Physical Characteristics 19

19.52 Taxiway Curves. Changes in direction of taxiways should be as few and small as possible. The radii of the curves should be compatible with the manoeuvring capability and normal taxiing speeds of the aeroplanes for which the taxiway is intended. An example of widening taxiways to achieve the wheel clearance specified is illustrated below.

Figure 19.10: Taxiway curves

19.53 Holding Bays and Runway Holding Positions. Inevitably, at a busy aerodrome, aeroplanes will be required to wait their turn for take-off. It is common to see a stream of traffic waiting along the taxiway for take-off, but at an international airport the queues for take-off can exceed the capability of the taxiway to accommodate all the aircraft waiting. In this situation or where environmental considerations exist, holding bays are provided adjacent to runway entrances which leave the taxiways clear. At some major aerodromes with particularly high traffic levels or intense peaks in traffic density, ‘sin bins’ are established to take aeroplanes out of the stream if something has gone wrong. Regardless of the position of holding bays, the entrance to the runway will be protected by a defined mandatory holding point set back from the edge of the runway to accommodate all the traffic using the runway. A runway holding position must be established on a taxiway if the location or alignment of the taxiway is such that a taxiing aircraft or vehicle can infringe an obstacle limitation surface or interfere with the operation of radio navigation aids (ILS or MLS). The method of indicating a runway holding position is covered later in the notes (under Signs and Markings). A runway holding position, or positions, must be established at the distances in the table on page 384 at an intersection of a taxiway with a runway; and an intersection of a runway with another runway when the former runway is part of a standard taxi-route.

Aerodromes - Physical Characteristics 19

383

19 Aerodromes - Physical Characteristics

Characteristics Physical - Aerodromes 19

Figure 19.11 Holding points

Runway Holding Point Positions (Distance from Centre Line of Runway)

 

Type of Runway

 

Runway code number

 

 

 

 

 

 

 

 

1

2

 

3

4

 

 

 

 

 

 

 

 

 

 

 

Take-off

30 m

40 m

 

75 m

75 m

 

 

 

 

 

 

 

 

Non-instrument (Visual)

30 m

40 m

 

75 m

75 m

 

 

 

 

 

 

 

 

Non-precision Instrument

40 m

40 m

 

75 m

75 m

 

 

 

 

 

 

 

 

Precision CAT I

60 m(b)

60 m(b)

 

90 m(a,b)

90 m(a,b,c)

 

 

 

 

 

 

 

 

Precision CAT II/III

-

-

 

90 m(a,b)

90 m(a,b,c)

 

 

 

 

 

 

Notes:

 

 

 

 

 

a.

May be increased if holding elevation lower than runway

 

 

b.

May be increased to avoid interference with radio navigation aids

 

c.

For code F this should be 107.5 m

 

 

 

 

Figure 19.12 Minimum distances from runway centre lines of holding positions

384

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