CAT.POL.A.330 Landing – dry runways

LANDING DISTANCE CORRECTION FACTORS

(a)Unless otherwise specified in the AFM, or other performance or operating manuals from the manufacturers, the variable affecting the landing performance and the associated factor that should be applied to the AFM data are shown in the table below. It should be applied in addition to the operational factors as prescribed in CAT.POL.A.330 (a) and CAT.POL.A.330(b). Table 1 Landing distance correction factors

(b)The soil should be considered firm when there are wheel impressions but no rutting.

RUNWAY SLOPE Unless otherwise specified in the AFM, or other performance or operating manuals from the manufacturer, the landing distances required should be increased by 5 % for each 1 % of downslope.

LANDING MASS CAT.POL.A.330 establishes two considerations in determining the maximum permissible landing mass at the destination and alternate aerodromes.

(a)Firstly, the aeroplane mass will be such that on arrival the aeroplane can be landed within 70 % or 80 %, as applicable, of the LDA on the most favourable (normally the longest) runway in still air. Regardless of the wind conditions, the maximum landing mass for an aerodrome/aeroplane configuration at a particular aerodrome cannot be exceeded.

(b)Secondly, consideration should be given to anticipated conditions and circumstances. The expected wind, or ATC and noise abatement procedures, may indicate the use of a different runway. These factors may result in a lower landing mass than that permitted under (a), in which case dispatch should be based on this lesser mass.

(c)The expected wind referred to in (b) is the wind expected to exist at the time of arrival.

ALTERNATE AERODROMES The alternate aerodromes for which the landing mass is required to be determined in accordance with CAT.POL.A.330 are:

(a)destination alternate aerodromes;

(b)fuel ERA aerodromes; and

(c)re-dispatch or re-clearance aerodromes.

LANDING DISTANCES AND CORRECTIVE FACTORS The AFM provides performance data for the landing distance under conditions defined in the applicable certification standards. This distance, commonly referred to as the ALD, is the distance from the position on the runway of the screen height to the point where the aeroplane comes to a full stop on a dry runway. The determination of the ALD is based on the assumption that the landing is performed in accordance with the conditions and the procedures set out in the AFM on the basis of the applicable certification standards. As a matter of fact, any particular landing may be different from the landing technique that is assumed in the AFM for certification purposes. The aircraft may approach the runway faster and/or higher than assumed; the aircraft may touch down further along the runway than the optimum point; the actual winds and other weather factors may be different from those assumed in the calculation of the ALD; and maximum braking may not be always achievable. For this reason, the LDA is required by CAT.POL.A.330 and CAT.POL.A.335 to be longer than the ALD. The margins by which the LDA shall exceed the ALD on dry runways, in accordance with CAT.POL.A.330, are shown in the following Table 1.

Table 1: Corrective factors for dry runways

If the runway is wet and the AFM does not provide specific performance data for dispatch on wet runways, a further increase of 15 % of the landing distance on dry runways has to be applied, in accordance with CAT.POL.A.335, as shown in the following Table 2: Table 2: Corrective factors for wet runways

However, for aeroplanes approved under CAT.POL.A.355, when landing on wet runways, CAT.POL.A.355 further requires the flight crew to apply the longer of the landing distance resulting from the above table and the landing distance resulting from the application of CAT.OP.MPA.303(b).). If performance information for the assessment of LDTA is not available as per CAT.OP.MPA.303(b)(2), the required landing distance on wet runways should be at least: 1.15 x 1.67 x ALD for turbojet-powered aircraft and 1.15 x 1.43 x ALD for turbopropeller-powered aircraft.