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Getting to Grips with Aircraft Noise

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8 - FLYING A NOISE ABATEMENT<br />

DEPARTURE PROCEDURE<br />

8.6. THE AIRBUS DEPARTURE ANALYSIS SOFTWARE (ADAS)<br />

This <strong>to</strong>ol will be integrated in the PEP environment in 2004, as an "on-ground"<br />

preparation <strong>to</strong>ol in order <strong>to</strong> compute the optimized inputs <strong>to</strong> set in the FMS2-NADP<br />

panel. This will fasten the optimization process, which is currently manual and takes<br />

several hours.<br />

8.6.1. ADAS INPUTS<br />

8.6.1.1. TAKEOFF OPTIMIZATION INPUTS<br />

Temperature, wind, pressure altitude, takeoff configuration (fixed or <strong>to</strong> be optimized),<br />

runway characteristics (Slope, TORA, TODA, ASDA, obstacles <strong>to</strong> be considered,<br />

runway state...). If the TOW is fixed, the <strong>to</strong>ol will maximize the TFLEX value for that<br />

actual weight.<br />

8.6.1.2. NOISE INPUTS<br />

Acoustic constraints, microphone positions...<br />

8.6.1.3. OPERATIONAL FLIGHT PATH INPUTS<br />

Type of <strong>Noise</strong> Abatement Departure Procedure: Close-in, Distant.<br />

Some of the input parameters (acceleration altitude, thrust reduction altitude, rating after<br />

reduction…) may be fixed by the user. If not, the <strong>to</strong>ol will optimize them.<br />

52<br />

Flight Operations Support & Line Assistance<br />

<strong>Getting</strong> <strong>to</strong> grips <strong>with</strong> aircraft noise

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