The indication of the sound power level
The indication of the sound power level provided for in Part 14 of the Annex shall be affixed, when applicable, visibly, legibly and indelibly on the UA, unless that is not possible or not warranted on account of the size of the product, and on the packaging.
To determine the UA’s sound power level (LWA), it is necessary to set up a test area where the device is placed at a sufficient distance from any reflective object that may cause any failure in the sound level measurement.
These tests will be performed with the device turned on, simulating a stationary flight phase. If it has accessories, tests will be done with all its possible configurations. The noise tests shall be carried out with the UA’s rotors operating at a speed corresponding to the UA’s hovering under MTOM. It will be necessary to perform several tests to corroborate that an acceptable acoustic level has been achieved.
The following process must be followed to calculate the surface time-averaged sound pressure level. The A-weighted surface time-averaged sound pressure level shall be determined at least three times for each UA configuration. If at least two determined values do not differ by more than 1 dB, further measurements will not be necessary. Otherwise, the measurements shall be continued until two values differing by no more than 1 dB are obtained. The surface time-averaged sound pressure level for calculating the sound power level of a UA configuration is the arithmetic mean of the two highest values that do not differ by more than 1 dB. The report shall contain the technical data necessary to identify the source under test and the noise test code, and the acoustical data.
The maximum sound power level, depending on the class of the UA, is shown in the following table.
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