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Analysis and Ranking of the Acoustic Disturbance Potential of ...

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Report No. 6945<br />

BBN Systems arid Technologies Corporation<br />

-<br />

similar single-engine airplane) was determined to cause hauled out harbor<br />

seals to vacate <strong>the</strong> beach most <strong>of</strong> <strong>the</strong> t,ime. [This estimate was based on<br />

observations for flyovers at ranges <strong>of</strong> about 120 m (Johnson 1977).] The<br />

response <strong>of</strong> walruses varies widely but <strong>the</strong>y were reported to become alert <strong>and</strong><br />

move into <strong>the</strong> water when "aircraftn approach within 1-1.5 km at altitudes<br />

varying from 150 to 1500 m (Salter 1979). If <strong>the</strong> aircraft is assumed to be a<br />

twin engine turboprop, an estimated received level <strong>of</strong> 100 dB is obtained using<br />

a slant range <strong>of</strong> 1 km. The overall ambient noise level on beaches <strong>of</strong>ten<br />

exceeds this value because <strong>of</strong> surf noise (see Fig. 3.10). This suggests that<br />

walruses are reacting to.visua1 stimuli ra<strong>the</strong>r than acoustic, or perhaps both.<br />

Alternatively, <strong>the</strong> observations may have been made on protected beaches with<br />

no surf <strong>and</strong> low ambient noise or for overflights with larger aircraft than<br />

that assumed in <strong>the</strong> analysis. Among <strong>the</strong> o<strong>the</strong>r Alaskan pinniped species that<br />

have been observed to react to aircraft, specific response thresholds have not<br />

been reported.<br />

Table 5.13.<br />

Airborne Sound Zone <strong>of</strong> Influence Estimates for Pinnipeds.<br />

Minimum slant range for probable disturbance by aircraft 1<br />

Species Harbor Seal Pacific Walrus<br />

L, Criterion 2 110 dB 100 dB<br />

- - -<br />

Light 1-eng Prop<br />

Light 2-eng TProp<br />

120 m<br />

300 m<br />

B737-200 400 m<br />

B727<br />

F-4C Military<br />

420 m<br />

1100 m<br />

Notes: (1)<br />

Range estimated by using Eq. (13) for St<strong>and</strong>ard Day Conditions<br />

toge<strong>the</strong>r with aircraft radiated noise data from Table A-3.<br />

(2) The Lr criterion for probable disturbance is determined by using<br />

observed response information from Sec. 2.4 <strong>and</strong> estimating <strong>the</strong><br />

Lr in <strong>the</strong> dominant b<strong>and</strong>width for <strong>the</strong> aircraft type <strong>and</strong> range.

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