Federal Register - August 27, 2021

Versión en texto ¿Qué es?Dateas es un sitio independiente no afiliado a entidades gubernamentales. La fuente de los documentos PDF aquí publicados es la entidad gubernamental indicada en cada uno de ellos. Las versiones en texto son transcripciones no oficiales que realizamos para facilitar el acceso y la búsqueda de información, pero pueden contener errores o no estar completas.

Fuente: Federal Register

Federal Register / Vol. 86, No. 164 / Friday, August 27, 2021 / Notices minimal influence of wind on the noise recording.
d Hover condition 2 sound elevation angle at 45 degrees: The aircraft maintains a hover condition at a lateral distance of 20 feet to the microphone position and at 20 feet AGL. Test when the conditions are optimal for minimal influence of wind on the noise recording.
e Hover condition 3 overhead, or sound elevation angle at 90 degrees:
The aircraft maintains a hover condition at 20 feet AGL and hold centered within
270 degrees relative to the microphone position for hover conditions described in paragraphs 16c and d of this rule, stabilize the aircraft in hover and record the sound in accordance with paragraph 16f of this rule.
c Hover condition 1 sound elevation angle at zero degrees: The aircraft maintains a hover condition at a lateral distance of 20 feet to the microphone and at 4 feet AGL rotors in the same plane as the microphone. Test when the conditions are optimal for
48287

a one foot radial over the microphone location.
f For the noise measurements at each hover condition, record the value of the equivalent sound level Leq and SPL in 13 octave bands for a minimum of 30
seconds for each of the test conditions paragraphs 16c through e of this rule.
g The tolerance of the hover height or lateral distance is within 1 ft., and the tolerance of the headings is within 5 degrees.

3

!

I
ol
!

11:1

4 microphone

l
0

Sketch of supplemental hover test conditions. D = 20 feet.
b Acoustic equipment that meets the specifications prescribed in paragraphs 19 and 20 of this rule; and c The calibration and measurement procedures prescribed in paragraphs 21 and 22 of this rule.
18 Measurement of aircraft noise received on the groundNoise unit definition Reference part 36, appendix J, section J36.109b, as modified:
a The sound exposure level, as expressed in LAE, is defined as the level,
L Where T0 is the reference integration time of one second and t2t1 is the integration time interval.

VerDate Sep<11>2014

17:52 Aug 26, 2021

Jkt 253001

log
2 P
At dt 10 To h1
Po
2.

rtz
dB

c The integral equation of paragraph 18b can also be expressed as:

PO 00000

Frm 00174

Fmt 4703

Sfmt 4703

E:FRFM27AUN1.SGM

EN27AU21.008

lotter on DSK11XQN23PROD with NOTICES1

AE

= 10

in decibels, of the time integral of squared A-weighted sound pressure PA over a given time period or event, with reference to the square of the standard reference sound pressure P0
of 20 micropascals and a reference duration of one second.
b The sound exposure level in units of decibels dB is defined by the expression:

27AUN1

EN27AU21.007

17 Measurement of aircraft noise received on the groundGeneral Reference: Part 36, appendix J, section J36.109a, as modified: Aircraft noise measurements made for the purpose of noise certification in accordance with the requirements of this regulation must be obtained using:
a The noise evaluation metric prescribed in paragraph 18 of this rule;

Acerca de esta edición

Federal Register - August 27, 2021

TítuloFederal Register

PaísEstados Unidos de América

Fecha27/08/2021

Nro. de páginas293

Nro. de ediciones7794

Primera edición14/03/1936

Ultima edición12/06/2026

Descargar esta edición

Otras ediciones

<<<Agosto 2021>>>
DLMMJVS
1234567
891011121314
15161718192021
22232425262728
293031