ADA-154319
NTIS
Information is our business.
U.S. DEPARTMENT OF COMMERCE
National Technical Information Service
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Perceived Noise level (PNL) |
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2.3.2 |
Sound Exposure Level (SEL) |
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24-Hour Above (TA) |
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2.5.2 |
Day, Evening, Night (TA) |
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2.7 |
Evaluation of the DNL Metric for Heliport/ Helistop Noise Impact Assessment |
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1.1 |
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3.1 |
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6.1 |
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6.3 |
Permissible Distance Between a Speaker and Listeners of Voice and Ambient Level |
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7.1 |
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AI |
Articulation Index |
AICUZ |
Air Installation Compatible Use Zones |
AIR |
Aerospace Information Report |
ALM |
A-Weighted Maximum Sound Level |
ANSI |
American National Standards Institute |
ARP |
Aerospace Recommended Practice |
CHABA |
Committee on Hearing, Bioacoustics and Biomechanics |
CNEL |
Community Noise Equivalent Level |
CNR |
Composite Noise Rating |
dB |
Decibel |
DNL |
Day-Night Average Noise Level |
DOT |
Department of Transportation |
DRC |
Damage Risk Criteria |
EPA |
Environmental Protection Agency |
EPNL |
Effective Perceived Noise level |
HUD |
Housing and Urban Development |
Hz |
Hertz |
ICAO |
International Civil Aviation 0rganization |
IEC |
International Electrotechnical Commission |
ISO |
International Standards 0rganization |
Ldn |
Day-Night Average Sound Level |
Leq |
Equivalent Sound Level |
Lx |
An Airport Cumulative Metric Derived from dBA |
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NASA |
National Aeronautics and Space Administration |
NEF |
Noise Exposure Forecast |
NIPTS |
Noise Induced Permanent Threshold Shift |
NNI |
Noise and Number Index |
NREM |
Non-Rapid Eye Movement Sleep |
NTSB |
National Transportation Safety Board |
OSHA |
Occupational Safety and Health Administration |
PNL |
Perceived Noise Level |
PNLT |
Tone Corrected Perceived Noise Level |
PSIL |
Preferred Speech Interference Level |
REM |
Rapid Eye Movement Sleep |
SAE |
Society of Automotive Engineers |
SEL |
Sound Exposure Level |
SIL |
Speech Interference Level |
SST |
Super Sonic Transport |
TA |
Time Above (a certain noise level) |
TTS |
Temporary Threshold Shift |
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Section 1.0 General Introduction
Aviation noise significantly affects
several million people in the United States. In a great number of instances,
aircraft noise simply merges into the urban din, a cacophony of buses, trucks,
motorcycles, automobiles and construction noise. However, in locations closer to
airports and aircraft flight tracks, aircraft noise becomes more of a concern.
The Federal Aviation Administration (FAA) presents this report in an effort to
enhance public understanding of the impact of noise on people and to answer many
questions that typically arise. Information on aircraft noise indices, human
response to noise, and criteria for land use controls is included. Additionally,
information on hearing damage is presented, along with occupational health
standards for noise exposure.
This document has been developed after
reviewing the rather extensive literature in each topical area, including many
original research papers, and also by taking advantage of literature searches
and reviews carried out under FAA and other Federal funding over the past two
decades. Efforts have been made to present the critical findings and conclusions
of pertinent research, providing, when possible, a "bottom line" conclusion,
criterion, or perspective to the reader concerned with aviation
noise.
How to Read This Document
1. If you want only a
general, non-technical presentation of the fundamental issues and concerns with
aircraft noise, read this introduction and the one-page summaries at the
beginning of each section.
2. If you are an engineer, planner, social
scientist or an individual conducting an environmental impact, assessment,
consider reading each section of interest in its entirety.
3. If you wish
to do an in-depth study, assessment or analysis, delve into the text and the
references listed. For more information, consider contacting the staff of the
FAA 0ffice of Environment and Energy, Noise Abatement Division,, in Washington,
D.C. 20591.
What is Sound?
Sound is a complex vibration
transmitted through the air which, upon reaching our ears, may be perceived as
beautiful, desirable, or unwanted. It is this unwanted sound which people
normally refer to as noise.
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Typical Decibel (dBA) Values Encountered in Daily Life and Industry*
Rustling leaves |
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Room in a quiet dwelling at midnight |
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Soft whispers at 5 feet |
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Men's clothing department of large store |
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Window air conditioner |
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Conversational speech |
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Household department of large store |
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Busy restaurant |
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Typing pool (9 typewriters in use) |
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Vacuum cleaner in private residence (at 10 feet) |
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Ringing alarm clock (at 2 feet) |
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Loudly reproduced orchestral music in large room |
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Beginning of hearing damage if prolonged exposure over 85 dBA
Printing press plant |
86 |
Heavy city traffic |
92 |
Heavy diesel-propelled vehicle (about 25 feet away) |
92 |
Air grinder |
95 |
Cut-off saw |
97 |
Home lawn mower |
98 |
Turbine condenser |
98 |
150 cubic foot air compressor |
100 |
Banging of steel plate |
104 |
Air hammer |
107 |
Jet airliner (500 feet overhead) |
115 |
* When distances are not specified, sound levels are the value at the
typical location of the machine operator.
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How Does Sound Get Around?
Sound moves outward from its point of origin in waves just as ripples move
outward from the point at which a pebble enters a pond.
Sound, just as
the ripple in the pond, requires a medium in which to travel; this medium is
usually air.
What is a Decibel?
The decibel (dB) is a
shorthand way to express the amplitude of sound (the relative height of those
ripples in the pond). Because the "ripples" of sound typically experienced may
vary in height from 1 to 100,000 "units", it becomes rather cumbersome to
maintain an intuitive feeling for what different values represent. The decibel
allows people to understand sound strength using numbers ranging between 20 and
120, a more familiar and manageable set of values. Table 1.1 provides a
listing Of some typical sounds and their respective sound levels (expressed in
decibels) at given distances.
The decibel also relates well to the way in
which people perceive sound. A 10 dB increase in a sound seems twice as loud to
the listener, while a 10 dB decrease seems only half as loud. In general,
changes in sound level of 3 or 4 dB are barely perceptible.
What is
Frequency or Pitch?
Some of the ripples in the pond may be very
short; these are analogous to high pitched sounds such as the voice of a
soprano. Other wavelets might be very broad; these waves are analogous to a bass
or baritone voice. Most sounds we hear are composed of a mixture of these
different length sound waves, giving complexity, richness and character to our
experience of sound.
What is the Most Important Effect of Aviation
Noise?
Annoyance is the most prevalent effect of aircraft noise. It
is important to note that while the overall, or average, community attitude
about a noise level is usually what is reported, some individuals will be much
more and others much less upset or annoyed with the sound in question. Figure 1.1 shows
this typical response pattern. This variation in response is what makes the
science of measuring "community response" a rather complicated
matter.
What are Other Principal Effects of Aircraft
Noise?
1. speech interference
2. sleep interference
3.
hearing damage risk
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While hearing damage is not a common result of aircraft noise exposure,
speech and sleep interferences are major concerns of neighbors close to
airports.
What are Some Less Frequently Identified Effects of Noise on
Humans?
1. physiological (cardiovascular and circulatory)
problems
2. psychological problems (stemming from intense
annoyance)
3. social behavioral problems
At the present time there
is no conclusive evidence to link these effects with aircraft noise. As
discussed in the text, these topical areas are often rife with conflicting
research results and are very controversial. The summary of the non-auditory
effects section (Section 8.0)
provides current guidance for interpreting these reported
effects.
What Other Areas May be Affected by Aircraft
Noise?
1. real estate values
2. land use
3.
wildlife
4. farm animals
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Years of experience in airport planning and development have resulted in
guidelines which match uses of land -- like hospitals or concert halls -- with
normally compatible noise levels; these guidelines are published in an FAA
regulation called Federal Aviation Regulation (FAR) PART 150. Implementation of
an FAR150 study will assist airport operators and neighbors in minimizing the
extent of non-compatible land uses.
While the reactions of animals to
noise have been studied, it is another research area plagued with widely varying
results. In all but extreme cases (such as in pristine wilderness or in the case
of excessive noise levels) wildlife and domesticated animals rarely display any
reactions to aviation noise.
How Do You Measure Aircraft
Noise?
sound is often measured using a sound level meter with a
filter which simulates the human hearing response. This filter and the human ear
give greater emphasis to sounds in the speech-important frequency bands and less
emphasis to the lower and higher frequencies. This differential response in the
human ear may have developed over the course of human evolution as a way to
filter the sounds of wind and water which might interfere with survival-related
communications such as "Here comes a Tyrannosaurus Rex--run for it!" In any
event, this filter is called the A-weighting filter, and the sound measured with
this filter is called the A-level (AL).
Now I Know What AL is, but I
Am Confused About "Energy Dose." What Exactly is the Sound Exposure Level
(SEL)?
When our sound level meter is measuring the AL, think of the
sound falling on the microphone like rain or snow. The maximum rate of rainfall
is the maximum AL. Now consider the sound level meter as a bucket or pail. After
the "noise event" has passed (aircraft flyover or truck passby) the rain or snow
collected in the bucket (having passed through the microphone) is the noise dose
or Sound Exposure Level (SEL). Essentially, loud noise events create a large
bucket (dose) of sound energy, while quieter events create smaller
buckets.
Now What Do I Do With "Buckets" of Noise (the Leq and
DNL)?
The buckets are typically collected over a 24-hour time period
and are poured into a large container. The total volume collected during the
24-hour time period is averaged to formulate a value called the "Equivalent
sound Level", or Leq. When the buckets collected during the nighttime hours are
multiplied by 10 (because of greater potential for disturbing people) and then
the volume averaged, we formulate a value called the "Average Day Night sound
Level" or DNL. The Leq and DNL are values one often encounters in looking at the
overall noise exposure from an airport operation.
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1. Richards, E. S, and J. B. Ollerhead. Noise Burden
Factor-
-New Way of Rating Airport Noise. Sound and Vibration,
V.7,
No, 12, December 1973.
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INTRODUCTION
This section describes the noise metrics utilized
in conducting analyses of aircraft noise. While dozens of additional metrics
exist, this section focuses on the officially designated family of indices. A
working knowledge of these measures is extremely valuable in understanding the
remainder of this report.
AVIATION APPLICATIONS/ISSUES
1.
Correlation between human response and various measures of sound.
2.
Selection of the best metrics for specific applications.
3. Selection of
weighting factors for sound occurring at various times of day.
4.
Selection of metrics which are accurate, relatively easy to measure, compute and
understand.
GUIDANCE/POLICY/EXPERIENCE
1. The fundamental
sound level metric designated as the A-Weighted Sound Level, or AL. This metric
has often appeared in the literature as dBA. It is designated for measuring
noise at an airport and surrounding areas by Part 150.
2. Single event
dose or energy metric designated as the Sound Exposure Level or SEL.
3.
Airport yearly average noise exposure measure designated as the Yearly Average
Day Night Level or DNL. The DNL has often appeared in the literature as Ldn..
Required by Part 150 to measure the exposure of individuals to noise resulting
from the operation of an airport.
4. Effective Perceived Noise Level or
EPNL designated as the certification metric for large transport turbojet
aircraft and helicopters.
5. Time functions of ALm (such as Time Above,
TA and L-Values, L-10) identified as supplementary metrics for use in
environmental impact analyses.
6. Octave and one-third octave spectra
identified as important in specific applications such as sound proofing and
speech interference studies.
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(2) Single Event Energy Dose
(3) Cumulative Energy Average Metrics
(4) Cumulative Time Metrics
The paragraphs below describe and
differentiate these four generic classes of acoustical metrics. An understanding
of these four classes essential for an individual undertaking a comprehensive
assessment of noise effects. (For mathematical formulations of each of the noise
metrics, the reader is referred to The Handbook of Noise Ratings (Ref. 1).
2.2 SINGLE EVENT MAXIMUM SOUND LEVEL METRICS
The
following noise metrics are generally related, each representing a maximum sound
level. The applications of these metrics are diagrammed in Figure 2.2.
2.2.1 A-Weighted Sound Level: ALm (Historically dBA),
Expressed in dB. The A-weighted Sound Level is the single event maximum
sound level metric. A-weighted sound pressure level is sound pressure level
which has been filtered or weighted to reduce the influence of the low and high
frequency extremes. Because unweighted sound pressure level does not correlate
well with human assessment of the loudness of sounds, various weighting networks
are added to sound level meters to attenuate low and high frequency noise in
accordance with accepted equal loudness contours. One of these weighting
networks is designated "A" (shown in Figure
2.3).
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It was originally employed for sounds less than 55 dB in level; now A-level
is used for all levels of sound because it has been found to correlate well with
people's subjective judgment of the loudness of sounds. Its simplicity and
superiority over unweighted SPL in predicting people's responses to noise have
contributed to its wide acceptance. The ALM is currently used for noise
certification of small propeller-driven aircraft; also, in FAA Advisory Circular
36-3C it is used as the basis for airport access restrictions which discriminate
solely on the basis of noise level.
2.2.2
D-Weighted Sound Level: DLm (Historicall dB(D)), Expressed in dB.
D-weighted sound pressure level or D-level is sound pressure level which has
been frequency-filtered to reduce the effect of the low frequency noise and to
recognize the annoyance at higher frequencies. D-level is measured in decibels
with a standard sound level meter with contains a "D" weighting network with the
response curve shown in Figure 2.3. D-level
was developed as a simple approximation of perceived noise level (PNL) for use
in assess aircraft noise. PNL, addressed in the next paragraph, can be estimated
from the D-level by this equation: PNL = dB(D) + 7.
2.2.3 Perceived Noise Level (PNL), Expressed in dB.
Perceived Noise Level (PNL) is a rating of the noisiness that has been used
almost exclusively in aircraft noise assessment. PNL is computed from sound
pressure levels measured in octave or one-third octave frequency bands. This
rating is most accurate in estimating the perceived noisiness of broadband
sounds of similar time duration which do not contain strong discrete frequency
components. Currently it is used by the FAA and foreign governmental agencies in
the noise certification process for all turbojet -- powered aircraft and large
propeller-driven transports. The perceived noise level is expressed in decibels.
These units translate the subjective linearly additive noisiness scale to a
logarithmic dB-type
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acoustical energy associated with the fluctuating sound (during the
prescribed time period) is equal to the total acoustical energy associated with
a steady sound level of Leq for the same period of time. The purpose of Leq is
to provide a single number measure of noise averaged over a specified time
period.
2.4.2 Day-Night Sound Level (DNL),
Expressed in dB. Day-Night Sound Level (DNL) was developed as a single
number measure of community noise exposure. It is often referred to as Ldn in
the literature. DNL was introduced as a simple method for predicting the effects
on a population of the average long term exposure to environmental noise. It is
an enhancement of the Equivalent Sound Level (Leq) because a correction for
nighttime noise intrusions was added. A 10 dB correction is applied to nighttime
(10 p.m. to 7 a.m.) sound levels to account for increased annoyance due to noise
during the night hours. DNL uses the same energy equivalent concept as Leq. The
specified time integration period is 24 hours. As in the case of Leq, there is
no stipulation of a minimum noise sampling threshold. The DNL can be derived
directly from the A-weighted sound level or the sound exposure level, as shown
in Figure 2.2.
For assessing long term noise exposure, the yearly average DNL (DNL y-avg) is
the specified metric in the FAA FAR Part 150 noise compatibility planning
process. In the remainder of this document, the term DNL will be used (in lieu
of DNL y-avg), yearly average being implied.
2.4.3
Community Noise Equivalent Level (CNEL), in dB. CNEL, like DNL,
incorporates the energy average A-weighted sound level integrated over a 24-hour
period Weightings are applied for the noise levels occurring during the evening
(7 p.m. - 10 p.m.) and nighttime (10 p.m. - 7 a.m.). CNEL differs from DNL in
the addition of the evening weighting step function of 3 dB which is intended to
account for activity interference and annoyance during that time period. It was
originally used by the state of California, but it is being phased
out.
2.4.4 Noise Exposure Forecast (NEF), in
dB. Noise Exposure Forecast performs the same role as DNL or CNEL but is
developed using EPNL as the intermediate single event dose metric. The NEF
metric incorporates a weighting factor which effectively imposes a 12.2 dB
penalty on sound occurring between 10 p.m. and 7 a.m. This corresponds to a
nighttime event multiplier of 16.7. NEF correlates extremely well with DNL and
the equivalency DNL = NEF + 35 is often used.
2.5
CUMULATIVE TIME METRICS
2.5.1 24-Hour
Time Above (TA), Expressed in Minutes. The 24-hour TA metric provides the
duration in minutes for which aircraft related noise exceeded specified
A-weighted sound levels. An example of a TA contour is shown in Figure 2.4. TA is
one of the criteria specified in HUD Circular 1390.2 for determining eligibility
for HUD construction funding (Ref. 3). TA'S
inverse, the L-value (e.g., L 10) is used (along with Leq) as the FHWA criteria
for planning and design of Federal-aid highways. Further, TA can be related
directly to some "threshold activated" physiological or annoyance effects.
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2.5.2 Day, Evening, Night (TA), Expressed in
Minutes. The Day-TA metrics provide the duration in minutes for which
aircraft related noise exceeded specified A-weighted sound levels during the
period 7:00 a.m. to 7:00 p.m. The Evening TA metrics provide the duration in
minutes for which aircraft related noise exceeded A-weighted sound levels during
the period from 7:00 p.m. to 10:00 p.m. The Night TA metrics provide the
duration in minutes for which aircraft related noise exceeded A-weighted sound
levels during the period from 10:00 p.m. to 7:00 a.m.
2.6 DNL: THE STANDARD CUMULATIVE AVERAGE ENERGY
METRIC
The FAA selected DNL as the cumulative average energy metric
to be used in airport noise exposure studies. While a dialogue continues within
research circles concerning weighting functions, the DNL has emerged as a sound
and workable tool for use in land use planning and in relating aircraft noise to
community reaction. The substantiating basis for the DNL can perhaps best be
summarized as follows:
1) Pragmatically speaking, it works. Engineers and planners have acquired
over 30 years working experience with a nominal 10 dB nighttime weighting
function. This experience has been successful, contributing to wise zoning and
planning decisions.
2) The nominal 10 dB decrease in ambient noise levels
in many residential areas at nighttime provides a sensible basis for the
weighting factor.
2.7 EVALUATION OF THE DNL METRIC
FOR HELIPORT/HELISTOP NOISE IMPACT ASSESSMENT
With the increase in
helicopter operations in and around urban areas, the FAA has sought to include
helicopters in the environmental planning process. In this context, the question
has arisen of whether or not the average cumulative energy metric DNL, which is
used in the analysis of noise from conventional aircraft, would also be
appropriate for analysis of helicopter noise. Most commercial airports have
hundreds of operations a day, while heliports generally handle fewer than
thirty. The metric used to analyze helicopter noise would have to be sensitive
enough to accurately reflect community response at comparatively low levels of
noise exposure (lower cumulative levels because of fewer flights).
In
order to investigate whether or not DNL would be appropriate, the FAA supported
a field test program to examine subjective response to helicopter operations.
The actual study was conducted by NASA Langley Research Center and is summarized
below (Ref. 4).
In the study, researchers examined the reaction of community residents to low
numbers of helicopter noise events. Residents of the selected community were
interviewed twenty-three times about their general noise annoyance on particular
days. Unknown to them, on those days helicopter flights had been controlled for
the test purpose; the number of flights per day varied from 0 to 32. The
exposure varied randomly through each of the
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METRIC |
DESCRIPTION |
One-third Octave Sound Pressure Levels |
The one-third octave band sound pressure levels are the starting point for all other metrics; useful in implementation of soundproofing |
PNL |
Sound Level from which EPNL was developed |
PNLT |
Sound Level from which EPNL was developed |
EPNL |
A maximum sound level single event cumulative metric developed from the PNLT and PNL sound level. Used in FAR Part 36, Appendix C Certification, Advisory Circular 36-lB and Advisory Circular 36-2A. |
NEF |
An Airport cumulative metric no longer in use in the U.S. but often used in older studies; replaced by DNL (the FAA approved metric) |
Alm |
A sound level metric applied as follows:
1050.lC Analysis FAR Part 36 Appendix F Certification Specific eligibility for Soundproofing Implementation of Soundproofing Noise Monitoring Systems FAA Advisory Circular |
TA |
An airport cumulative metric derived from dB(A) and applied as follows:
l050.lD Analysis Noise Monitoring Systems |
Lx |
An airport Cumulative metric derived from dB(A) and applied as follows:
l050.lD Analysis Noise Monitoring Systems |
SEL |
A maximum sound level, single event cumulative metric derived from dB(A) and applied as follows:
Noise Monitoring Systems |
Leq |
An airport cumulative metric derived from SEL; no application in aviation |
DNL |
An airport cumulative metric derived from SEL with the following applications:
Airport Noise Analysis FAR l050.lD Analysis General Eligibility for Soundproofing Noise Monitoring Systems |
CNEL |
An airport cumulative metric derived from SEL used only by the state of California; CNEL will be phased out in the next few years. |
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1. Pearson, Karl. Handbook of Noise
Ratings. Bolt, Beranek and Newman, Inc. NASA CR-2376, April 1974.
2. Hassall, J.R. and K. Zaveri. Acoustic Noise
Measurements. Bruel & Kjaer, January 1979.
3.
Housing and Urban Development Circular 1390.2.
4.
Fields, James M. and Clemans A. Powell. Community Survey of Helicopter Noise
Annoyance Conducted Under Controlled Noise Exposure Conditions. Unpublished
Report, December 1984.
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Section 3.0 ANNOYANCE AND AIRCRAFT NOISE
INTRODUCTION
The typical response of humans to aircraft noise
is annoyance. Annoyance response is remarkably complex and, considered on an
individual basis, displays wide variability for any given noise level.
Fortunately, when one considers average annoyance reactions within a community,
one can develop aggregate annoyance response/noise level relationships. This
section introduces the reader to the factors which influence individual
annoyance response. Also included are examples of research findings which
display aggregate community annoyance responses.
AVIATION
APPLICATION/ISSUES
Annoyance is the number one consequence of
excessive aircraft noise. The continued growth of the aviation industry and
expansion of airport capacity is in part dependent on how well noise
compatibility planning is
handled.
GUIDANCE/POLICY/EXPERIENCE
It is the charter of
the FAA to assure safety and promote civil aviation. Promoting civil aviation
means, among other things, addressing the problems of aircraft noise annoyance.
The FAA, working with other members of the community, has taken a series of
steps designed to bring about greater compatibility between aircraft noise
levels and affected individuals. Actions include:
1. Source noise
certification regulations
2. FAR Part 150 Airport Noise Exposure / Land Use
Compatibility Planning Process
3. Research into the mechanism of annoyance to
aircraft noise
4. Advisory publications designed to mitigate aircraft noise
impact on noise sensitive areas.
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alienated or of being ignored and abused is the root of many human annoyance
reactions. If people feel that those creating the noise care about their welfare
and are doing what they can to mitigate the noise, they are usually more
tolerant of the noise and are willing and able to accommodate higher noise
levels.
B. Judgment of the Importance and Value of the Activity which
is Producing the Noise. If the noise is produced by an activity which people
feel is vital, they are not as bothered by it as they would be if the
noise-producing activity was considered superfluous.
C. Activity at
the Time an Individual Hears a Noise. An individual's sleep,, rest and
relaxation have been found to be more easily disrupted by noise than his
communication and entertainment activities.
D. Attitudes about
Environment. The existence of undesirable features in a person's residential
environment will influence the way in which he reacts to a particular
intrusion.
E. General Sensitivity to Noise. People vary in their
ability to hear sound, their physiological predisposition to noise and their
emotional experience of annoyance to a given noise.
F. Belief about
the Effect of Noise on Health. The extent to which people believe that
exposure to aircraft noise will damage their health affects their response to
aviation noise.
G. Feeling of Fear Associated with the Noise. For
instance, the extent to which an individual fears physical harm from the source
of the noise will affect his attitude toward the noise.
3.3.2 Physical Variables. A number of physical factors
have also been identified by researchers as influencing the way in which an
individual may react to a noise. These factors include:
A. Type of
Neighborhood. Instances of annoyance, disturbance and complaint associated
with a particular noise exposure will be greatest in rural areas, followed by
suburban and urban residential areas, and then commercial and industrial areas
in decreasing order. The type of neighborhood may actually be associated with
one's expectations regarding noise there. People expect rural neighborhoods to
be quieter than cities. Consequently, a given noise exposure may produce greater
negative reaction in a rural area.
B. Time of Day. A number of
studies has suggested that noise intrusions are considered more annoying in the
early evening and at night than during the day.
C. Season. Noise
is considered more disturbing in the summer than in the winter. This is
understandable since, during the summer, windows are likely to be open and
recreational activities take place out of doors.
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D. Predictability of the Noise. Research has revealed that individuals
exposed to unpredictable noise have a lower noise tolerance than those exposed
to predictable noise.
E. Control over the Noise Source. A person
who has no control over the noise source will be more annoyed than one who is
able to exercise some control.
F. Length of Time an Individual Is
Exposed to a Noise. There is little evidence supporting the argument that
annoyance resulting from noise will decrease with continued exposure; rather,
under some circumstances, annoyance may increase the longer one is
exposed.
3.4 REVIEW OF RECENT
RESEARCH
The inherent variability in the way individuals react to
noise makes it impossible to predict accurately how any one individual will
respond to a given noise. However, when one considers the community as a whole,
trends emerge which relate noise to annoyance. In this way it is possible to
correlate DNL with community annoyance. This measure will represent the average
annoyance response for the community.
In any community there will be a
given percentage of the population highly annoyed, a given percentage mildly
annoyed and others who will not be annoyed at all. The changing percentage of
population within a given response category is the best indicator of noise
annoyance impact.
Various studies have focused on the relationship
between annoyance and noise exposure, one researcher, in analyzing the results
of numerous social surveys conducted at major airports in several countries,
derived the curves shown in Figure 3.1 relating
degree of annoyance and percent of population affected with noise exposure
expressed in DNL (Ref. 1). A survey
conducted in the Netherlands investigated the relationship between the DNL and
the percentage of those questioned who suffered feelings of fear, disruption of
conversation, sleep or work activities (Ref. 2). Figure 3.2 reflects
these findings.
In 1960 the "Wilson Committee" was appointed by the
British Government to investigate the nature, sources and effects of the problem
of noise (Ref.
3). The final report, published in 1963, included results of extensive
examination of community response to aircraft operations at London Heathrow
Airport. Figure
3.3, adapted from that report, shows the relationship between DNL and the
percent of the population disturbed in various activities including sleep,
relaxation, conversation and television viewing. Disturbance response categories
for startle and house vibration are also included.
The EPA publication
"Information on Levels of Environmental Noise Requisite to Protect Health and
Welfare with an Adequate Margin of Safety" provides a relationship between the
percent of population highly annoyed and the Day-Night Sound Level (DNL) (Ref. 4). These data
are shown in Figure
3.4, along with the relationship between annoyance, complaints and community
reaction.
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3.5 CONCLUSION
This section has presented a
series of relationships useful in interpreting average community response to
aircraft noise. These data should provide the reader with the necessary
perspective to begin understanding the human reactions to various levels of
cumulative noise exposure (DNL).
1. Richards, E. J, and J. B. 0llerhead. Noise Burden
Factor - New Way of Rating Airport Noise. Sound and Vibration, V. 7,
No, 12, December 1973.
2. Kryter, Karl D. The
Effects of Noise on Man. New York, Academic Press, 1970.
3. Great Britain Committee on the Problem of Noise. Noise, Final
Report. Presented to Parliament by the Lord Minister for Science by Command of
Her Majesty. London, H. M. Stationery Office, July 1963.
4. U.S. Environmental Protection Agency, Office of Noise
Abatement and Control, Washington, D.C. Information on Levels of Environmental
Noise Requisite to Protect Public Health and Welfare with an Adequate Margin of
Safety. March 1974.
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Section 4.0 DIFFERENT SOURCES/DIFFERENT HUMAN RESPONSE?
INTRODUCTION
This section addresses a fundamental question
raised from time to time in connection with aviation noise related law suits,
environmental impact assessments, and research studies. It has been suggested
that aircraft noise levels should be treated as more annoying to people than the
same sound levels generated by other sources. A review of the research shows
that very strong positions have been taken both supporting and opposing the
theory. The most recent papers appearing in the scientific journals concede that
a differential in response may exist but it can not be shown to be statistically
significant.
AVIATION APPLICATIONS/ISSUES
Should aircraft
noise be considered as comparable to noise from other sources in the land use
planning and environmental assessment
process?
GUIDANCE/POLICY/EXPERIENCE
In the general
application of noise exposure/land use criteria, aircraft noise should be
considered in the same manner as noise from other sources.
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4.1 INTRODUCTION
In assessing comparative
contributions to the overall annoyance with noise experienced by an individual,
the issue of whether or not aircraft noise should be compared with other ambient
sources continues to arise. The issue is an important one in terms of
establishing acceptable cumulative noise exposure levels for various land use
categories. This section reviews current literature on this controversial
topic.
4.2 SCHULTZ - KRYTER DEBATE
In
1978, Theodore Schultz published an article synthesizing results from many
social surveys on noise annoyance. In this article he stated that it is possible
to compare aircraft and other transportation noise equally, and to find and use
a median annoyance response curve for them (Ref. 1). In order
to compare these various results, Schultz developed some theories and formulas
with which he determined which parts of each survey would fall into the "highly
annoyed" category. He also figured the DNL indices for these surveys and plotted
them (see Figure
4.1). Figure
4.2 reproduces Schultz's "synthesis curve", the median of all the noise
surveys.
Karl Kryter, responding in 1982 to Schultz's article, proposed a
different relationship (Ref. 2).. While
Schultz only considered people who were highly annoyed, Kryter stated that all
individuals annoyed should be considered in these comparisons. He also developed
the DNL values for each study differently, so his values varied significantly
from those of Schultz. Kryter also attempted to explain the poor correlation
between noise exposure and annoyance in individuals by explaining that, while it
is assumed that noise exposure is homogeneous over a given neighborhood, an
individual's particular dose of noise may vary quite a bit.
Kryter cited
Grandjean (Ref.
3), another researcher who found that aircraft noise is significantly more
disturbing than other noise. This Swiss study stated that it took a DNL of 10 to
15 dB higher for road traffic noise to cause equal disturbance as aircraft.
Kryter then explained his concept of the "effective exposure" of noise, rather
than the exposure that may actually be measured or reported. Kryter suggests
that because aircraft noise falls over a structure, like a house, equally, as
opposed to passing through interfering structures as traffic noise would do (as
in moving from the front to the back of a house), the "effective noise exposure"
would be greater than that of traffic noise. Kryter further submits that, for a
house facing the road, residents in the back yard would experience diminished
noise from those in the front yard; however, they would all experience equal
aircraft noise. Likewise, each room in the house would experience nearly
identical exposure to aircraft noise (Kryter evidently only considered single -
level homes). Kryter found a front to back of house difference of 17 - 21 dB for
road traffic and only 0.3 dB for aircraft noise. Thus, Kryter suggests that
aircraft noise must be considered separately from other transportation
noise.
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For the same noise level, a greater percentage of
people are highly annoyed by aircraft noise. The
difference in annoyance at the two sources is not
constant but instead increases as Ldn increases. The
difference in annoyance is equivalent to about 8 dB at
Ldn of 55 dB increasing to about 15 dB at Ldn of 65 dB.
Hall puts forth some possible explanations of these variations. For example,
the sporadic time pattern of aircraft noise differs from the relatively steady
noise of road traffic. Thus, maximum levels for aircraft noise will be higher.
Hall suggests that until further work can be done, "Ldn is a reasonable
predictor of response to any particular source, but there are differences in
response to different sources at the same Ldn value." Hall concluded that the
best thing to do, then, would be to use separate functions to estimate community
response to different types of noise.
In a later article (published in
December 1984), Hall further addressed this complex issue, substantially
altering his previous conclusions (Ref. 5). He
references about a dozen papers published on this subject over the last five
years. Hall suggests that intrinsic differences may exist but can not be
substantiated as statistically significant. His summary statements are excerpted
below:
The overwhelming conclusion from the recent literature is that different studies have led to different dose-response functions. This has happened for different sources, for different types of one source, and even for different studies at the same location (e.g., Heathrow). There is some consistency of evidence that the annoyance response function for rail noise is lower than for road or aircraft noise. (Rohrmann reaches the same conclusion in his review of relevant literature.) There is also some indication, but with fewer studies pertaining to it, that the aircraft annoyance function is higher than that for road traffic. However, the evidence is not strong enough to totally reject the hypothesis that all of this is just random variation about the "average" response.
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Lastly, an "average" dose-response function appears to be useful in two
contexts, both defined by limited information. The first is the general
situation we are now in, in which it appears that different dose-response
functions are warranted, but we cannot specify precisely the conditions calling
for each. Although we suspect the variance in results is not simply random, it
almost behaves as if it were, in which case the "average" function represents
our best current estimate. The second situation will arise in the future, when
we may be able to specify clearly the conditions calling for separate
dose-response functions. Even then, there will undoubtedly be conditions which
we cannot categorize, in which case again the "average" response function would
be. the best one to use.
4.4
CONCLUSION
For matters of policy, there does not exist at this
time enough evidence to support the requirement of a differential for comparing
aircraft noise with noise from other sources. All transportation and other
ambient noise sources therefore can be treated as comparable when considering
aviation noise impact.
1. Schultz, Theodore. Synthesis of Social Surveys on Noise
Annoyance. J. Acoust. Soc. Am. 64, 1978.
2.
Kryter, Karl D. Community Annoyance from Aircraft and Ground Vehicle Noise.
J. Acoust. Soc. Am. 72 (4), October 1982.
3.
Grandjean, P. Graf, A. Lauber, H.P. Meier, and R. Huller. Survey on the Effects
of Aircraft Noise in Switzerland. Inter-Noise 76, Washington, D.C., April
1976.
4. Hall, Fred L., Susan E. Bernie, Martin
Taylor, and John E. Palmer. Direct Comparison of Community Response to Road
Traffic Noise and to Aircraft Noise. J. Acoust, Soc. Am. 70 (6), December
1981.
5. Hall, Fred L. Community Response to Noise: Is
All Noise the Same? J. Acoust. Soc. Am. 76 (4), October 1984.
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INTRODUCTION
This section describes the human hearing mechanism
and the processes of temporary and permanent hearing loss. The results of
research are presented and the potential for hearing loss in aviation noise
environments evaluated. OSHA hearing protection criteria are also
addressed.
AVIATION APPLICATIONS/ISSUES
1. Permanent or
temporary hearing loss.
a. cockpit crew
b. flight attendants
c.
passengers
d. persons in communities exposed to
aircraft
overflight
2. Temporary hearing loss for the same categories
of individuals listed above.
GUIDANCE/POLICY/EXPERIENCE
1.
FAA-sponsored research results show that permanent hearing loss is not a
likelihood for a) cockpit crew, b) flight attendants, c) passengers, d) people
exposed to overflights.
2. Temporary hearing loss (up to several hours
recovery time) may occur in commercial aviation noise environments. These
temporary sensitivity shifts are not unusual in the industrial setting and do
not exceed OSHA criteria.
3. Persons on the ground exposed to aircraft
overflights would typically not experience any temporary hearing loss due to the
relatively short duration of the noise exposure.
4. A greater degree of
temporary and possible permanent hearing loss can result in the case of long
exposure times in certain small propeller driven aircraft.
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5.1 INTRODUCTION
It is well established
that continuous exposure to high levels of noise will damage human hearing. This
section begins with a description of the hearing mechanism, followed by
discussion of the effects of noise on hearing, along with criteria for hearing
protection established by the military, the FAA and OSHA. Finally, methods for
protection of hearing are discussed.
5.2 THE
HEARING MECHANISM
The ear is an external sense organ designed to
receive and respond to air-borne acoustic vibratory energy. Figure 5.1 provides
a schematic cross section showing the outer, middle and inner ears. The external
ear, made up of the auricle (the outer portion of the ear) and the ear canal,
transmits sounds to the eardrum. The eardrum, which is a very thin membrane that
moves very slightly in response to sound pressure levels, separates the ear
canal from the middle ear.
The middle ear is an air-filled cavity that
lies between the outer and the inner ear (see Figure 5.2). It
acts as a mechanical amplifier of the air pressure vibrations from the eardrum
and through a series of bones called the ossicles. Air pressure vibrations
displace the eardrum, which then displaces the ossicles, a link of three small
bones which reach across the middle ear cavity to the delicate, fluid-filled
membranes of the inner ear. The ossicles, made up of the malleus, the incus and
the stapes, rest against the opening to the inner ear, the oval window; when the
ossicles are displaced, the stapes pushes through the oval window, displacing
the fluid in the inner ear.
The middle ear allows pressure variations in
air to be transmitted into pressure variations in fluid with very little loss of
energy. This is due in part to the relative size difference between the eardrum
and the oval window (the eardrum has an area 20 times that of the oval window).
Thus, the force exerted on the inner ear fluid by the stapes is about the same
as the force exerted on the eardrum by the sound wave in the air, but the
resulting pressure is much greater -- as much as a ratio of 22 to 1.
The
inner ear contains the final section of the organ of hearing, the cochlea, which
rests, coiled like a snail, against the oval window. As the stapes forces the
oval window in and out, the fluid of the cochlea is also moved. About thirty
thousand hair cells (called cilia) located in the cochlea react to the fluid
motions, translating them to nerve impulses (and converting them from mechanical
to electrical energy), then transmitting the impulses to the brain for
interpretation.
Acoustical energy may also be conducted to the inner ear
through vibration of bone. An example is the sound of one's own voice.
Bone-conducted vibrations set up similar patterns of vibration of the cochlear
partition as does air-conducted sound.
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the effects of noise on the crew and passengers inside an aircraft or on the
effects of noise on individuals regularly exposed to aviation noise, such as
people who reside around airports.
5.6.1
Interior Aircraft Noise. The FAA, in 1981, sponsored research to
investigate the potential impact of interior aircraft noise on the crew and
passengers of an aircraft (Ref. 2). The
researchers concluded that the damage risk criteria of CHABA, discussed in the
above paragraphs, is adequate for evaluation of potential hearing damage in both
commercial and business jet-powered aircraft. Interior noise levels in both
types of aircraft were tested, and none of the average levels in commercial or
business jets exceeded the CHABA recommended levels. The study reports that less
than 0.l% of the commercial and less than l% of business jets are expected to
exceed damage risk contours. Given these small percentages, the researchers drew
the following conclusions:
For the crew of an aircraft, long
exposures to noise of as many as sixteen hours flight time should not present
any problems as long as the average daily exposure is four hours. (Four hours is
currently the maximum average daily amount flown in commercial jet
aircraft.)
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1. Michael, P.L., 14.T. Anchor, G.R. Bienvenue et al.
Community Noise Fundamentals: A Training Manual and Study Guide.
Pennsylvania State University College of Education, June 1980.
2. Pearson, Karl S, and John F, l4ilby. "Possibility of
Hearing Loss from Exposure to Interior Aircraft Noise." Ref. No.
FAA-AEE-81-15, November 1981.
3. Parnell, Nagel, &
Cohen, "Evaluation of Hearing Levels of Residents Living Near a Major
Airport," Report FAA-RD-72-72, June 1972.
4. Ward,
Cushing & Burns, "TTS From Neighborhood Aircraft Noise," Journal
of Acoustical Society of America, Vol. 60, No. 1, July 1976.
5. Kabuto & Suzuki, "Temporary Threshold Shift from
Transportation Noise," Journal of Acoustical Society of America, Vol.
66, No. 1, July 1979.
6. Occupational Safety and
Health Administration, Code of Federal Regulations, Title 29, Chapter 27, Part
1910.
7. U.S. Environmental Protection Agency,
"Information on Levels of Environmental Noise Requisite to Protect Public
Health and Welfare with an Adequate Margin of Safety," EPA 550/9-74-004,
March 1974.
8. U.S. Air Force Regulation 161-35, April
1982.
9. U.S. Air Force. Design Note 3F1, January
1974.
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Section 6.0 SPEECH INTERFERENCE
INTRODUCTION
Speech interference is a principal factor in human
annoyance response. It can also be a critical factor in situations requiring a
high degree of intelligibility essential to safety. This section contains a
summary of research results useful in estimating the degree of speech
intelligibility as a function of distance in various ambient noise environments.
Criteria are also presented defining levels of intelligibility deemed acceptable
(through experience) in various work situations.
AVIATION
APPLICATIONS/ISSUES
1. Annoyance to aircraft noise
2.
Interference with cockpit
communication
GUIDANCE/POLICY/EXPERIENCE
1. Speech
intelligibility is adequately assessed using single event noise measures such as
ALm, SIL or PSIL.
2. Activities where speech intelligibility is critical
include class room instruction, outdoor concerts and other leisure listening
endeavors.
3. Advisory information for speech intelligibility in aircraft
cockpit environment has been developed by the FAA.
4. Surveys of
annoyance to aircraft noise reflect to a large extent reactions to activity
interference very often associated with speech interference.
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6.1 INTRODUCTION
A major annoyance
associated with aircraft noise is interference with verbal communication. This
section discusses the various measures of speech intelligibility that have been
developed, explains how to assess speech intelligibility and outlines the
implications of speech interference for individuals on the ground and in the
cockpit of an aircraft.
6.2 MEASURES OF SPEECH
INTELLIGIBILITY
A number of noise metrics have evolved for assessing
the influence of noise on speech.
1. The Preferred Speech Interference
Level (PSIL) is defined as the arithmetic average of the sound pressure
levels in the 500 Hz, 1000 Hz and 2000 Hz octave bands.
2. The Speech
Interference Level (SIL) is defined as the arithmetic average of the sound
pressure levels at the 500, 1000, 2000 and 4000 Hz octave bands.
3.
The Articulation Index (AI) is a value, between zero and 1.0, which
describes the masking of speech by background noise; this value is found by
evaluating the signal to noise ratio in specific frequency bands. There are
different methods specified for different bandwidths, depending on the
resolution required. For example, a masking noise with a continuous spectrum can
be evaluated with fewer points than a spectrum punctuated by sharp spikes and
deep valleys. The AI can be adjusted upward through the use of visual cues.
Figure 6.1 reflects the relation between the calculated AI and the effective AI
for communications where the listener can see the lips and face of the talker.
The AI is the most sophisticated and most accurate technique developed to assess
speech
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5. A-Weighted Sound Level (AL), defined in Section 2.0, is found to correlate well with SIL and PSIL formostsounds associated with aviation.
6.3 ASSESSING SPEECH INTELLIGIBILITY
There are many ways to assess speech intelligibility using the methods discussed above. Various tables exist throughout speech interference
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literature which relate AI levels, SIL and PSIL to levels of speech
intelligibility.
Table 6.1 is one example of such a table; it relates speech interference
levels to levels of effective communication. Figure 6.3 provides the permissible
distance between a speaker and listeners for specified voice levels and ambient
noise levels, using AL (referred to in the table as dBA).
Another helpful
interpretive scheme has been developed by the U.S. Army, which has determined
through research and experience the levels of speech or sentence intelligibility
appropriate for various workspaces. Table 6.2 depicts
the relationship between NC values and speech quality.
6.4 SPEECH INTERFERENCE ON THE
GROUND
Speech interference associated with aircraft noise is a
primary source of annoyance to individuals on the ground. The disruption of
leisure activities such as listening to the radio, television, music and
conversation gives rise to frustration and irritation. Quality speech
communication is obviously also important in the classroom, office and
industrial settings. In one 1963 study, sponsored by the British government,
researchers found that aircraft noise of 75 dB annoyed the
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1. Peterson, Arnold P.G. Handbook of Noise Measurement.
GenRad, Inc., 1980.
2. U.S. Air Force. Design
Note 3F1. January 1974.
3. Great Britain Committee
on the Problem of Noise. Noise, Final Report. Presented to Parliament by
the Lord Minister for Science by Command of Her majesty. London, H. M.
Stationery Office, July 1963.
4. Industrial Audiology.
Cockpit Communication Interference. FAA Order Number DTAFAO1-82-81561;
July 1982.
5. FAA Advisory Circular Draft on Cockpit
Speech Interference.
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INTRODUCTION
This section describes the sleep process and
reviews research relating the percentage of an exposed population experiencing
awakening to noise level. Design criteria are also identified for avoiding
unacceptable rates of awakening.
AVIATION
APPLICATIONS/ISSUES
Sleep interference associated with aircraft
noise.
GUIDANCE/POLICY/EXPERIENCE
Sleep interference is one
of the factors contributing to aircraft noise annoyance. Airport nighttime
restrictions have been employed to minimize this annoyance. In the case of
nighttime operations an exterior maximum sound level (ALm) of 72 dB is
identified as an acceptable sleep interference threshold for windows closed
condition. This corresponds to an interior ALm of about 55 dB.
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7.3.1 Arousal from Sleep. The study revealed
that, while research has yielded widely varying conclusions as to what the
threshold of arousal from sleep is, the level of a noise which can interfere
with falling or waking from sleep ranges from 35 to 70 dB. The varied results of
researchers arise because several factors affect how easily a person will be
awakened from sleep. As mentioned above, a person's age is a prominent factor
affecting arousal. Children sleep the heaviest, the elderly the lightest, sleep.
Thus, older people have a much lower , arousal threshold than do younger
people.
As one might expect, there is also a rise in the threshold of
arousal as sleep stages deepen. The average difference in the arousal threshold
from being awake to stage 4 NREH sleep is about 17.5 dB. Lastly, because of the
cyclical nature of the two sleep stages (REM and NREM), an individual's
susceptibility to arousal varies throughout the night. However, in a normal
8-hour sleep night, more time is spent in lighter stages of sleep in the last
half than in the first half. This implies that airport use restrictions limiting
early morning flight from 3 a.m. to 7 a.m. are particularly important. Although
people are also susceptible to arousal at the beginning of a sleep period when
they are just trying to fall asleep, in general arousal is more likely during
the late hours of sleep.
7.3.2 Measuring Sleep
Interference. Some studies have shown generally that the single event energy
dose of a noise event (EPNL or SEL), and not the maximum level (in PNL or AL) is
a better predictor of sleep interference (Refs. 4, 5). These
findings have been contradicted in a report by 0hrstrom and Rylander, who assert
that peak levels should be used to determine tolerable night levels of noise (Ref. 6).
Researchers continue to debate this question.
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1. Kales A, and J. Kales. Evaluation and Treatment of
Insomnia. New York, Oxford University Press, 1984.
2. Griefahn, Barbara. Research on Noise-Disturbed Sleep Since
1973. In Proceedings of the Third International Congress on Noise as a
Public Health Problem. ASHA Report No. 10, April 1980.
3. Kryter, Karl. D., Analysis of Laboratory and Field Data on
Awakening from Noise.
4.Lukas, J., Measures of
Noise Level: Their Relative Accuracy in Predicting Objective and Subjective
Responses to Noise During Sleep. EPA-600/1-7-010, U.S. Environ. Protect.,
Agency. Feb. 1977.
5. Horonjeff, R., R. Bennett, and
S. ________, Sleep Interference BBN Rpt. 3710 Dec. 1978, Electric Bower
Research Institute, Inc., Palo Alto, CA 94302.
6.
0hrstrom, E., and R. Rylander, Sleep Disturbance Effects of Traffic Noise - A
Laboratory Study on After Effects, J. Sound and Vib. Vol. 84, 1982,
pp. 87-103.
7. LeVere, T. G. Morlock and F. Hart,
Waking performance decrements following minimal sleep description: The
effects of habituation during sleep, Physiological Psychology, Vol.
3, 1975, pp. 147-174.
8. Ando, Y. and H. Hatton,
Effects of Noise on Sleep of Babies, J. Acoust. Soc. Am. Vol. 62,
1977, pp. 199-204.
9. Reported in Kryter, K. D.,
Community Annoyance from Aircraft and Ground Vehicle Noise, J. Acoust.
Soc. Am. Vol. 72, 1982, pp. 1222-1242.
10. Wyle
Labs, Res. Staff. Study of Soundproofing Public Buildings Near Airports.
Ref. No. DOT-FAA-AEQ-77-9, April 1977.
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INTRODUCTION
This section summarizes a series of contemporary research
studies which hypothesize correlation between noise exposure in general (in many
cases aircraft noise exposure) and various human physiological or behavioral
effects. While some studies show a significant correlation, other studies show
none. Although research continues, there does not exist a succession of studies
which corroborate the "cause and effect" theory. While the reader should be
aware of research in this area, the topics reviewed in this section are
considered to be beyond the realm of normally accepted and recognized aircraft
noise effects.
AVIATION APPLICATION/ISSUES
1.
Cardiovascular effects
2. Achievement scores
3. Birth
weight
4. Mortality rates
5. Psychiatric
admissions
GUIDANCE/POLICY/EXPERIENCE
1. As cited above the
relationship between these suggested "effects" and aircraft noise has not been
repeatedly and consistently demonstrated. On the contrary, many studies directly
contradict those which show an effect.
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1. U.S. Environmental Protection Agency, "Information on
Levels of Environmental Noise Requisite to Protect Public Health and Welfare
with an Adequate Margin of Safety," EPA 550/9-74-004, March 1974.
2. People Against Nuclear Energy v. U.S. Nuclear Regulatory
Commission U.S. Court of Appeals for the District of Columbia, May 14,
1982.
3. Wesler, John F. Unpublished Information Paper
on the Effects of Noise. Federal Aviation Administration, AEE-120, Washington,
D.C., 1981.
4. Thompson, "Epidemiology Feasibility
Study: Effects of Noise on the Cardiovascular System," EPA Report 550/9-81-103,
September 1981.
5. Meecham & Shaw, "Effects of Jet
Noise on Mortality Rates," British Journal of Audiology, Vol. 13,
1979.
6. Frerichs, Beeman & Coulson, "Los Angeles
Airport Noise and Mortality - Faulty Analysis and Public Policy," American
Journal of Public Health, Vol. 70, No. 4, April 1980.
7. Jones & Tauscher, "Residence Under an Airport Landing
Pattern as a Factor in Teratism," Archives of Environmental Health, Vol. 33,
1978.
8. Edmonds, Layde & Erickson, "Airport Noise and
Teratogenesis," Archives of Environmental Health, Vol. 34, pp. 243-247,
1979.
9. Meecham & Smith, "Effect of Jet Aircraft
Noise on Mental Hospital Admissions," British Journal of Audiology, Vol. ii, pp.
81-85, 1977.
10. Gattoni & Tarnopolsky, "Aircraft
Noise and Psychiatric Morbidity," Psychological Medicine, Vol. 3, pp. 516-520,
1973.
11. Knipschild, "V. Medical Effects of Aircraft
Noise: Community Cardiovascular Survey," International Archives of 0ccupational
and Environmental Health, Vol. 40, 1977.
12.
Knipschild, "VI. Medical Effects of Aircraft Noise: General Study,"
International Archives of 0ccupational and Environmental Health, Vol. 40,
1977.
13. Knipschild, "VII. Medical Effects of
Aircraft Noise: Drug Survey," International Archives of Occupational and
Environmental Health, Vol. 40, 1977.
14. Knipschild,
"VIII. Medical Effects of Aircraft Noise: Review and Literature," International
Archives of Occupational and Environmental Health, Vol. 40, 1977.
15. Charles Frances Davison et. al. v. Department of Defense
et. al., U.S. District Court for Southern District of Ohio, May 1982.
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INTRODUCTION
This section summarizes research concerning the
effects of aviation noise on wild mammals, birds and fish, on farm animals
(swine, cattle, poultry and mink), and on a variety of laboratory animals. While
a significant amount of research has been conducted on the reactions of animals
to noise, it has proven difficult to draw any general conclusions on the subject
because there is much variability in response both between and within species.
Thus, no clear policies or guidelines have been developed concerning noise
exposure and animals.
AVIATION APPLICATION/ISSUES
1. Harm
to animals in U.S, wildlife refuges, national parks, and wilderness
areas
2. Effects on the productivity of domestic
animals
GUIDANCE/POLICY/EXPERIENCE
Animals are rarely
exposed to high noise levels outside of the laboratory, and most have proven
impervious to the aircraft noise they do experience. Nevertheless, a few species
have demonstrated little tolerance of aircraft noise and have shown few signs of
adapting to it. Since no well-established guidelines concerning noise and
animals exist, it is important to remain aware of the issue and alert to the
possibility that "off-limits" wildlife areas may be desirable in the future for
selected wildlife areas.
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A 1963 study found that pigs exposed to recorded jet and propeller aircraft
sounds of 120 to 135 dB daily from 6 a.m. to 6 p.m. from weaning time or before,
until slaughter at 200 pounds body weight, showed no differences in feeding or
weight gain from pigs unexposed to the sounds (Ref.
5).
Another study also reported that dairy cattle showed no
differences in milk production when exposed to aircraft noise. The researchers
compared milk cow herds located within three miles of a number of air force
bases using jet aircraft (13 percent of the herds were within 1 mile of the end
of an active runway). Dairy cattle studied in the vicinity of Edwards Air Force
Base (California) showed few abnormal behavioral reactions due to sonic booms,
though they had been exposed to the booms for several years and so may have
become habituated (Ref. 6). Other
studies also supported this evidence that cattle are generally not affected by
the sonic boom or other aircraft noise.
Poultry have shown no more
reaction to aircraft noise than swine or cattle. In a 1958 study, recorded
aircraft flyover noise at 80 to 115 dB at 300 to 600 Hz was played daily and
every third night from the beginning of the hens brooding until the chicks were
9 weeks old. There resulted no difference in weight gain, feeding efficiency,
meat tenderness or yield, or mortality between sound-exposed and non-exposed
chicks (Ref. 7).
Broad breasted bronze turkeys were exposed to recordings of low flying jet
planes at l10 to 135 dB for 4 minutes during the third day of brooding. The
turkeys typically ceased brooding but resumed it shortly, with no decrease in
egg laying (Ref.
8). A final study showed that chicken eggs exposed to daily sonic booms for
21days during their incubation hatched normally (Ref. 9).
In
a 1968 study on mink, one hundred twenty animals were exposed to simulated sonic
booms ranging from 2.0 to 0.5 lb per sq ft. The litters of mink exposed to the
booms were larger than those of mink not exposed. No racing, squealing or other
signs of panic were observed in the animals. Animals that died naturally were
examined; no disorders which could be traced to the sonic booms were found (Ref. 10). Female
mink showed little or no response to exposure to sonic boom during breeding,
birth of kits, or whelping. Again, no signs of panic were observed.
9.4 LABORATORY ANIMALS
Mice, rats, monkeys, and
rabbits have been examined in numerous studies, the results of which are briefly
reviewed here (Ref.
11). The studies generally exposed the test animals to a certain level of
noise for a predetermined period of time; response was measured in terms of
physiological change. Increases and decreases in body chemicals and in the
weights of body organs were typically observed in the tests. Although some of
the bodily changes were typical of reactions to stress (and noise is often
considered stressful), it was not clear that the changes were significant or
dangerous. As with humans, hearing damage occurred when the animals were exposed
to high level noise; however, animals are rarely exposed to extreme aircraft
noise.
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1. Edwards, Richard G., Alvin B. Broderson, Roger W.
Barbour et al. Assessment of the Environmental Compatibility of Differing
Helicopter Noise Certification Standards. U.S. Department of Transportation,
FAA, June 1979.
2. International Civil Aviation
0rganization, Sonic Boom Committee. Report. . First meeting, Montreal, ICAO Doc.
9011, SBC/1, May 1972.
3. International Civil Aviation
0rganization, Sonic Boom Committee. Report. Second meeting, Montreal, ICAO Doc.
9064, SBC/2, June 1973.
4. U.S. Department of
Transportation, FAA. Concorde Supersonic Transport Aircraft: Final
Environmental Impact Statement. Vol. 1, September 1975.
5. Bond, J. C.F. Winchester, L.E. Campbell, and J.C. Webb.
Effects of Loud Sound on the Physiology and Behavior of Swine. U.S.
Department of Agriculture, Agricultural Research Service Technical Bulletin, No.
1280.
6. Parker, J.B, and N.D. Bayley.
Investigations on Effects of Aircraft Sound on Milk Production of Dairy
Cattle, 1957-1958. U.S. Department of Agriculture, Agricultural Research
Service, Animal Husbandry Research Division, 1960.
7.
Stadelman, W.J. The Effects of Sounds of Varying Intensity on Hatchability of
Chicken Eggs. Poultry Science, 37, 1958.
8.
Jeannoutot, D.W. and J.L. Adams. Progesterone Versus Treatment by High
Intensity Sound as Methods of Controlling Broodiness in Broad Breasted Bronze
Turkeys. Poultry Science, 40, 1961.
9.
Bell, W.B. Animal Response to Sonic Boom. Paper presented at the 80th
meeting of the Acoustical Society of America, Houston, November 1970.
10. Travis, H.F., G.V. Richardson, J.R. Menear, and J. Bond.
The Effects of Simulated Sonic Booms on Reproduction and Behavior of
Farm-Raised Mink. ARS 44-200, U.S. Department of Agriculture, Agricultural
Research Service, June 1968.
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INTRODUCTION
This section reviews the effects of strong low
frequency acoustical energy in creating some of the more unusual (albeit rare)
aircraft noise effects. The consideration of low frequency sound in creating
vibration (and secondary noise) in structures is discussed. While structural
vibration is not a common concern for commercial transport airplanes, there may
be some need to exercise caution in helicopter operations in close proximity to
buildings. A brief review is also provided addressing human physiological
reactions to intense low frequency sound as one might encounter near engine test
stands. Criteria are presented for both annoyance to vibration and human
physical damage risk for exposure to intense infrasound.
AVIATION
APPLICATIONS/ISSUES
1. Vibration of wall and windows
2.
Radiation of secondary noise
3. Human physiological response to intense
low frequency
sound
4. Sonic Booms (illegal in U.S, for civil
aircraft
operations)
GUIDANCE/POLICY/EXPERIENCE
The
issue of low frequency energy and its impact on buildings and people was
explored in detail in regard to the Concorde SST operations in the U.S. Impacts
were found to be negligible. Consequently low frequency effects from civil
commercial aircraft remains a minor issue in most environmental impact
assessments. There remains the need however to consider carefully possible
effects of low frequency energy in the operation of helicopters in close
proximity to buildings.
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worst case example, the Concorde supersonic transport creates sound pressure
levels at low frequencies (below 30 Hz) which are well below EPA sensation and
damage risk levels. All other commercial transport levels fall below those of
the Concorde, indicating no potential health effects associated with low
frequency noise from in-service commercial aircraft.
10.5.2 International Standards 0rganization (ISO).
Generally, human tolerance of vibration is lowest in the 4-8 Hz frequency
range, and this is the basis of limits proposed by the ISO Technical Committee
108 working Group. Human tolerance to vibration also depends on situational
factors; for example, the blurring of vision which is merely an annoyance to a
train passenger could impair safety and efficiency in the workplace. It is also
not known to what extent non-auditory sensations of noise are symptoms of
psychological stress.
10.6 SONIC BOOM
FAA flight rules require
civil aircraft to fly at subsonic speed over U.S. land areas in order to prevent
sonic booms from impacting the U.S. environment. For supersonic aircraft
approaching or leaving U.S. boundaries, flight rules stipulate that the aircraft
be operated in a manner that will not cause direct sonic shock waves to encroach
upon the U.S. (Ref. 6).
Sonic booms result when a projectile such as an
aircraft exceed the speed of sound. The phenomenon we call a boom is similar in
many ways to an explosion, characterized by a rapid increase in pressure above
the ambient pressure, followed by a negative pressure excursion. An example of
this N-wave signature is shown in Figure 10.3.
A great deal of research was conducted in the1950's and 1960's by the U.S. Air Force and prospective manufacturers of the an American SST. (The U.S. SST program was eventually cancelled). The relationships
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One of the most famous studies on the sonic boom was conducted in 1964 over
Oklahoma City (Ref.
8). Eight sonic booms a day at a median peak overpressure level of 1.2 psf
(57.46 pascals) were experienced by this community over a six-month period. Figure 10.4,
below, reveals the percentage of responding residents who reported adverse
reactions to the sonic booms. Based on this and many other studies, the U.S. EPA
has stated that "the peak overpressure of a sonic boom that occurs during the
day should be no more than 35.91 pascals (0.75 psf) if the population is not to
be annoyed or the general health and welfare adversely affected " (Ref. 9).
As
a matter of interest, a rather unusual phenomenon called secondary sonic booms
were observed shortly after the introduction of Concorde service to the U.S. In
essence, sonic shock waves from the Concorde were refracting off the
discontinuity at the top of the earth's atmosphere and bending back down to the
earth, l4hile the level of the overpressures was not high enough to cause any
damage, people did take notice. After a study of these "mystery booms" by the
FAA / DOT (Ref.
10), the Concorde pilots implemented changes in their operational procedures
to minimize the occurrences.
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10.7 CONCLUSION
As discussed in this
section, low frequency sound and its effects are relatively minor considerations
in assessing aircraft nose impact. The case of helicopter operations in close
proximity to buildings, however, remains an area warranting close scrutiny.
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1. Hershey, Robert L., Russ J. Kevala, and Sharon L.
Burns. Analysis of the Effect of Concorde Aircraft Noise on Historic
Structures. Rep. No. FAA-RD-75-118, July 1975.
2.
Wiggins, John H. The Influence of Concorde Noise on Structural
Vibrations. Rep. No. FAA-75-1241-1, July 1975.
3.
Schomer, Paul. The Role of Vibration and Rattle in Human Response to
Helicopter Noise. Unpublished Report, December 1986.
4. Douglas Aircraft Company, Long Beach CA. Sonic Boom
Modeling Investigation of Topographical and Atmospheric Effects. Final
Report, FAA-NO-70-l0, July 1970.
5. U.S.
Environmental Protection Agency, Office of Noise Abatement and Control,
Washington D.C. Information on Levels of Environmental Noise Requisite to
Protect Public Health and Welfare with an Adequate Margin of Safety. March
1976.
6. Code of Federal Regulations, FAR
91.55.
7. Federal Aviation Administration, Office of
Planning. Some Considerations of Sonic Boom. May 1961.
8. Borsky, P.N. Community Reactions to Sonic Booms in the
Oklahoma City Area. National Opinion Research Center, AHRL-TR-65-37,
1965.
9. U.S. Environmental Protection Agency.
Information on Levels of Environmental Noise Requisite to Protect Public
Health and Welfare with an Adequate Margin of Safety. 550/9-74-004, March
1976.
10. Rickley, Edward J, and Allan D. Pierce.
Detection and Assessment of Secondary Sonic Boom in New England.
FAA-AEE-80-22, May 1980.
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INTRODUCTION
Over the past 10 years, researchers in aviation
acoustics have suggested that penalties be assessed (dB increments added) for
sounds which possess impulsive characteristics. Helicopter blade slap which
accompanies certain modes of flight operation has been the primary subject of
this research. This section reviews the research. and, as elsewhere, finds
conflicting results. While some researchers find the need for an adjustment
others do not. Complex distinctions between detectability and annoyance are key
to the debate. In the end, the position adopted by the International Civil
Aviation Organization (ICAO) was that no correction is necessary.. Nonetheless,
the Helicopter Association International (HAT), and the FAA continue to conduct
research to minimize impulsive helicopter noise.
AVIATION
APPLICATION/ISSUES
The question is raised, in connection with
helicopter noise, whether or not an impulsivity correction is necessary to
properly assess human
reaction.
GUIDANCE/POLICY/EXPERIENCE
After years of
research, ICAO concluded that an impulsivity adjustment was unnecessary to
properly certificate aircraft; this, in effect, implies that human response is
adequately assessed without a special impulsivity adjustment to the EPNL metric.
Nonetheless efforts continue to reduce impulsive noise which dominates
helicopter noise in certain flight regimes.
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1. Wright, S.E, and A. Damongeot. Psychoacoustic
Studies of Impulsive Noise. Paper #55, Third European Rotorcraft Powered
Lift Aircraft Forum, Aeronautical and Astronautical Association of France,
September 1971.
2. Patterson, James, Ben T. Mizo,
Paul D. Schemer, Robert T, Camp. Subjective Ratings of Annoyance Produced by
Rotary-Wind Aircraft Noise. U.S. Army Aeromedical Research Laboratory,
Report No. 77-12. May 1977.
3. Powell, Clemans A.
A Subjective Field Study of Helicopter Blade-Slap Noise. NSA Technical
memorandum 78758, July 1978.
4. Loughborough
University of Technology. Studies of Helicopter Noise Perception: Background
Information Paper. ICAD Committee on Aircraft Noise, Working Group B,
December 1981.
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INTRODUCTION
The issue of whether noise occurring at different
times of the day should be assigned weighting factors to represent different
human sensitivity to noise intrusion has been a subject of much concern and
research over the past 35 years. This section briefly reviews the research and
practice. The metric selected by the FAA as the standard for use in airport
noise impact assessment uses a 10 dB nighttime weighting
factor.
AVIATION APPLICATON/ISSUES
1. Should aircraft noise
occurring in the evening or at nighttime be assigned a weighting penalty to
account for increased sensitivity to noise intrusions?
2. If a weighting
is appropriate, what is the value of the weighting
function?
GUIDANCE/POLICY/EXPERIENCE
The FAA has designated
the Yearly Average Day Night Sound Level as the metric for assessing airport
cumulative noise impact. This metric assigns a 10 dB weighting between the hours
of 10 p.m. and 7 a.m.
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Merits |
Deficiencies |
Accepted by all levels of |
Energy summation method Hides some value judgments Ignores time of week and Not known if the 10dB Not known if the time |
Various recommendations were offered by conference participants concerning
DNL. The representatives of several governmental agencies spoke in favor of
maintaining agreement between Federal agencies as to what metric to use; they
also stated a desire to have that metric be one that is applicable to all kinds
of noise, (i.e. traffic, background, aircraft) which DNL is. Other
recommendations from conference discussion groups and individuals included the
following:
1. Researchers were urged to reconsider changing lifestyles
and to reflect on whether 10 PM to 7 AM is the most sensitive portion of the
day. Evening or transition may be more important.
2. DNL should remain a
rough screening device. The DNL penalty, for example, could impact school
operations if a large number of operations were shifted to the day. The public
is urged to pursue local independent decisions on this matter.
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There is also the possibility that people's perception of and annoyance
with daytime noise affects their perception of nighttime noise, some researchers
feel that there may be more complaints about nighttime noise because people view
it as a more valid complaint than something like television disruption; thus,
the perspective on time-of-day may be skewed. One study suggested that daytime
activities, which usually involve communicating or concentrating tasks, might be
more sensitive to interruption than sleep.
The report stated that the one
point that researchers seem to agree on -- although again, empirical evidence is
scant -- is that the most annoying/disturbing times for noise to occur are when
a person is trying to go to sleep and when he is preparing to awaken. However,
bedtime
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1. Workshop Proceedings, NASA Langley Research Center.
Time of Day Corrections to Aircraft Noise Metrics. Rep. No. FAA-EE-80-3,
March 1980.
2. Fields, James M. Research on the
Effect of Noise at Different Times of Day: Models, Methods and Findings.
Unpublished Report, August 1984.
3. Pearson, K.
S. The Effects of Duration and Background Noise level on Perceived
Noisiness. FAA ADS-78, Federal Aviation Administration, April
1966.
4. Taylor S. M., F. L. Hall and S. E. Bernie.
?Effect of Background Levels on community Responses to Aircraft Noise,
J. Sound & Vib, Vol. 71, No. 2, July 22, 1980.
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INTRODUCTION
Noise contours or footprints are the accepted
technique for displaying airport cumulative noise exposure. Noise contours are
also employed in comparing the noise footprints of individual aircraft. Contours
can be developed for different noise indices, but airport contours generally
express DNL while individual aircraft contours usually portray either SEL, EPNL
or ALm.
AVIATION APPLICATION/ISSUES
1. Contours are
used as the tool to assess land use compatibility.
2. Contours are also
used to portray the noise exposure of single operations of various aircraft
types.
GUIDANCE/POLICY/EXPERIENCE
The noise contour
program developed by the FAA and approved for use in FAA funded airport land use
compatibility studies is the Integrated Noise Model or INM. This program can
also generate single event contours. A new microcomputer-based model which will
generate noise contours for helicopters is now under
development.
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INTRODUCTION
This section describes the development of criteria
linking cumulative airport noise exposure and compatible land use. Criteria are
presented which have been designated for use in FAA funded compatibility
studies.
AVIATION APPLICATION/ISSUES
1. FAR PART 150,
Airport Noise Compatibility Programs
2. Planning guidance for developers
and zoning officials.
3. Guidance for the granting of HUD and VA
mortgage
guarantees.
4. Airport master plans.
5. Environmental
Impact Assessments
GUIDANCE/POLICY/EXPERIENCE
The FAA
has published criteria in FAR PART 150 for use in compatibility studies. Other
similar criteria have been published by the Department of Defense, the Federal
Interagency Committee on Urban Noise, and the American National Standards
Institute (ANSI).
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Land Use |
|
|
Livestock Farming |
| |
General Manufacturing |
Marginally to 80 dB Incompatible above 80 dB |
Incompatible above 85 dB |
Music Shells |
|
|
Playground, Riding, Golf |
Marginally to 75 dB Incompatible above 75 dB |
Compatible with special details up to 80 dB |
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|
|
|
||||||
Residential, other than mobile homes and transient lodgings |
Y |
N(1) |
N(1) |
N |
N |
N |
Mobile home parks |
Y |
N |
N |
N |
N |
N |
Transient lodgings |
Y |
N(1) |
N |
N(1) |
NN |
N |
|
||||||
Schools |
Y |
N(1) |
N(1) |
N |
N |
N |
Hospitals and nursing homes |
Y |
N |
N |
N | ||
Churches, auditoriums, and concert halls |
Y |
N |
N |
N | ||
Governmental services |
Y |
Y |
N |
N | ||
Transportation |
Y |
Y |
Y(2) |
Y(3) |
Y(4) |
Y(4) |
Parking |
Y |
Y |
Y(2) |
Y(3) |
Y(4) |
N |
|
||||||
Offices, business and professional |
Y |
Y |
N |
N | ||
Wholesale & retail--building materials, hardware & farm equip. |
Y |
Y |
Y(2) |
Y(3) |
Y(4) |
N |
Retail trade--general |
Y |
Y |
N |
N | ||
Utilities |
Y |
Y |
Y(2) |
Y(3) |
Y(4) |
N |
Communication |
Y |
Y |
N |
N | ||
|
||||||
Manufacturing, general |
Y |
Y |
Y(2) |
Y(3) |
Y(4) |
N |
Photographic and optical |
Y |
Y |
N |
N | ||
Agriculture (except livestock) and forestry |
Y |
Y(6) |
Y(7) |
Y(8) |
Y(6) |
Y(8) |
Livestock farming and breeding |
Y |
Y(6) |
Y(7) |
N |
N |
N |
Mining and fishing, resource production and extraction |
Y |
Y |
Y |
Y |
Y |
Y |
|
||||||
Outdoor sports and spectator sports |
Y |
Y(5) |
Y(5) |
N |
N |
N |
Outdoor music shells, amphitheaters |
Y |
N |
N |
N |
N |
N |
Nature exhibits and zoos |
Y |
Y |
N |
N |
N |
N |
Amusements, parks, resorts, and camps |
Y |
Y |
Y |
N |
N |
N |
Golf courses, riding stables and water recreation |
Y |
Y |
N |
N |
Numbers in parentheses refer to notes.
*The designations contained in this table do not constitute Federal
determination that any use of land covered by the program is acceptable or
unacceptable under Federal, State or local law. The responsibility for
determining the acceptable and permissible land uses and the relationship
between specific properties and specific noise contours rests with the local
authorities. FAA determinations under Part 150 are not intended to substitute
federally determined land uses for those determined to be appropriate by local
authorities in response to locally determined needs and values in achieving
compatible land uses.
NOTES FOR TABLE 1
(1) Where the community determines that residential or school uses must be allowed, measures to achieve outdoor to indoor Noise Level Reduction (NLR) of at least 25 dB and 30 dB should be incorporated into building codes and be considered in individual approvals. Normal residential construction can be expected to provide a NLR of 20 dB, thus, the reduction requirements are often stated as 5, 10, or 15 dB over standard construction and normally assume mechanical ventilation and closed windows year round. However, the use of NLR criteria will not eliminate outdoor noise problems.
(2) Measures to achieve NLR 25 dB must be incorporated into the
design and construction of portions of these buildings where the public is
received, office areas, noise sensitive areas or where the normal noise level is
low.
(3) Measures to achieve NLR of 30 dB must be incorporated
into the design and construction of portions of these buildings where the public
is received, office areas, noise sensitive areas or where the normal noise level
is low.
(4) Measures to achieve NLR of 35 dB must be
incorporated into the design and construction of portions of these buildings
where the public is received, office areas, noise sensitive areas or where the
normal noise level is low.
(5) Land use compatible provided
special sound reinforcement systems are installed.
(6)
Residential buildings require an NLR of 25.
(7) Residential
buildings require an NLR of 30.
(8) Residential buildings not
permitted.
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NOISE ZONE |
|
RESPONSE | |
|
|
Zone of highest intensity; frequency and intensity of noise is such as to be loud and annoying.(Inhabitants may complain repeatedly and even form groups to protest.) | |
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Second most intensive zone; noise is more moderate in character. (Inhabitants may complain vigorously and concerted group action is a possibility.) | |
|
|
Lowest noise level zone; the noise may, however, interfere occasionally with certain activities of the residents. |
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1. American National Standard. Sound Level Description
for Determination of Compatible Land Use. Rep. No. ANSI S3.23-1980,
1980.
2. FAA Code of Federal Regulations, Part
150.
3. Federal interagency Committee on Urban Noise.
Guidelines for Considering Noise in Land Use Planning and Control. June
1980.
4. U.S. Air Force. Manual 19-10. Planning in
the Noise Environment. Chapter 4.
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INTRODUCTION
This section reviews research conducted to assess
the effect of aircraft noise on real estate values. While an effect is observed
it is considered an influence which is often offset by the advantages associated
with ready access to the airport and employment
opportunities.
AVIATION APPLICATION/ISSUES
The effect of
aircraft noise on real estate values is a topic often associated with
environmental
assessments.
GUIDIANCE/POLICY/EXPERIENCE
Studies indicate
that a one decibel change in cumulative airport noise exposure (in DNL) usually
results in a 0.5 to 2% decrease in real estate values.
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Study Area (Year, mean property value) |
Range of Noise Levels (DNL) |
Best NDI-NEF Estimate* (Percent) |
Los Angeles (1960, $19,772) Dallas (1960, $18,011) All Areas (1960, $18,074) Minneapolis (1967, $19,683) San Francisco (1970, $27,600) San Jose (1970, $21,000) Boston (1970, $13,000) Toronto (1969-1973, $30,000-35,000) Dallas (1970, $22,000) Washington, D.C. (1970, $32,724) |
55 - 75 55 - 75 55 - 75 55 - 85 60 - 80 60 - 80 60 - 80 55 - 70 55 - 90 55 - 70 |
1.8 2.3 2.0 0.6 1.5 0.7 0.6 0.9 0.6 1.0 |
*The NDI-NEF is the percentage decrease in a given property value per unit
increase in the DNL
Nelson found that the studies can be divided into
two groups and some conclusions drawn. The first group of estimates in the table
was based on 1960 data (and included New York, Los Angeles and Dallas) and
suggests a range of 1.8 to 2.3 percent decrease in value per decibel (DNL). The
second group of estimates, covering the period from1967 to 1970, suggests a mean
of 0.8 percent devaluation per decibel change in DNL. Nelson then excludes the
San Francisco data (which was influenced by unique climatic and political
differences) and finds a mean of 0.7 percent devaluation per decibel change in
DNL.
Nelson also notes that there seems to be a decline in the noise
depreciation index over time, from 1960-1970. This could be due either to noise
sensitive people being replaced by those less bothered by noise, or to the
enhanced commercial value of land near airports. Evidence exists to support
either of these hypotheses (Ref.
2).
15.4 CONCLUSION
The bottom
line is that noise has been shown to decrease the value of property by only a
small amount -- approximately 1% decrease per decibel (DNL). At a minimum, the
depreciation of a home due to aircraft noise is equal to the cost of moving to a
new residence. Because there are many other factors that affect the price and
desirability of a residence, the annoyance of aircraft noise remains just one of
the considerations that affect the market value of a home.
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1. Nelson, Jon P. Economic Analysis of Transportation
Noise Abatement. Ballenger Publishing Company: Cambridge, Massachusetts,
1978.
2. Crowley, R. W. A Case Study of the
Effects on an Airport on Land Values. Journal of Transport Economics and
Policy, Vol. 7, May, 1978.
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