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时间:2010-07-17 21:54来源:蓝天飞行翻译 作者:admin
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

Part IV. ASSESSMENT OF AIRPORT 5. Reporting of data to the certificating
N O I S E . . . . . . . ............................. IV-1 authority. . . . . . . . . . . . . . . . . . . . . . . . .
6. Nomenclature: symbols and units. . . . .
Part V. BALANCED APPROACH TO NOISE 7. Sound attenuation in air . . . . . . . . . . . .
M A N A G E M E N T . . . . . . . . . . . . . . . . . . . . . . . . . . . V-1 8. Adjustment of helicopter flight
test results . . . . . . . . . . . . . . . . . . . . . . .
9. Adjustment of aeroplane flight
test results . . . . . . . . . . . . . . . . . . . . .
APPENDICES
APPENDIX 3. Noise evaluation method
APPENDIX I. Evaluation method for noise for noise certification of propcller-driven
certification of subsonic jet aeroplanes - aeroplanes not exceeding 8 6 18 kg -
application for certificate of airworthiness application for certificate of airworthiness
for the prototype accepted for the prototype accepted before
before 6 October 1977. . . . . . . . . . . . . . . . . . . . . . APP 1-1 17 November 1988. . . . . . . . . . . . . . . . . . . . . . . .
1. Introduction. . . . . . . . . . . . . . . . . . . . . . . APP 1-1
2. Noise certification test and
measurement conditions . . . . . . . . . . . . . APP 1-1
3. Measurement of aeroplane noise
received on the ground. . . . . . . . . . . . . . APP 1-3
4. Calculation of effective perceived
noise level from measured
noise data . . . . . . . . . . . . . . . . . . . . . . . . APP 1-4
1. Introduction . . . . . . . . . . . . . . . . . . . . . .
2. Noise certification test and
measurement conditions . . . . . . . . . . . .
3. Measurement of aeroplane noise
received on the ground . . . . . . . . . . . . .
4. Reporting of data to the certificalitig
authority and correction of measured
data . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
APP 2- 1
APP 2-1
APP 2-3
APP 2-9
APP 2-15
APP 2-16
APP 2-19
APP 2-19
APP 2-25
APP 3-1
APP 3-1
APP 3-1
APP 3-1
APP 3-2
Table of Contents Annex 16 - Environmental Protection
Page Page
APPENDIX 4. Evaluation method for noise
certification of helicopters not exceeding
3 175 kg maximum certificated take-off mass . . .
6. Reporting of data to the certificating
authority and validity of results . . . . . . APP 6-5
APP 4- 1
1. Introduction. . . . . . . . . . . . . . . . . . . . . . .
2. Noise certification test and
measurement conditions . . . . . . . . . . . . .
3. Noise unit definition. . . . . . . . . . . . . . . .
4. Measurement of helicopter noise
received on the ground. . . . . . . . . . . . . .
5. Adjustment to test results. . . . . . . . . . . .
6. Reporting of data to the certificating
authority and validity of results. ......
APP 4-1 ATTACHMENTS
ATTACHMENT A. Equations for the
calculation of noise levels as a function
of take-off mass . . . . . . . . . . . . . . . . . . . . . . .
APP 4- 1
APP 4-2
ATT A- 1
ATT B-1
APP 4-2
APP 4-3 ATTACHMENT B. Guidelines for noise
certification of propeller-driven
APP 4-4 STOL aeroplanes . . . . . . . . . . . . . . . . . . . . . . . . .
ATTACHMENT C. Guidelines for noise
certification of installed auxiliary power
units (MU) and associated aircraft systems
during ground operation. . . . . . . . . . . . . . . . . . . .
APPENDIX 5. Monitoring aircraft noise on
and in the vicinity of aerodromes. . . . . . . . . . . . . APP 5-1
1. Introduction . . . . . . . . . . . . . . . . . . . . . . . ATT C-1
2. Definition . . . . . . . . . . . . . . . . . . . . . . . .
3. Measurement equipment. ............
4. Field equipment installation. . . . . . . . . .
APP 5-1
APP 5-1
APP 5-1
APP 5-3
ATTACHMENT D. Guidelines for evaluating
an alternative method of measuring helicopter
noise during approach . . . . . . . . . . . . . . . . . . . . . ATT D-1
APPENDIX 6. Noise evaluation method for
noise certification of propeller-driven
ATTACHMENT E. Applicability of Annex 16
noise certification Standards
aeroplanes not exceeding 8 6 18 kg - for propeller-driven aeroplanes . . . . . . . . . . . . . .
application for certificate of airworthiness
ATT E-1
A T F-1
for the prototype accepted on or
after 1 7 November 1988 .................... ATTACHMENT F. Guidelines for noise
APP 6-1 certification of tilt-rotor aircraft. . . . . . . . . . . . . .
I. Introduction.. .....................
2. Noise certification test and
measurement conditions. . . . . . . . . . . . .
3. Noise unit definition. ...............
4. Measurement of aeroplane noise
 
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