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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

application for certificate of airworthiness
for the prototype accepted on or after
17 November 1988 and before
1 January2006 . . . . . . . . . . . . . . . . . . . . . . . . . . .
CHAPTER 7. Propeller-driven STOL aeroplanes .
CHAPTER 8. Helicopters ................
3.1 Applicability. . . . . . . . . . . . . . . . . . . . . . . . 8.1 Applicability . . . . . . . . . . . . . . . . . . . . . . . .
3.2 Noise measurements. . . . . . . . . . . . . . . . . .
3.3 Noise measurement points . . . . . . . . . . . . .
3.4 Maximum noise levels . . . . . . . . . . . . . . . .
3.5 Trade-offs . . . . . . . . . . . . . . . . . . . . . . . . . .
8.2 Noise evaluation measure. . . . . . . . . . . . . .
8.3 Reference noise measurement points . . . . .
8.4 Maximum noise levels . . . . . . . . . . . . . . . .
8.5 Trade-offs. . . . . . . . . . . . . . . . . . . . . . . . . . .
3.6 Noise certification reference procedures . .
3.7 Test procedures. . . . . . . . . . . . . . . . . . . . . . 8.6 Noise certification reference procedures . .
8.7 Test procedures . . . . . . . . . . . . . . . . . . . . . .
CHAPTER 4.
1. Subsonic jet aeroplanes - application for
certificate of airworthiness for the prototype
accepted on or after 1 January 2006
2. Propeller-driven aeroplanes over 8 618 kg -
application for certificate of airworthiness
for the prototype accepted on or after
1 January20 06 . . . . . . . . . . . . . . . . . . . . . . . . .
CHAPTER 9. Installed auxiliary power units
(APU) and associated aircraft systems during ground
operations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11-9-1
CHAPTER 10. Propeller-driven aeroplanes not
exceeding 8 618 kg - application for certificate
of airworthiness for the prototype or derived
11-4- 1 version accepted on or after 1 7 November 1 988 . . . 11- 10- I
ANNEX 16 - VOLUME I (iii) 24/11/05
Annex I6 - Environmenfal Protection Volume I
10.1 Applicability. . . . . . . . . . . . . . . . . . . . . . . .
10.2 Noise evaluation measure. . . . . . . . . . . . . .
10.3 Reference noise measurement points. ....
10.4 Maximum noise levels . . . . . . . . . . . . . . . .
10.5 Noise certification reference procedures . .
10.6 Test procedures. . . . . . . . . . . . . . . . . . . . . .
CHAPTER 11. Helicopters not exceeding
3 175 kg maximum certificated take-off mass. . . . .
11.1 Applicability . . . . . . . . . . . . . . . . . . . . . . . .
1 1.2 Noise evaluation measure. . . . . . . . . . . . . .
11.3 Reference noise measurement point . . . . .
11.4 Maximum noise level. . . . . . . . . . . . . . . . .
11.5 Noise certification reference procedure. ..
1 1.6 Test procedures. . . . . . . . . . . . . . . . . . . . . .
CHAPTER 12. Supersonic aeroplanes . . . . . . . . .
Page Page
5. Reporting of data to the certificating
authority and correcting
measured data . . . . . . . . . . . . . . . . . . . . APP 1- 12
6. Nomenclature. . . . . . . . . . . . . . . . . . . . . APP 1-14
7. Mathematical formulation of
noy tables. . . . . . . . . . . . . . . . . . . . . . . . APP 1-17
8. Sound attenuation in air . . . . . . . . . . . . APP 1-18
9. Detailed correction procedures . . . . . . . APP 1-26
APPENDIX 2. Evaluation method for
noise certification of:
1. Subsonic jet aeroplanes - application for
certificate of airworthiness for the prototype
accepted on or after 6 October 1977
2. Propellerdriven aeroplanes over 5 700 kg -
application for certificate of airworthiness
f& the prototype accepted on or after
11-12-1 1 January 1985 and before 17 November 1988
3. Propeller-driven aeroplanes over 8 618 kg -
12.1 Supersonic aeroplanes - application for application for certificate of airworthiness
certificate of airworthiness for the for the prototype accepted on or after
prototype accepted before 17 November 1988
1 January 1975 . . . . . . . . . . . . . . . . . . . . . . 11-12-1 4. Helicopters . . . . . . . . . . . . . . . . . . . . . . . . . . . APP 2-1
12.2 Supersonic aeroplanes - application for
certificate of airworthiness for
prototype accepted on or after
1 January 1975 . . . . . . . . . . . .
the
1. Introduction . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . 11-12-1 2. Noise certification test and
measurement conditions . . . . . . . . . . . .
CHAPTER 13. Tilt-rotor aircraft . . . . . . . . . . . . . 11-13-1 3. Measurement of aircraft noise
received on the mound . . . . . . . . . . . . .
Part 111. NOISE MEASUREMENT FOR 4. Calculation of effective perceived
MONITORING PURPOSES ..... .:. ......... 111-1 noise level from measured
noise data. . . . . . . . . . . . . . . . . . . . . . . .
 
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