FAA 14 CFR PART 36-2011 NOISE STANDARDS AIRCRAFT TYPE AND AIRWORTHINESS CERTIFICATION《噪音标准 飞机机型和适航性证明》.pdf

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1、900 14 CFR Ch. I (1111 Edition) Pt. 36 section is FAA approved and specifies main-tenance required under 43.16 and 91.403 of the Federal Aviation Regulations unless an alternative program has been FAA ap-proved. Amdt. 355, 45 FR 60182, Sept. 11, 1980, as amended by Amdt. 356, 54 FR 34330, Aug. 18, 1

2、989 PART 36NOISE STANDARDS: AIR-CRAFT TYPE AND AIRWORTHI-NESS CERTIFICATION Subpart AGeneral Sec. 36.1 Applicability and definitions. 36.2 Requirements as of date of application. 36.3 Compatibility with airworthiness re-quirements. 36.5 Limitation of part. 36.6 Incorporations by reference. 36.7 Acou

3、stical change: Transport category large airplanes and jet airplanes. 36.9 Acoustical change: Propeller-driven small airplanes and propeller-driven commuter category airplanes. 36.11 Acoustical change: Helicopters. Subpart BTransport Category Large Airplanes and Jet Airplanes 36.101 Noise measurement

4、 and evaluation. 36.103 Noise limits. 36.105 Flight Manual Statement of Chapter 4 equivalency. Subpart C Reserved Subpart DNoise Limits for Supersonic Transport Category Airplanes 36.301 Noise limits: Concorde. Subpart E Reserved Subpart FPropeller Driven Small Airplanes and Propeller-Driven, Commut

5、er Cat-egory Airplanes 36.501 Noise limits. Subpart G Reserved Subpart HHelicopters 36.801 Noise measurement. 36.803 Noise evaluation and calculation. 36.805 Noise limits. Subparts IN Reserved Subpart ODocumentation, Operating Limitations and Information 36.1501 Procedures, noise levels and other in

6、formation. 36.1581 Manuals, markings, and placards. 36.1583 Noncomplying agricultural and fire fighting airplanes. APPENDIX A TO PART 36AIRCRAFT NOISE MEASUREMENT AND EVALUATION UNDER 36.101 APPENDIX B TO PART 36NOISE LEVELS FOR TRANSPORT CATEGORY AND JET AIR-PLANES UNDER 36.103 APPENDIXES CE TO PAR

7、T 36 RESERVED APPENDIX F TO PART 36FLYOVER NOISE RE-QUIREMENTS FOR PROPELLER-DRIVEN SMALL AIRPLANE AND PROPELLER-DRIVEN, COMMUTER CATEGORY AIRPLANE CERTIFI-CATION TESTS PRIOR TO DECEMBER 22, 1988 APPENDIX G TO PART 36TAKEOFF NOISE RE-QUIREMENTS FOR PROPELLER-DRIVEN SMALL AIRPLANE AND PROPELLER-DRIVE

8、N, COMMUTER CATEGORY AIRPLANE CERTIFI-CATION TESTS ON OR AFTER DECEMBER 22, 1988 APPENDIX H TO PART 36NOISE REQUIRE-MENTS FOR HELICOPTERS UNDER SUBPART H APPENDIX I TO PART 36 RESERVED APPENDIX J TO PART 36ALTERNATIVE NOISE CERTIFICATION PROCEDURE FOR HELI-COPTERS UNDER SUBPART H HAVING A MAXIMUM CE

9、RTIFICATED TAKEOFF WEIGHT OF NOT MORE THAN 7,000 POUNDS AUTHORITY: 42 U.S.C. 4321 et seq.; 49 U.S.C. 106(g), 40113, 4470144702, 44704, 44715; sec. 305, Pub. L. 96193, 94 Stat. 50, 57; E.O. 11514, 35 FR 4247, 3 CFR, 19661970 Comp., p. 902. SOURCE: Docket No. 9337, 34 FR 18364, Nov. 18, 1969, unless o

10、therwise noted. Subpart AGeneral 36.1 Applicability and definitions. (a) This part prescribes noise stand-ards for the issue of the following cer-tificates: (1) Type certificates, and changes to those certificates, and standard air-worthiness certificates, for subsonic transport category large airpl

11、anes, and for subsonic jet airplanes regardless of category. (2) Type certificates and changes to those certificates, standard airworthi-ness certificates, and restricted cat-egory airworthiness certificates, for propeller-driven, small airplanes, and for propeller-driven, commuter cat-egory airplan

12、es except those airplanes VerDate Mar2010 14:10 Mar 01, 2011 Jkt 223043 PO 00000 Frm 00910 Fmt 8010 Sfmt 8010 Y:SGML223043.XXX 223043wwoods2 on DSK1DXX6B1PROD with CFRProvided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-901 Federal Aviation Administration

13、, DOT 36.1 that are designed for agricultural air-craft operations (as defined in 137.3 of this chapter, as effective on January 1, 1966) or for dispersing fire fighting ma-terials to which 36.1583 of this part does not apply. (3) A type certificate and changes to that certificate, and standard air-

14、worthiness certificates, for Concorde airplanes. (4) Type certificates, and changes to those certificates, for helicopters ex-cept those helicopters that are des-ignated exclusively for argicultural aircraft operations (as defined in 137.3 of this chapter, as effective on January 1, 1966), for dispe

15、nsing fire fighting materials, or for carrying ex-ternal loads (as defined in 133.1(b) of this chapter, as effective on December 20, 1976). (b) Each person who applies under Part 21 of this chapter for a type of air-worthiness certificate specified in this part must show compliance with the applicab

16、le requirements of this part, in addition to the applicable airworthi-ness requirements of this chapter. (c) Each person who applies under Part 21 of this chapter for approval of an acoustical change described in 21.93(b) of this chapter must show that the aircraft complies with the applica-ble prov

17、isions of 36.7, 36.9, or 36.11 of this part in addition to the applicable airworthiness requirements of this chapter. (d) Each person who applies for the original issue of a standard airworthi-ness certificate for a transport cat-egory large airplane or for a jet air-plane under 21.183 must, regardl

18、ess of date of application, show compliance with the following provisions of this part (including appendix B): (1) The provisions of this part in ef-fect on December 1, 1969, for subsonic airplanes that have not had any flight time before (i) December 1, 1973, for airplanes with maximum weights grea

19、ter than 75,000 pounds, except for airplanes that are powered by Pratt (ii) December 31, 1974, for airplanes with maximum weights greater than 75,000 pounds and that are powered by Pratt and (iii) December 31, 1974, for airplanes with maximum weights of 75,000 pounds and less. (2) The provisions of

20、this part in ef-fect on October 13, 1977, including the stage 2 noise limits, for Concorde air-planes that have not had flight time before January 1, 1980. (e) Each person who applies for the original issue of a standard airworthi-ness certificate under 21.183, or for the original issue of a restric

21、ted category airworthiness certificate under 21.185, for propeller-driven, commuter cat-egory airplanes for a propeller driven small airplane that has not had any flight time before January 1, 1980, must show compliance with the applicable provisions of this part. (f) For the purpose of showing com-

22、pliance with this part for transport category large airplanes and jet air-planes regardless of category, the fol-lowing terms have the following mean-ings: (1) A Stage 1 noise level means a flyover, lateral or approach noise level greater than the Stage 2 noise limits prescribed in section B36.5(b)

23、of appen-dix B of this part. (2) A Stage 1 airplane means an air-plane that has not been shown under this part to comply with the flyover, lateral, and approach noise levels re-quired for Stage 2 or Stage 3 airplanes. (3) A Stage 2 noise level means a noise level at or below the Stage 2 noise limits

24、 prescribed in section B36.5(b) of appendix B of this part but higher than the Stage 3 noise limits prescribed in section B36.5(c) of appen-dix B of this part. (4) A Stage 2 airplane means an air-plane that has been shown under this part to comply with Stage 2 noise lev-els prescribed in section B36

25、.5(b) of ap-pendix B of this part (including use of the applicable tradeoff provisions spec-ified in section B36.6) and that does not comply with the requirements for a Stage 3 airplane. (5) A Stage 3 noise level means a noise level at or below the Stage 3 noise limits prescribed in section B36.5(c)

26、 of appendix B of this part. (6) A Stage 3 airplane means an air-plane that has been shown under this VerDate Mar2010 14:10 Mar 01, 2011 Jkt 223043 PO 00000 Frm 00911 Fmt 8010 Sfmt 8010 Y:SGML223043.XXX 223043wwoods2 on DSK1DXX6B1PROD with CFRProvided by IHSNot for ResaleNo reproduction or networkin

27、g permitted without license from IHS-,-,-902 14 CFR Ch. I (1111 Edition) 36.2 part to comply with Stage 3 noise lev-els prescribed in section B36.5(c) of ap-pendix B of this part (including use of the applicable tradeoff provisions spec-ified in section B36.6). (7) A subsonic airplane means an airpl

28、ane for which the maximum oper-ating limit speed, Mmo, does not exceed a Mach number of 1. (8) A supersonic airplane means an airplane for which the maximum oper-ating limit speed, Mmo, exceeds a Mach number of 1. (9) A Stage 4 noise level means a noise level at or below the Stage 4 noise limit pres

29、cribed in section B36.5(d) of appendix B of this part. (10) A Stage 4 airplane means an airplane that has been shown under this part not to exceed the Stage 4 noise limit prescribed in section B36.5(d) of appendix B of this part. (11) A Chapter 4 noise level means a noise level at or below the maxim

30、um noise level prescribed in Chapter 4, Paragraph 4.4, Maximum Noise Levels, of the International Civil Aviation Or-ganization (ICAO) Annex 16, Volume I, Amendment 7, effective March 21, 2002. Incorporated by reference, see 36.6. (g) For the purpose of showing com-pliance with this part for transpor

31、t category large airplanes and jet air-planes regardless of category, each air-plane may not be identified as com-plying with more than one stage or configuration simultaneously. (h) For the purpose of showing com-pliance with this part, for helicopters in the primary, normal, transport, and restric

32、ted categories, the following terms have the specified meanings: (1) Stage 1 noise level means a takeoff, flyover, or approach noise level greater than the Stage 2 noise limits pre-scribed in section H36.305 of appendix H of this part, or a flyover noise level greater than the Stage 2 noise limits p

33、rescribed in section J36.305 of appen-dix J of this part. (2) Stage 1 helicopter means a heli-copter that has not been shown under this part to comply with the takeoff, flyover, and approach noise levels re-quired for Stage 2 helicopters as pre-scribed in section H36.305 of appendix H of this part,

34、or a helicopter that has not been shown under this part to com-ply with the flyover noise level re-quired for Stage 2 helicopters as pre-scribed in section J36.305 of appendix J of this part. (3) Stage 2 noise level means a takeoff, flyover, or approach noise level at or below the Stage 2 noise limi

35、ts pre-scribed in section H36.305 of appendix H of this part, or a flyover noise level at or below the Stage 2 limit prescribed in section J36.305 of appendix J of this part. (4) Stage 2 helicopter means a heli-copter that has been shown under this part to comply with Stage 2 noise lim-its (includin

36、g applicable tradeoffs) pre-scribed in section H36.305 of appendix H of this part, or a helicopter that has been shown under this part to comply with the Stage 2 noise limit prescribed in section J36.305 of appendix J of this part. (5) Maximum normal operating RPM means the highest rotor speed cor-r

37、esponding to the airworthiness limit imposed by the manufacturer and ap-proved by the FAA. Where a tolerance on the highest rotor speed is specified, the maximum normal operating rotor speed is the highest rotor speed for which that tolerance is given. If the rotor speed is automatically linked with

38、 flight condition, the maximum normal operating rotor speed cor-responding with that flight condition must be used during the noise certifi-cation procedure. If rotor speed can be changed by pilot action, the highest normal operating rotor speed specified in the flight manual limitation section for

39、power-on conditions must be used during the noise certification proce-dure. Doc. No. 13243, Amdt. 364, 40 FR 1034, Jan. 6, 1975 EDITORIAL NOTE: For FEDERAL REGISTER ci-tations affecting 36.1, see the List of CFR Sections Affected, which appears in the Finding Aids section of the printed volume and a

40、t www.fdsys.gov. 36.2 Requirements as of date of ap-plication. (a) Section 21.17 of this chapter not-withstanding, each person who applies for a type certificate for an aircraft covered by this part, must show that the aircraft meets the applicable re-quirements of this part that are effec-tive on t

41、he date of application for that VerDate Mar2010 14:10 Mar 01, 2011 Jkt 223043 PO 00000 Frm 00912 Fmt 8010 Sfmt 8010 Y:SGML223043.XXX 223043wwoods2 on DSK1DXX6B1PROD with CFRProvided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-903 Federal Aviation Administ

42、ration, DOT 36.6 type certificate. When the time inter-val between the date of application for the type certificate and the issuance of the type certificate exceeds 5 years, the applicant must show that the aircraft meets the applicable requirements of this part that were effective on a date, to be

43、selected by the applicant, not earlier than 5 years before the issue of the type certificate. (b) Section 21.101(a) of this chapter notwithstanding, each person who ap-plies for an acoustical change to a type design specified in 21.93(b) of this chapter must show compliance with the applicable requi

44、rements of this part that are effective on the date of application for the change in type de-sign. When the time interval between the date of application for the change in type design and the issuance of the amended or supplemental type certifi-cate exceeds 5 years, the applicant must show that the

45、aircraft meets the applicable requirements of this part that were effective on a date, to be se-lected by the applicant, not earlier than 5 years before the issue of the amended or supplemental type certifi-cate. (c) If an applicant elects to comply with a standard in this part that was effective af

46、ter the filing of the applica-tion for a type certificate or change to a type design, the election: (1) Must be approved by the FAA; (2) Must include standards adopted between the date of application and the date of the election; (3) May include other standards adopted after the standard elected by

47、the applicant as determined by the FAA. Amdt. 3654, 67 FR 45211, July 8, 2002; Amdt. 3624, 67 FR 63195, Oct. 10, 2002 36.3 Compatibility with airworthi-ness requirements. It must be shown that the aircraft meets the airworthiness regulations constituting the type certification basis of the aircraft

48、under all condi-tions in which compliance with this part is shown, and that all procedures used in complying with this part, and all procedures and information for the flight crew developed under this part, are consistent with the airworthiness regulations constituting the type cer-tification basis

49、of the aircraft. Doc. No. 9337, 34 FR 18364, Nov. 18, 1969, as amended by Amdt. 3614, 53 FR 3540, Feb. 5, 1988 36.5 Limitation of part. Pursuant to 49 U.S.C. 1431(b)(4), the noise levels in this part have been de-termined to be as low as is economi-cally reasonable, technologically prac-ticable, and appropriate to the type of aircraft to which they apply. No deter-min