FAA 14 CFR PART 21-2011 CERTIFICATION PROCEDURES FOR PRODUCTS AND PARTS《产品和零件的认证程序》.pdf

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1、121 SUBCHAPTER CAIRCRAFT PART 21CERTIFICATION PROCE-DURES FOR PRODUCTS AND PARTS SPECIAL FEDERAL AVIATION REGULATION NO. 88 Subpart AGeneral Sec. 21.1 Applicability. 21.2 Falsification of applications, reports, or records. 21.3 Reporting of failures, malfunctions, and defects. 21.4 ETOPS reporting r

2、equirements. 21.5 Airplane or Rotorcraft Flight Manual. 21.6 Manufacture of new aircraft, aircraft engines, and propellers. 21.7 Continued airworthiness and safety im-provements for transport category air-planes. 21.8 Approval of articles. 21.9 Replacement and modification articles. Subpart BType Ce

3、rtificates 21.11 Applicability. 21.13 Eligibility. 21.15 Application for type certificate. 21.16 Special conditions. 21.17 Designation of applicable regulations. 21.19 Changes requiring a new type certifi-cate. 21.20 Compliance with applicable require-ments. 21.21 Issue of type certificate: normal,

4、util-ity, acrobatic, commuter, and transport category aircraft; manned free balloons; special classes of aircraft; aircraft en-gines; propellers. 21.23 Reserved 21.24 Issuance of type certificate: primary category aircraft. 21.25 Issue of type certificate: Restricted category aircraft. 21.27 Issue o

5、f type certificate: surplus air-craft of the Armed Forces. 21.29 Issue of type certificate: import prod-ucts. 21.31 Type design. 21.33 Inspection and tests. 21.35 Flight tests. 21.37 Flight test pilot. 21.39 Flight test instrument calibration and correction report. 21.41 Type certificate. 21.43 Loca

6、tion of manufacturing facilities. 21.45 Privileges. 21.47 Transferability. 21.49 Availability. 21.50 Instructions for continued airworthi-ness and manufacturers maintenance manuals having airworthiness limita-tions sections. 21.51 Duration. 21.53 Statement of conformity. 21.55 Responsibility of type

7、 certificate hold-ers to provide written licensing agree-ments. Subpart CProvisional Type Certificates 21.71 Applicability. 21.73 Eligibility. 21.75 Application. 21.77 Duration. 21.79 Transferability. 21.81 Requirements for issue and amend-ment of Class I provisional type certifi-cates. 21.83 Requir

8、ements for issue and amend-ment of Class II provisional type certifi-cates. 21.85 Provisional amendments to type cer-tificates. Subpart DChanges to Type Certificates 21.91 Applicability. 21.93 Classification of changes in type de-sign. 21.95 Approval of minor changes in type de-sign. 21.97 Approval

9、of major changes in type de-sign. 21.99 Required design changes. 21.101 Designation of applicable regulations. Subpart ESupplemental Type Certificates 21.111 Applicability. 21.113 Requirement of supplemental type certificate. 21.115 Applicable requirements. 21.117 Issue of supplemental type certifi-

10、cates. 21.119 Privileges. 21.120 Responsibility of supplemental type certificate holders to provide written permission for alterations. Subpart FProduction Under Type Certificate Only 21.121 Applicability. 21.122 Location of or change to manufac-turing facilities. 21.123 Production under type certif

11、icate. 21.125 Production inspection system: Mate-rials Review Board. 21.127 Tests: aircraft. 21.128 Tests: aircraft engines. 21.129 Tests: propellers. 21.130 Statement of conformity. VerDate Mar2010 14:10 Mar 01, 2011 Jkt 223043 PO 00000 Frm 00131 Fmt 8010 Sfmt 8010 Y:SGML223043.XXX 223043wwoods2 on

12、 DSK1DXX6B1PROD with CFRProvided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-122 14 CFR Ch. I (1111 Edition) Pt. 21 Subpart GProduction Certificates 21.131 Applicability. 21.133 Eligibility. 21.135 Requirements for issuance. 21.137 Location of manufacturi

13、ng facilities. 21.139 Quality control. 21.143 Quality control data requirements; prime manufacturer. 21.147 Changes in quality control system. 21.149 Multiple products. 21.151 Production limitation record. 21.153 Amendment of the production certifi-cates. 21.155 Transferability. 21.157 Inspections a

14、nd tests. 21.159 Duration. 21.161 Display. 21.163 Privileges. 21.165 Responsibility of holder. Subpart HAirworthiness Certificates 21.171 Applicability. 21.173 Eligibility. 21.175 Airworthiness certificates: classifica-tion. 21.177 Amendment or modification. 21.179 Transferability. 21.181 Duration.

15、21.182 Aircraft identification. 21.183 Issue of standard airworthiness cer-tificates for normal, utility, acrobatic, commuter, and transport category air-craft; manned free balloons; and special classes of aircraft. 21.184 Issue of special airworthiness certifi-cates for primary category aircraft. 2

16、1.185 Issue of airworthiness certificates for restricted category aircraft. 21.187 Issue of multiple airworthiness cer-tification. 21.189 Issue of airworthiness certificate for limited category aircraft. 21.190 Issue of a special airworthiness cer-tificate for a light-sport category air-craft. 21.19

17、1 Experimental certificates. 21.193 Experimental certificates: general. 21.195 Experimental certificates: Aircraft to be used for market surveys, sales dem-onstrations, and customer crew training. 21.197 Special flight permits. 21.199 Issue of special flight permits. Subpart IProvisional Airworthine

18、ss Certificates 21.211 Applicability. 21.213 Eligibility. 21.215 Application. 21.217 Duration. 21.219 Transferability. 21.221 Class I provisional airworthiness cer-tificates. 21.223 Class II provisional airworthiness cer-tificates. 21.225 Provisional airworthiness certificates corresponding with pro

19、visional amend-ments to type certificates. Subpart JDelegation Option Authorization Procedures 21.231 Applicability. 21.235 Application. 21.239 Eligibility. 21.243 Duration. 21.245 Maintenance of eligibility. 21.247 Transferability. 21.249 Inspections. 21.251 Limits of applicability. 21.253 Type cer

20、tificates: application. 21.257 Type certificates: issue. 21.261 Equivalent safety provisions. 21.267 Production certificates. 21.269 Export airworthiness approvals. 21.271 Airworthiness approval tags. 21.273 Airworthiness certificates other than experimental. 21.275 Experimental certificates. 21.277

21、 Data review and service experience. 21.289 Major repairs, rebuilding and alter-ation. 21.293 Current records. Subpart KApproval of Materials, Parts, Processes, and Appliances 21.301 Applicability. 21.303 Replacement and modification parts. 21.305 Approval of materials, parts, proc-esses, and applia

22、nces. Subpart LExport Airworthiness Approvals 21.321 Applicability. 21.325 Export airworthiness approvals. 21.327 Application. 21.329 Issuance of export certificates of air-worthiness. 21.331 Issuance of export airworthiness ap-provals for aircraft engines, propellers, and articles. 21.335 Responsib

23、ilities of exporters. Subpart MDesignated Alteration Station Authorization Procedures 21.431 Applicability. 21.435 Application. 21.439 Eligibility. 21.441 Procedure manual. 21.443 Duration. 21.445 Maintenance of eligibility. 21.447 Transferability. 21.449 Inspections. 21.451 Limits of applicability.

24、 21.461 Equivalent safety provisions. 21.463 Supplemental type certificates. 21.473 Airworthiness certificates other than experimental. 21.475 Experimental certificates. 21.477 Data review and service experience. VerDate Mar2010 14:10 Mar 01, 2011 Jkt 223043 PO 00000 Frm 00132 Fmt 8010 Sfmt 8010 Y:S

25、GML223043.XXX 223043wwoods2 on DSK1DXX6B1PROD with CFRProvided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-123 Federal Aviation Administration, DOT Pt. 21, SFAR No. 88 21.493 Current records. Subpart NAcceptance of Aircraft Engines, Propellers, and Articl

26、es for Import 21.500 Acceptance of aircraft engines and propellers. 21.502 Acceptance of articles. Subpart OTechnical Standard Order Authorizations 21.601 Applicability. 21.603 TSO marking and privileges. 21.605 Application and issue. 21.607 General rules governing holders of TSO authorizations. 21.

27、609 Approval for deviation. 21.611 Design changes. 21.613 Recordkeeping requirements. 21.615 FAA inspection. 21.617 Issue of letters of TSO design ap-proval: import appliances. 21.619 Noncompliance. 21.621 Transferability and duration. AUTHORITY: 42 U.S.C. 7572; 49 U.S.C. 106(g), 40105, 40113, 44701

28、44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. EFFECTIVE DATE NOTE: By Amdt. 21-92, 74 FR 53384, Oct. 16, 2009, part 21 was amended by removing the word Administrator and adding in its place the word FAA wherever it appeared; removing the word shall and adding in its place the word must whe

29、rever it appeared; and removing the phrase type certificate only and adding in its place the phrase type certificate wherever it ap-peared, effective Apr. 14, 2010. This effective date was postponed to Apr. 16, 2011 at 75 FR 9095, Mar. 1, 2010. EDITORIAL NOTE: For miscellaneous amend-ments to cross

30、references in this Part 21 see Amdt. 2110, 31 FR 9211, July 6, 1966. SPECIAL FEDERAL AVIATION REGULATION NO. 88FUEL TANK SYSTEM FAULT TOLERANCE EVALUATION REQUIRE-MENTS 1. Applicability. This SFAR applies to the holders of type certificates, and supple-mental type certificates that may affect the ai

31、rplane fuel tank system, for turbine-pow-ered transport category airplanes, provided the type certificate was issued after January 1, 1958, and the airplane has either a max-imum type certificated passenger capacity of 30 or more, or a maximum type certificated payload capacity of 7,500 pounds or mo

32、re. This SFAR also applies to applicants for type certificates, amendments to a type cer-tificate, and supplemental type certificates affecting the fuel tank systems for those air-planes identified above, if the application was filed before June 6, 2001, the effective date of this SFAR, and the cert

33、ificate was not issued before June 6, 2001. 2. Compliance: Each type certificate holder, and each supplemental type certificate hold-er of a modification affecting the airplane fuel tank system, must accomplish the fol-lowing within the compliance times specified in paragraph (e) of this section: (a

34、) Conduct a safety review of the airplane fuel tank system to determine that the de-sign meets the requirements of 25.901 and 25.981(a) and (b) of this chapter. If the cur-rent design does not meet these require-ments, develop all design changes to the fuel tank system that are necessary to meet the

35、se requirements. The FAA (Aircraft Cer-tification Office (ACO), or office of the Transport Airplane Directorate, having cog-nizance over the type certificate for the af-fected airplane) may grant an extension of the 18-month compliance time for develop-ment of design changes if: (1) The safety revie

36、w is completed within the compliance time; (2) Necessary design changes are identified within the compliance time; and (3) Additional time can be justified, based on the holders demonstrated aggressiveness in performing the safety review, the com-plexity of the necessary design changes, the availabi

37、lity of interim actions to provide an acceptable level of safety, and the resulting level of safety. (b) Develop all maintenance and inspection instructions necessary to maintain the de-sign features required to preclude the exist-ence or development of an ignition source within the fuel tank system

38、 of the airplane. (c) Submit a report for approval to the FAA Aircraft Certification Office (ACO), or office of the Transport Airplane Directorate, having cognizance over the type certificate for the affected airplane, that: (1) Provides substantiation that the air-plane fuel tank system design, inc

39、luding all necessary design changes, meets the require-ments of 25.901 and 25.981(a) and (b) of this chapter; and (2) Contains all maintenance and inspec-tion instructions necessary to maintain the design features required to preclude the ex-istence or development of an ignition source within the fu

40、el tank system throughout the operational life of the airplane. (d) The Aircraft Certification Office (ACO), or office of the Transport Airplane Direc-torate, having cognizance over the type cer-tificate for the affected airplane, may ap-prove a report submitted in accordance with paragraph 2(c) if

41、it determines that any pro-visions of this SFAR not complied with are compensated for by factors that provide an equivalent level of safety. (e) Each type certificate holder must com-ply no later than December 6, 2002, or within VerDate Mar2010 14:10 Mar 01, 2011 Jkt 223043 PO 00000 Frm 00133 Fmt 80

42、10 Sfmt 8002 Y:SGML223043.XXX 223043wwoods2 on DSK1DXX6B1PROD with CFRProvided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-124 14 CFR Ch. I (1111 Edition) 21.1 18 months after the issuance of a type cer-tificate for which application was filed be-fore Jun

43、e 6, 2001, whichever is later; and each supplemental type certificate holder of a modification affecting the airplane fuel tank system must comply no later than June 6, 2003, or within 18 months after the issuance of a supplemental type certificate for which application was filed before June 6, 2001

44、, whichever is later. Doc. No. 19996411, 66 FR 23129, May 7, 2001, as amended by Amdt. 2182, 67 FR 57493, Sept. 10, 2002; 67 FR 70809, Nov. 26, 2002; Amdt. 21 83, 67 FR 72833, Dec. 9, 2002 Subpart AGeneral 21.1 Applicability. (a) This part prescribes (1) Procedural requirements for the issue of type

45、 certificates and changes to those certificates; the issue of pro-duction certificates; the issue of air-worthiness certificates; and the issue of export airworthiness approvals. (2) Rules governing the holders of any certificate specified in paragraph (a)(1) of this section; and (3) Procedural requ

46、irements for the approval of certain materials, parts, processes, and appliances. (b) For the purposes of this part, the word product means an aircraft, air-craft engine, or propeller. In addition, for the purposes of Subpart L only, it includes components and parts of air-craft, of aircraft engines

47、, and of propel-lers; also parts, materials, and appli-ances, approved under the Technical Standard Order system. Doc. No. 5085, 29 FR 14563, Oct. 24, 1964, as amended by Amdt. 212, 30 FR 8465, July 2, 1965; Amdt. 216, 30 FR 11379, Sept. 8, 1965 EFFECTIVE DATE NOTE: By Doc. No. FAA- 2006-25877, 74 F

48、R 53384, Oct. 16, 2009, 21.1 was revised, effective Apr. 14, 2010. This effective date was subsequently postponed to Apr. 16, 2011 at 75 FR 9095, Mar. 1, 2010. For the con-venience of the user, the revised text is set forth as follows: 21.1 Applicability and definitions. (a) This part prescribes (1)

49、 Procedural requirements for issuing and changing (i) Design approvals; (ii) Production approvals; (iii) Airworthiness certificates; and (iv) Airworthiness approvals; (2) Rules governing applicants for, and holders of, any approval or certificate speci-fied in paragraph (a)(1) of this section; and (3) Procedural requirements for the ap-proval of articles. (b) For the purposes of this part (1) Airworthiness approval means a