1、989 Federal Aviation Administration, DOT 45.1 PART 45IDENTIFICATION AND REGISTRATION MARKING Subpart AGeneral Sec. 45.1 Applicability. Subpart BIdentification of Aircraft and Related Products 45.10 Marking. 45.11 Marking of products. 45.13 Identification data. 45.14 Identification of critical compon
2、ents. 45.15 Replacement and modification parts. 45.16 Marking of life-limited parts. Subpart CNationality and Registration Marks 45.21 General. 45.22 Exhibition, antique, and other air-craft: Special rules. 45.23 Display of marks; general. 45.25 Location of marks on fixed-wing air-craft. 45.27 Locat
3、ion of marks; nonfixed-wing air-craft. 45.29 Size of marks. 45.31 Marking of export aircraft. 45.33 Sale of aircraft; removal of marks. AUTHORITY: 49 U.S.C. 106(g), 40103, 44109, 4011340114, 4410144105, 4410744108, 44110 44111, 44504, 44701, 4470844709, 4471144713, 44725, 4530245303, 46104, 46304, 4
4、6306, 47122. EFFECTIVE DATE NOTE: By FAA 2006-25877, 74 FR 53394, Oct. 16, 2009, the authority cita-tion for part 45 was revised, effective Apr. 14, 2010. The effective date of this revision was subsequently postponed to Apr. 16, 2011 at 75 FR 9095, Mar. 1, 2010. For the convenience of the user, the
5、 revised text is set forth as fol-lows: AUTHORITY: 49 U.S.C. 106(g), 40103, 40113 40114, 4410144105, 4410744111, 44504, 44701, 4470844709, 4471144713, 44725, 4530245303, 46104, 46304, 46306, 47122. SOURCE: Docket No. 2047, 29 FR 3223, Mar. 11, 1964, unless otherwise noted. EFFECTIVE DATE NOTE: At 74
6、 FR 53394, Oct. 16, 2009, part 45 was amended by removing the word Administrator and the words Ad-ministrator of the FAA and adding in their place the word FAA wherever they appear; and by removing the word shall and adding in its place the word must wherever it ap-pears, effective Apr. 14, 2010. Th
7、e effective date of these revisions was subsequently postponed to Apr. 16, 2011 at 75 FR 9095, Mar. 1, 2010. Subpart AGeneral 45.1 Applicability. This part prescribes the requirements for (a) Identification of aircraft, and identification of aircraft engines and propellers that are manufactured unde
8、r the terms of a type or production cer-tificate: (b) Identification of certain replace-ment and modified parts produced for installation on type certificated prod-ucts; and (c) Nationality and registration marking of U.S. registered aircraft. Doc. No. 2047, 29 FR 3223, Mar. 11, 1964, as amended by
9、Amdt. 453, 32 FR 188, Jan. 10, 1967 EFFECTIVE DATE NOTE: By Amdt. 45-26, 74 FR 53394, Oct. 16, 2009, 45.1 was amended by revising paragraphs (a) and (b) and removing paragraph (c), effective Apr. 14, 2010. The ef-fective date of these revisions was subse-quently postponed to Apr. 16, 2011 at 75 FR 9
10、095, Mar. 1, 2010. For the convenience of the user, the revised text is set forth as follows: 45.1 Applicability. * * * * * (a) Marking products and articles manu-factured under (1) A type certificate; (2) A production approval as defined under part 21 of this chapter; and (3) The provisions of an a
11、greement between the United States and another country or ju-risdiction for the acceptance of products and articles; and (b) Nationality and registration marking of U.S. registered aircraft. Subpart BIdentification of Aircraft and Related Products EFFECTIVE DATE NOTE: By Docket No. FAA-2006-25877, 7
12、4 FR 53394, Oct. 16, 2009, the heading of subpart B was revised, effective Apr. 14, 2010. The effective date of this revi-sion 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: Subpart BMarking of Prod
13、ucts and Articles VerDate Mar2010 14:10 Mar 01, 2011 Jkt 223043 PO 00000 Frm 00999 Fmt 8010 Sfmt 8010 Y:SGML223043.XXX 223043wwoods2 on DSK1DXX6B1PROD with CFRProvided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-990 14 CFR Ch. I (1111 Edition) 45.10 45.10
14、 Marking. No person may mark a product or ar-ticle in accordance with this subpart unless (a) That person produced the product or article (1) Under part 21, subpart F, G, K, or O of this chapter; or (2) For export to the United States under the provisions of an agreement between the United States an
15、d another country or jurisdiction for the accept-ance of products and articles; and (b) That product or article conforms to its approved design, and is in a con-dition for safe operation; and, for a TSO article; that TSO article meets the applicable performance standards. Doc. No. FAA-2006-25877, 74
16、 FR 53394, Oct. 16, 2009 EFFECTIVE DATE NOTE: By Doc. No. FAA- 2006-25877, 74 FR 53394, Oct. 16, 2009, 45.10 was added, effective Apr. 14, 2010. The effec-tive date of this addition was subsequently postponed to Apr. 16, 2011 at 75 FR 9095, Mar. 1, 2010. 45.11 Marking of products. (a) Aircraft. A ma
17、nufacturer of air-craft covered under 21.182 of this chap-ter must mark each aircraft by attach-ing a fireproof identification plate that (1) Includes the information specified in 45.13 using an approved method of fireproof marking; (2) Must be secured in such a manner that it will not likely be def
18、aced or re-moved during normal service, or lost or destroyed in an accident; and (3) Except as provided in paragraphs (d) through (h) of this section, must be secured to the aircraft fuselage exte-rior so that it is legible to a person on the ground, and must be either adja-cent to and aft of the re
19、ar-most en-trance door or on the fuselage surface near the tail surfaces. (b) Aircraft engines. A manufacturer of an aircraft engine produced under a type certificate or production certifi-cate must mark each engine by attach-ing a fireproof identification plate. Such plate (1) Must include the info
20、rmation specified in 45.13 using an approved method of fireproof marking; (2) Must be affixed to the engine at an accessible location; and (3) Must be secured in such a manner that it will not likely be defaced or re-moved during normal service, or lost or destroyed in an accident. (c) Propellers an
21、d propeller blades and hubs. Each person who produces a pro-peller, propeller blade, or propeller hub under a type certificate or production certificate must mark each product or part using an approved fireproof meth-od. The marking must (1) Be placed on a non-critical sur-face; (2) Contain the info
22、rmation specified in 45.13; (3) Not likely be defaced or removed during normal service; and (4) Not likely be lost or destroyed in an accident. (d) Manned free balloons. A manufac-turer of manned free balloons must mark each balloon by attaching the identification plate described in para-graph (a) o
23、f this section. The plate must be secured to the balloon enve-lope and must be located, if prac-ticable, where it is legible to the oper-ator when the balloon is inflated. In addition, the basket and heater assem-bly must be permanently and legibly marked with the manufacturers name, part number (or
24、 equivalent), and serial number (or equivalent). (e) Aircraft manufactured before March 7, 1988. The owner or operator of an air-craft manufactured before March 7, 1988 must mark the aircraft by attach-ing the identification plate required by paragraph (a) of this section. The plate must be secured
25、at an accessible exte-rior or interior location near an en-trance, if the model designation and builders serial number are also dis-played on the exterior of the aircraft fuselage. The model designation and builders serial number must be (1) Legible to a person on the ground, (2) Located either adja
26、cent to and aft of the rear-most entrance door or on the fuselage near the tail surfaces, and (3) Displayed in such a manner that they are not likely to be defaced or re-moved during normal service. (f) For powered parachutes and weight-shift-control aircraft, the iden-tification plate required by p
27、aragraph (a) of this section must be secured to the exterior of the aircraft fuselage so VerDate Mar2010 14:10 Mar 01, 2011 Jkt 223043 PO 00000 Frm 01000 Fmt 8010 Sfmt 8010 Y:SGML223043.XXX 223043wwoods2 on DSK1DXX6B1PROD with CFRProvided by IHSNot for ResaleNo reproduction or networking permitted w
28、ithout license from IHS-,-,-991 Federal Aviation Administration, DOT 45.13 that it is legible to a person on the ground. (g) The identification plate described in paragraph (a) of this section may be secured to the aircraft at an accessible location near an entrance for (1) Aircraft produced for (i)
29、 Operations under part 121 of this chapter, (ii) Commuter operations (as defined in 119.3 of this chapter), or (iii) Export. (2) Aircraft operating under part 121 of this chapter and under an FAA-ap-proved continuous airworthiness main-tenance program; or (3) Aircraft operating in commuter air carri
30、er operations (as defined in 119.3 of this chapter) under an FAA- approved continuous airworthiness maintenance program. (h) Gliders. Paragraphs (a)(3) and (e) of this section do not apply to gliders. Amdt. No. 4526, 74 FR 53394, Oct. 16, 2009 45.13 Identification data. (a) The identification requir
31、ed by 45.11 (a) through (c)shall include the following information: (1) Builders name. (2) Model designation. (3) Builders serial number. (4) Type certificate number, if any. (5) Production certificate number, if any. (6) For aircraft engines, the estab-lished rating. (7) On or after January 1, 1984
32、, for aircraft engines specified in part 34 of this chapter, the date of manufacture as defined in 34.1 of that part, and a designation, approved by the Adminis-trator of the FAA, that indicates com-pliance with the applicable exhaust emission provisions of part 34 and 40 CFR part 87. Approved desig
33、nations in-clude COMPLY, EXEMPT, and NON-US as appropriate. (i) The designation COMPLY indi-cates that the engine is in compliance with all of the applicable exhaust emis-sions provisions of part 34. For any en-gine with a rated thrust in excess of 26.7 kilonewtons (6000 pounds) which is not used or
34、 intended for use in com-mercial operations and which is in compliance with the applicable provi-sions of part 34, but does not comply with the hydrocarbon emissions stand-ard of 34.21(d), the statement May not be used as a commercial aircraft engine must be noted in the perma-nent powerplant record
35、 that accom-panies the engine at the time of manu-facture of the engine. (ii) The designation EXEMPT indi-cates that the engine has been granted an exemption pursuant to the applica-ble provision of 34.7 (a)(1), (a)(4), (b), (c), or (d), and an indication of the type of exemption and the reason for
36、the grant must be noted in the permanent powerplant record that accompanies the engine from the time of manufac-ture of the engine. (iii) The designation NON-US indi-cates that the engine has been granted an exemption pursuant to 34.7(a)(1), and the notation This aircraft may not be operated within
37、the United States, or an equivalent notation ap-proved by the Administrator of the FAA, must be inserted in the aircraft logbook, or alternate equivalent docu-ment, at the time of installation of the engine. (8) Any other information the Admin-istrator finds appropriate. (b) Except as provided in pa
38、ragraph (d)(1) of this section, no person may re-move, change, or place identification information required by paragraph (a) of this section, on any aircraft, aircraft engine, propeller, propeller blade, or propeller hub, without the approval of the Administrator. (c) Except as provided in paragraph
39、 (d)(2) of this section, no person may re-move or install any identification plate required by 45.11, without the ap-proval of the Administrator. (d) Persons performing work under the provisions of Part 43 of this chapter may, in accordance with methods, techniques, and practices acceptable to the A
40、dministrator (1) Remove, change, or place the identification information required by paragraph (a) of this section on any aircraft, aircraft engine, propeller, pro-peller blade, or propeller hub; or (2) Remove an identification plate re-quired by 45.11 when necessary during maintenance operations. (
41、e) No person may install an identi-fication plate removed in accordance with paragraph (d)(2) of this section on any aircraft, aircraft engine, propeller, VerDate Mar2010 14:10 Mar 01, 2011 Jkt 223043 PO 00000 Frm 01001 Fmt 8010 Sfmt 8010 Y:SGML223043.XXX 223043wwoods2 on DSK1DXX6B1PROD with CFRProv
42、ided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-992 14 CFR Ch. I (1111 Edition) 45.14 propeller blade, or propeller hub other than the one from which it was re-moved. Amdt. 453, 32 FR 188, Jan. 10, 1967, as amended by Amdt. 4510, 44 FR 45379, Aug. 2, 197
43、9; Amdt. 4512, 45 FR 60183, Sept. 11, 1980; Amdt. 4520, 55 FR 32861, Aug. 10, 1990; 55 FR 37287, Sept. 10, 1990; Amdt. 4526, 74 FR 53395, Oct. 16, 2009 45.14 Identification of critical compo-nents. Each person who produces a part for which a replacement time, inspection interval, or related procedur
44、e is speci-fied in the Airworthiness Limitations section of a manufacturers mainte-nance manual or Instructions for Con-tinued Airworthiness shall perma-nently and legibly mark that compo-nent with a part number (or equiva-lent) and a serial number (or equiva-lent). Amdt. 4516, 51 FR 40703, Nov. 7,
45、1986 EFFECTIVE DATE NOTE: By Amdt. 45-26, 74 FR 53395, Oct. 16, 2009, 45.14 was removed, ef-fective Apr. 14, 2010. The effective date of this removal was subsequently postponed to Apr. 16, 2011 at 75 FR 9095, Mar. 1, 2010. 45.15 Replacement and modification parts. (a) Except as provided in paragraph
46、 (b) of this section, each person who produces a replacement or modifica-tion part under a Parts Manufacturer Approval issued under 21.303 of this chapter shall permanently and legibly mark the part with (1) The letters FAA-PMA; (2) The name, trademark, or symbol of the holder of the Parts Manufactu
47、rer Approval; (3) The part number; and (4) The name and model designation of each type certificated product on which the part is eligible for installa-tion. (b) If the Administrator finds that a part is too small or that it is otherwise impractical to mark a part with any of the information required
48、 by paragraph (a) of this section, a tag attached to the part or its container must include the information that could not be marked on the part. If the marking re-quired by paragraph (a)(4) of this sec-tion is so extensive that to mark it on a tag is impractical, the tag attached to the part or the
49、 container may refer to a specific readily available manual or catalog for part eligibility informa-tion. Amdt. 458, 37 FR 10660, May 26, 1972, as amended by Amdt. 4514, 47 FR 13315, Mar. 29, 1982 EFFECTIVE DATE NOTE: By Doc. No. FAA- 2006-25877, 74 FR 53395, Oct. 16, 2009, 45.15 was revised, effective Apr. 14, 2010. The effec-tive date of this revision was subsequent
