1004 

14 CFR Ch. I (1–1–14 Edition) 

§ 45.13 

(h) 

Gliders. Paragraphs (a)(3) and (e) 

of this section do not apply to gliders. 

[Amdt. 45–26, 74 FR 53394, Oct. 16, 2009, as 
amended by Amdt. 45–27, 76 FR 7486, Feb. 10, 
2011] 

§ 45.13

Identification data. 

(a) The identification required by 

§ 45.11 (a) through (c) must include the 
following information: 

(1) Builder’s name. 
(2) Model designation. 
(3) Builder’s 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, for 

aircraft engines specified in part 34 of 
this chapter, the date of manufacture 
as defined in § 34.1 of this chapter, and 
a designation, approved by the FAA, 
that indicates compliance with the ap-
plicable exhaust emission provisions of 
part 34 of this chapter and 40 CFR part 
87. Approved designations include 
COMPLY, EXEMPT, and NON–US, as 
appropriate. After December 31, 2012, 
approved designations also include EX-
EMPT NEW, and EXCEPTED SPARE, 
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 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 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 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 the United 
States’’, or an equivalent notation ap-
proved by the FAA, must be inserted in 
the aircraft logbook, or alternate 
equivalent document, at the time of in-
stallation of the engine. 

(iv) The designation EXEMPT NEW 

indicates that the engine has been 
granted an exemption pursuant to the 
applicable provision of § 34.7(h) of this 
chapter; the designation must be noted 
in the permanent powerplant record 
that accompanies the engine from the 
time of its manufacture. 

(v) The designation EXCEPTED 

SPARE indicates that the engine has 
been excepted pursuant to the applica-
ble provision of § 34.9(b) of this chapter; 
the designation must be noted in the 
permanent powerplant record that ac-
companies the engine from the time of 
its manufacture. 

(8) Any other information the FAA 

finds appropriate. 

(b) Except as provided in paragraph 

(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 FAA. 

(c) Except as provided in paragraph 

(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 FAA. 

(d) Persons performing work under 

the provisions of Part 43 of this chapter 
may, in accordance with methods, 
techniques, and practices acceptable to 
the FAA— 

(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. 

(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, 
propeller blade, or propeller hub other 

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