152
14 CFR Ch. I (1–1–24 Edition)
§ 21.111
regulations in effect on the date of the
application for the change.
(e) An application for a change to a
type certificate for a transport cat-
egory aircraft is effective for 5 years,
and an application for a change to any
other type certificate is effective for 3
years. If the change has not been ap-
proved, or if it is clear that it will not
be approved under the time limit es-
tablished under this paragraph, the ap-
plicant may do either of the following:
(1) File a new application for a
change to the type certificate and com-
ply with all the provisions of paragraph
(a) of this section applicable to an
original application for a change.
(2) File for an extension of the origi-
nal application and comply with the
provisions of paragraph (a) of this sec-
tion. The applicant must then select a
new application date. The new applica-
tion date may not precede the date the
change is approved by more than the
time period established under this
paragraph (e).
(f) For aircraft certificated under
§§ 21.17(b), 21.24, 21.25, and 21.27 the air-
worthiness requirements applicable to
the category of the product in effect on
the date of the application for the
change include each airworthiness re-
quirement that the FAA finds to be ap-
propriate for the type certification of
the aircraft in accordance with those
sections.
(g) Notwithstanding paragraph (b) of
this section, for transport category air-
planes, the applicant must show com-
pliance with each applicable provision
of part 26 of this chapter, unless the ap-
plicant has elected or was required to
comply with a corresponding amend-
ment to part 25 of this chapter that
was issued on or after the date of the
applicable part 26 provision.
[Doc. No. 28903, 65 FR 36266, June 7, 2000, as
amended by Amdt. 21–90, 72 FR 63404, Nov. 8,
2007; Amdt. 21–96, 77 FR 71695, Dec. 4, 2012;
Doc. No. FAA–2015–1621, Amdt. 21–100, 81 FR
96689, Dec. 30, 2016]
Subpart E—Supplemental Type
Certificates
S
OURCE
: Docket No. 5085, 29 FR 14568, Oct.
24, 1964, unless otherwise noted.
§ 21.111
Applicability.
This subpart prescribes procedural
requirements for the issue of supple-
mental type certificates.
§ 21.113
Requirement for supplemental
type certificate.
(a) If a person holds the TC for a
product and alters that product by in-
troducing a major change in type de-
sign that does not require an applica-
tion for a new TC under § 21.19, that
person must apply to the FAA either
for an STC, or to amend the original
type certificate under subpart D of this
part.
(b) If a person does not hold the TC
for a product and alters that product
by introducing a major change in type
design that does not require an applica-
tion for a new TC under § 21.19, that
person must apply to the FAA for an
STC.
(c) The application for an STC must
be made in the form and manner pre-
scribed by the FAA.
[Doc. No. FAA–2006–25877, Amdt. 21–92, 74 FR
53387, Oct. 16, 2009; Doc. No. FAA–2018–0119,
Amdt. 21–101, 83 FR 9169, Mar. 5, 2018]
§ 21.115
Applicable requirements.
(a) Each applicant for a supplemental
type certificate must show that the al-
tered product meets applicable require-
ments specified in § 21.101 and, in the
case of an acoustical change described
in § 21.93(b), show compliance with the
applicable noise requirements of part
36 of this chapter and, in the case of an
emissions change described in § 21.93(c),
show compliance with the applicable
fuel venting and exhaust emissions re-
quirements of part 34 of this chapter.
(b) Each applicant for a supplemental
type certificate must meet §§ 21.33 and
21.53 with respect to each change in the
type design.
[Amdt. 21–17, 32 FR 14927, Oct. 28, 1967, as
amended by Amdt. 21–42, 40 FR 1033, Jan. 6,
1975; Amdt. 21–52A, 45 FR 79009, Nov. 28, 1980;
Amdt. 21–61, 53 FR 3540, Feb. 5, 1988; Amdt.
21–68, 55 FR 32860, Aug. 10, 1990; Amdt. 21–71,
57 FR 42854, Sept. 16, 1992; Amdt. 21–77, 65 FR
36266, June 7, 2000]
§ 21.117
Issue of supplemental type
certificates.
(a) An applicant is entitled to a sup-
plemental type certificate if the FAA
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