161
Federal Aviation Administration, DOT
§ 21.184
the airplane complies with the applica-
ble requirements of that part.
(h)
New aircraft manufactured under
the provisions of § 21.6(b). An applicant
for a standard airworthiness certificate
for a new aircraft manufactured under
the provisions of § 21.6(b) is entitled to
a standard airworthiness certificate
if—
(1) The applicant presents evidence to
the FAA that the aircraft conforms to
a type design approved under a type
certificate or supplemental type cer-
tificate and to applicable Airworthi-
ness Directives;
(2) The aircraft has been inspected in
accordance with the performance rules
for a 100-hour inspections set forth in
§ 43.15 of this chapter and found air-
worthy by a person specified in para-
graph (d)(2) of this section; and
(3) The FAA finds after inspection,
that the aircraft conforms to the type
design, and is in condition for safe op-
eration.
[Amdt. 21–17, 32 FR 14927, Oct. 28, 1967]
E
DITORIAL
N
OTE
: For F
EDERAL
R
EGISTER
ci-
tations affecting § 21.183, see the List of CFR
Sections Affected, which appears in the
Finding Aids section of the printed volume
and at
www.govinfo.gov.
§ 21.184
Issue of special airworthiness
certificates for primary category
aircraft.
(a)
New primary category aircraft man-
ufactured under a production certificate.
An applicant for an original, special
airworthiness certificate-primary cat-
egory for a new aircraft that meets the
criteria of § 21.24(a)(1), manufactured
under a production certificate, includ-
ing aircraft assembled by another per-
son from a kit provided by the holder
of the production certificate and under
the supervision and quality control of
that holder, is entitled to a special air-
worthiness certificate without further
showing, except that the FAA may in-
spect the aircraft to determine con-
formity to the type design and condi-
tion for safe operation.
(b)
Imported aircraft. An applicant for
a special airworthiness certificate-pri-
mary category for an imported aircraft
type certificated under § 21.29 is enti-
tled to a special airworthiness certifi-
cate if the civil airworthiness author-
ity of the country in which the aircraft
was manufactured certifies, and the
FAA finds after inspection, that the
aircraft conforms to an approved type
design that meets the criteria of
§ 21.24(a)(1) and is in a condition for
safe operation.
(c)
Aircraft having a current standard
airworthiness certificate. An applicant
for a special airworthiness certificate-
primary category, for an aircraft hav-
ing a current standard airworthiness
certificate that meets the criteria of
§ 21.24(a)(1), may obtain the primary
category certificate in exchange for its
standard airworthiness certificate
through the supplemental type certifi-
cation process. For the purposes of this
paragraph, a current standard air-
worthiness certificate means that the
aircraft conforms to its approved nor-
mal, utility, or acrobatic type design,
complies with all applicable airworthi-
ness directives, has been inspected and
found airworthy within the last 12 cal-
endar months in accordance with
§ 91.409(a)(1) of this chapter, and is
found to be in a condition for safe oper-
ation by the FAA.
(d)
Other aircraft. An applicant for a
special airworthiness certificate-pri-
mary category for an aircraft that
meets the criteria of § 21.24(a)(1), and is
not covered by paragraph (a), (b), or (c)
of this section, is entitled to a special
airworthiness certificate if—
(1) The applicant presents evidence to
the FAA that the aircraft conforms to
an approved primary, normal, utility,
or acrobatic type design, including
compliance with all applicable air-
worthiness directives;
(2) The aircraft has been inspected
and found airworthy within the past 12
calendar months in accordance with
§ 91.409(a)(1) of this chapter and;
(3) The aircraft is found by the FAA
to conform to an approved type design
and to be in a condition for safe oper-
ation.
(e)
Multiple-category airworthiness cer-
tificates in the primary category and
any other category will not be issued; a
primary category aircraft may hold
only one airworthiness certificate.
[Doc. No. 23345, 57 FR 41368, Sept. 9, 1992, as
amended by Amdt. 21–70, 57 FR 43776, Sept.
22, 1992]
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