163
Federal Aviation Administration, DOT
§ 21.223
§ 21.215
Application.
Applications for provisional air-
worthiness certificates must be sub-
mitted to the Manufacturing Inspec-
tion District Office in the geographic
area in which the manufacturer or air
carrier is located. The application
must be accompanied by the pertinent
information specified in this subpart.
[Amdt. 21–67, 54 FR 39291, Sept. 25, 1989; 54 FR
52872, Dec. 22, 1989]
§ 21.217
Duration.
Unless sooner surrendered, super-
seded, revoked, or otherwise termi-
nated, provisional airworthiness cer-
tificates are effective for the duration
of the corresponding provisional type
certificate, amendment to a provi-
sional type certificate, or provisional
amendment to the type certificate.
§ 21.219
Transferability.
Class I provisional airworthiness cer-
tificates are not transferable. Class II
provisional airworthiness certificates
may be transferred to an air carrier eli-
gible to apply for a certificate under
§ 21.213(b).
§ 21.221
Class I provisional airworthi-
ness certificates.
(a) Except as provided in § 21.225, an
applicant is entitled to a Class I provi-
sional airworthiness certificate for an
aircraft for which a Class I provisional
type certificate has been issued if—
(1) He meets the eligibility require-
ments of § 21.213 and he complies with
this section; and
(2) The FAA finds that there is no
feature, characteristic or condition of
the aircraft that would make the air-
craft unsafe when operated in accord-
ance with the limitations established
in §§ 21.81(e) and 91.317 of this sub-
chapter.
(b) The manufacturer must hold a
provisional type certificate for the air-
craft.
(c) The manufacturer must submit a
statement that the aircraft conforms
to the type design corresponding to the
provisional type certificate and has
been found by him to be in safe oper-
ating condition under all applicable
limitations.
(d) The aircraft must be flown at
least five hours by the manufacturer.
(e) The aircraft must be supplied
with a provisional aircraft flight man-
ual or other document and appropriate
placards containing the limitations es-
tablished by §§ 21.81(e) and 91.317.
[Doc. No. 5085, 29 FR 14571, Oct. 24, 1964, as
amended by Amdt. 21–66, 54 FR 34329, Aug. 18,
1989]
§ 21.223
Class II provisional airworthi-
ness certificates.
(a) Except as provided in § 21.225, an
applicant is entitled to a Class II provi-
sional airworthiness certificate for an
aircraft for which a Class II provisional
type certificate has been issued if—
(1) He meets the eligibility require-
ments of § 21.213 and he complies with
this section; and
(2) The FAA finds that there is no
feature, characteristic, or condition of
the aircraft that would make the air-
craft unsafe when operated in accord-
ance with the limitations established
in §§ 21.83(h), 91.317, and 121.207 of this
chapter.
(b) The applicant must show that a
Class II provisional type certificate for
the aircraft has been issued to the
manufacturer.
(c) The applicant must submit a
statement by the manufacturer that
the aircraft has been manufactured
under a quality system adequate to en-
sure that the aircraft conforms to the
type design corresponding with the
provisional type certificate.
(d) The applicant must submit a
statement that the aircraft has been
found by him to be in a safe operating
condition under the applicable limita-
tions.
(e) The aircraft must be flown at
least five hours by the manufacturer.
(f) The aircraft must be supplied with
a provisional aircraft flight manual
containing the limitations established
by §§ 21.83(h), 91.317, and 121.207 of this
chapter.
[Doc. No. 5085, 29 FR 14571, Oct. 24, 1964, as
amended by Amdt. 21–12, 31 FR 13389, Oct. 15,
1966; Amdt. 21–66, 54 FR 34329, Aug. 18, 1989;
Amdt. 21–92, 74 FR 53390, Oct. 16, 2009]
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