149
Federal Aviation Administration, DOT
§ 21.85
is no feature, characteristic, or condi-
tion that would make the aircraft un-
safe when operated in accordance with
the limitations in paragraph (h) of this
section and §§ 91.317 and 121.207 of this
chapter.
(c) The applicant must apply for a
type certificate, in the transport cat-
egory, for the aircraft.
(d) The applicant must hold a U.S.
type certificate for at least one other
aircraft in the same transport category
as the subject aircraft.
(e) The FAA’s official flight test pro-
gram or the flight test program con-
ducted by the authorities of the coun-
try in which the aircraft was manufac-
tured, with respect to the issue of a
type certificate for that aircraft, must
be in progress.
(f) The applicant or, in the case of a
foreign manufactured aircraft, the
country in which the aircraft was man-
ufactured, must certify that—
(1) The aircraft has been designed and
constructed in accordance with the air-
worthiness requirements applicable to
the issue of the type certificate applied
for;
(2) The aircraft substantially com-
plies with the applicable flight char-
acteristic requirements for the type
certificate applied for; and
(3) The aircraft can be operated safe-
ly under the appropriate operating lim-
itations in this subchapter.
(g) The applicant must submit a re-
port showing that the aircraft has been
flown in all maneuvers necessary to
show compliance with the flight re-
quirements for the issue of the type
certificate and to establish that the
aircraft can be operated safely in ac-
cordance with the limitations in this
subchapter.
(h) The applicant must prepare a pro-
visional aircraft flight manual con-
taining all limitations required for the
issue of the type certificate applied for,
including limitations on weights,
speeds, flight maneuvers, loading, and
operation of controls and equipment
unless, for each limitation not so es-
tablished, appropriate operating re-
strictions are established for the air-
craft.
(i) The applicant must establish an
inspection and maintenance program
for the continued airworthiness of the
aircraft.
(j) The applicant must show that a
prototype aircraft has been flown for at
least 100 hours. In the case of an
amendment to a provisional type cer-
tificate, the FAA may reduce the num-
ber of required flight hours.
[Amdt. 21–12, 31 FR 13386, Oct. 15, 1966, as
amended by Amdt. 21–66, 54 FR 34329, Aug. 18,
1989]
§ 21.85
Provisional amendments to
type certificates.
(a) An applicant who manufactures
aircraft within the United States is en-
titled to a provisional amendment to a
type certificate if he shows compliance
with this section and the FAA finds
that there is no feature, characteristic,
or condition that would make the air-
craft unsafe when operated under the
appropriate limitations contained in
this subchapter.
(b) An applicant who manufactures
aircraft in a foreign country with
which the United States has an agree-
ment for the acceptance of those air-
craft for export and import is entitled
to a provisional amendment to a type
certificate if the country in which the
aircraft was manufactured certifies
that the applicant has shown compli-
ance with this section, that the air-
craft meets the requirements of para-
graph (e) of this section and that there
is no feature, characteristic, or condi-
tion that would make the aircraft un-
safe when operated under the appro-
priate limitations contained in this
subchapter.
(c) The applicant must apply for an
amendment to the type certificate.
(d) The FAA’s official flight test pro-
gram or the flight test program con-
ducted by the authorities of the coun-
try in which the aircraft was manufac-
tured, with respect to the amendment
of the type certificate, must be in
progress.
(e) The applicant or, in the case of
foreign manufactured aircraft, the
country in which the aircraft was man-
ufactured, must certify that—
(1) The modification involved in the
amendment to the type certificate has
VerDate Sep<11>2014
12:50 Apr 30, 2019
Jkt 247046
PO 00000
Frm 00159
Fmt 8010
Sfmt 8002
Y:\SGML\247046.XXX
247046
spaschal on DSK3GDR082PROD with CFR