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137
Federal Aviation Administration, DOT
§ 21.25
(i) Except as provided by paragraph
(c) of this section, a statement, in a
form and manner acceptable to the
FAA, certifying that: the applicant has
completed the engineering analysis
necessary to demonstrate compliance
with the applicable airworthiness re-
quirements; the applicant has con-
ducted appropriate flight, structural,
propulsion, and systems tests nec-
essary to show that the aircraft, its
components, and its equipment are re-
liable and function properly; the type
design complies with the airworthiness
standards and noise requirements es-
tablished for the aircraft under
§ 21.17(f); and no feature or char-
acteristic makes it unsafe for its in-
tended use;
(ii) The flight manual required by
§ 21.5(b), including any information re-
quired to be furnished by the applicable
airworthiness standards;
(iii) Instructions for continued air-
worthiness in accordance with
§ 21.50(b); and
(iv) A report that: summarizes how
compliance with each provision of the
type certification basis was deter-
mined; lists the specific documents in
which the type certification data infor-
mation is provided; lists all necessary
drawings and documents used to define
the type design; and lists all the engi-
neering reports on tests and computa-
tions that the applicant must retain
and make available under § 21.49 to sub-
stantiate compliance with the applica-
ble airworthiness standards.
(3) The FAA finds that—
(i) The aircraft complies with those
applicable airworthiness requirements
approved under § 21.17(f) of this part;
and
(ii) The aircraft has no feature or
characteristic that makes it unsafe for
its intended use.
(b) An applicant may include a spe-
cial inspection and preventive mainte-
nance program as part of the aircraft’s
type design or supplemental type de-
sign.
(c) For aircraft manufactured outside
of the United States in a country with
which the United States has a bilateral
airworthiness agreement for the ac-
ceptance of these aircraft, and from
which the aircraft is to be imported
into the United States—
(1) The statement required by para-
graph (a)(2)(i) of this section must be
made by the civil airworthiness au-
thority of the exporting country; and
(2) The required manuals, placards,
listings, instrument markings, and
documents required by paragraphs (a)
and (b) of this section must be sub-
mitted in English.
[Doc. No. 23345, 57 FR 41367, Sept. 9, 1992; as
amended by Amdt. 21–75, 62 FR 62808, Nov. 25,
1997]
§ 21.25
Issue of type certificate: Re-
stricted category aircraft.
(a) An applicant is entitled to a type
certificate for an aircraft in the re-
stricted category for special purpose
operations if he shows compliance with
the applicable noise requirements of
Part 36 of this chapter, and if he shows
that no feature or characteristic of the
aircraft makes it unsafe when it is op-
erated under the limitations prescribed
for its intended use, and that the air-
craft—
(1) Meets the airworthiness require-
ments of an aircraft category except
those requirements that the FAA finds
inappropriate for the special purpose
for which the aircraft is to be used; or
(2) Is of a type that has been manu-
factured in accordance with the re-
quirements of and accepted for use by,
an Armed Force of the United States
and has been later modified for a spe-
cial purpose.
(b) For the purposes of this section,
‘‘special purpose operations’’ includes—
(1) Agricultural (spraying, dusting,
and seeding, and livestock and preda-
tory animal control);
(2) Forest and wildlife conservation;
(3) Aerial surveying (photography,
mapping, and oil and mineral explo-
ration);
(4) Patrolling (pipelines, power lines,
and canals);
(5) Weather control (cloud seeding);
(6) Aerial advertising (skywriting,
banner towing, airborne signs and pub-
lic address systems); and
(7) Any other operation specified by
the FAA.
[Doc. No. 5085, 29 FR 14564, Oct. 24, 1964, as
amended by Amdt. 21–42, 40 FR 1033, Jan. 6,
1975]
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