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Source FARs section 21.16 modified.
21.017 Designation of applicable airworthiness standards
(1) An applicant for a type certificate for an aircraft mentioned in
regulation 21.021 or 21.025, or an aircraft engine or propeller, must
show that the aircraft, aircraft engine or propeller meets:
(a) the applicable requirements of this Part, and of the airworthiness
standards mentioned in Parts 22, 23, 25, 27, 29, 31, 32, 33 and 35,
that are effective on the date of application for that certificate
unless:
(i) otherwise specified by CASA; or
(ii) compliance with later effective amendments is elected or
required under this regulation; and
(b) any special conditions imposed under regulation 21.16.
(2) For special classes of aircraft (airships and other non-conventional
aircraft), including the engines and propellers installed thereon, for
which airworthiness standards have not been prescribed in these
regulations, the airworthiness standards are the portions of those
airworthiness standards mentioned in Parts 22, 23, 25, 27, 29, 31, 32,
33 and 35 that CASA considers to be appropriate for the aircraft and
applicable to a specific type design, or such airworthiness criteria as
CASA may consider provide an equivalent level of safety to those
Parts.
(3) An application for type certification of a transport category aircraft is
effective for 5 years, and an application for any other type certificate is
effective for 3 years, unless an applicant shows, before the application
lapses, that the aircraft requires a longer period of time for design,
development, and testing, and CASA approves a longer period.
(4) If an application ceases to be effective, the applicant may:
(a) file a new application for a type certificate and comply with all
the provisions of subregulation (1) applicable to an original
application; or
(b) file for an extension of the original application and comply with
the applicable airworthiness requirements of these regulations
that were effective on a date, to be selected by the applicant, not
earlier than the date which precedes the date of issue of the type
certificate by the time limit established under subregulation (3)
for the original application.
Civil Aviation Safety Regulations 1998 (CASR)
Office of Legal Counsel CASR
Civil Aviation Safety Authority 1st Edition – January 2003
Part 21 — 16
(5) If an applicant elects to comply with an amendment to these regulations,
or to any matter incorporated by reference in these regulations, that is
effective after the filing of the application for a type certificate, the
applicant must also comply with any other amendment or incorporated
matter that CASA considers is directly related to the application.
(6) For primary category aircraft, the airworthiness standards are the
airworthiness standards mentioned in Part 26 or such other
airworthiness criteria that CASA considers are appropriate to the
specific design and intended use and provide a level of safety
acceptable to CASA when the aircraft is operated under the
conditions stated in its type certification basis.
(7) For intermediate category aircraft, the airworthiness standards are the
airworthiness standards mentioned in Part 26 or such other
airworthiness criteria that CASA considers are appropriate to the
specific design and intended use and provide a level of safety
acceptable to CASA when the aircraft is operated under the
conditions stated in its type certification basis.
(8) If an airworthiness standard has been agreed by CASA or one of its
predecessors after 30 September 1993 as a response to a design
advice mentioned in section 100.3 or 100.6 of the Civil Aviation
Orders, the standard continues to apply until 5 years after the date of
approval of the design advice, unless the applicant elects to comply
with a later standard.
Source FARs section 21.17 modified.
21.019 Changes requiring a new type certificate
(1) A type certificate for an aircraft, aircraft engine or propeller ceases to
apply to an aircraft, aircraft engine or propeller of that type if:
(a) a change is made in the design configuration, power, power
limitations (engines), speed limitations (engines), or weight of
the aircraft, aircraft engine or propeller that is so extensive that a
substantially complete investigation of compliance with the
requirements applicable under regulation 21.017 is necessary in
the interests of aviation safety; or
Civil Aviation Safety Regulations 1998 (CASR)
CASR Office of Legal Counsel
1st Edition – January 2003 Civil Aviation Safety Authority
Part 21 — 17
(b) in the case of a normal, utility, acrobatic, commuter or transport
　
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