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category aircraft, a change is made:
(i) in the number of its engines or rotors; or
(ii) to engines or rotors using different principles of propulsion
or to rotors using different principles of operation; or
(c) in the case of an aircraft engine — a change is made in the
principle of operation; or
(d) in the case of propellers — a change is made in the number of
blades or principle of pitch change operation.
(2) A person who proposes to make a change mentioned in subregulation
(1) may apply to CASA for a new type certificate for the aircraft,
aircraft engine or propeller.
Source FARs section 21.19 modified.
21.021 Type certificate: normal, utility, acrobatic, commuter, and
transport category aircraft; manned free balloons; special
classes of aircraft; aircraft engines; propellers
An applicant is entitled to a type certificate for an aircraft (except an
aircraft mentioned in regulation 21.027) in the normal, utility,
acrobatic, commuter, or transport category, or for a manned free
balloon, or for a special class of aircraft or an aircraft engine or
propeller, if:
(a) the applicant submits the type design, test reports, and
computations necessary to show that the aircraft, aircraft engine
or propeller to be certificated meets the applicable requirements
of this Part, the airworthiness standards mentioned in these
regulations and any conditions subject to which the type
certificate is to be issued; and
(b) CASA is satisfied that the type design and the aircraft, engine or
propeller meet the applicable requirements of this Part and the
airworthiness standards mentioned in these regulations, and any
airworthiness provisions not complied with are compensated for
by factors that provide an equivalent level of safety; and
(c) for an aircraft — CASA is satisfied the aircraft can reasonably be
expected to be safe for its intended use when it is operated under
any conditions limiting its intended use.
Source FARs section 21.21 modified.
Civil Aviation Safety Regulations 1998 (CASR)
Office of Legal Counsel CASR
Civil Aviation Safety Authority 1st Edition – January 2003
Part 21 — 18
21.024 Type certificate: primary category aircraft
(1) The applicant is entitled to a type certificate for an aircraft in the
primary category if:
(a) the aircraft:
(i) is unpowered; is an aeroplane powered by a single,
naturally aspirated engine with a 61 knots or less VS0 stall
speed as defined in FARs section 23.49; or is a rotorcraft
powered by a single, naturally aspirated engine with a
29.3 kgm-2 main rotor disc loading limitation, under sea
level standard day conditions; and
(ii) has a maximum take-off weight of not more than 1225 kg
or, if the aircraft is a seaplane, a maximum take-off weight
of not more than 1530 kg; and
(iii) has a maximum seating capacity of not more than 4
persons, including the pilot; and
(iv) has an unpressurised cabin; and
(b) the applicant has submitted to CASA:
(i) except as provided by subregulation (3), a statement, in a
form and manner acceptable to CASA, certifying that: the
applicant has completed the engineering analysis necessary
to demonstrate compliance with the applicable
airworthiness requirements; the applicant has conducted
appropriate flight, structural, propulsion, and systems tests
necessary to show that the aircraft, its components, and its
equipment are reliable and function properly; the type
design complies with the airworthiness standards
established for the aircraft under subregulation 21.017 (6);
and the aircraft can reasonably be expected to be safe for
its intended use when it is operated under any conditions
limiting its intended use; and
(ii) the flight manual required by regulation 21.005, including
any information required to be furnished by the applicable
airworthiness standards; and
(iii) instructions for continued airworthiness in accordance with
subregulation 21.050 (2); and
(iv) a report that: summarises how compliance with each
provision of the type certification basis was determined;
lists the specific documents in which the type certification
data information is provided; lists all necessary drawings
and documents used to define the type design; and lists all
the engineering reports on tests and computations the
applicant must retain and make available under regulation
21.049 to substantiate compliance with the applicable
airworthiness standards; and
Civil Aviation Safety Regulations 1998 (CASR)
CASR Office of Legal Counsel
1st Edition – January 2003 Civil Aviation Safety Authority
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