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required by the airworthiness standards mentioned in Parts 22,
23, 25, 26, 27, 29, 31, 32, 33 and 35 and as specified in the
applicable airworthiness criteria for special classes of aircraft
mentioned in subregulation 21.017 (2);
(e) for primary and intermediate category aircraft, if maintenance on
the aircraft is to be carried out by an appropriately rated and
trained pilot-owner — a special inspection and preventive
maintenance program designed to be accomplished by the pilotowner;
(f) any other data necessary to allow, by comparison, the
determination of the airworthiness of later aircraft, aircraft
engines or propellers of the same type.
(2) The type design for an aircraft, aircraft engine or propeller type
certificated under regulation 21.029 consists of the following:
(a) the drawings and specifications, and a listing of those drawings
and specifications, necessary to define the configuration and the
design features of the aircraft, aircraft engine or propeller shown
to comply with the airworthiness standards applicable to it under
regulation 21.17;
(b) information on dimensions, materials, and processes necessary to
define the structural strength of the aircraft, aircraft engine or
propeller;
(c) the airworthiness limitations section of the instructions for
continued airworthiness as required by the airworthiness
standards mentioned in Parts 22, 23, 25, 26, 27, 29, 31, 32, 33
and 35, or as otherwise required by CASA and as specified in the
applicable airworthiness criteria for special classes of aircraft
mentioned in subregulation 21.017 (2);
(d) the operating limitations and other information necessary for the
safe operation of the aircraft, aircraft engine or propeller as
required by the airworthiness standards mentioned in Parts 22,
23, 25, 26, 27, 29, 31, 32, 33 and 35, and as specified in the
applicable airworthiness criteria for special classes of aircraft
mentioned in subregulation 21.017 (2);
(e) for primary category aircraft, if maintenance on the aircraft is to
be carried out by an appropriately rated and trained pilot-owner
— a special inspection and preventive maintenance program
designed to be accomplished by the pilot-owner;
(f) any other data necessary to allow, by comparison, the
determination of the airworthiness of later aircraft, aircraft
engines or propellers of the same type.
(3) The type design for an aircraft type certificated under regulation
21.029A consists of the type design that was accepted by the NAA of
the recognised country that issued the foreign type certificate for the
aircraft.
Source FARs section 21.31 modified.
Civil Aviation Safety Regulations 1998 (CASR)
Office of Legal Counsel CASR
Civil Aviation Safety Authority 1st Edition – January 2003
Part 21 — 28
21.033 Inspection and tests
(1) CASA is not required to issue, under regulation 21.013A, a type
certificate for an aircraft, aircraft engine or propeller unless the
applicant allows CASA to make any inspection and any flight and
ground test necessary to determine that the aircraft, aircraft engine or
propeller complies with the applicable requirements of these
regulations. However:
(a) no aircraft, aircraft engine, propeller, or part thereof may be
presented to CASA for test unless compliance with paragraphs
(2) (b), (c) and (d) has been shown for that aircraft, aircraft
engine, propeller, or part thereof; and
(b) no change may be made to an aircraft, aircraft engine, propeller,
or part thereof between the time that compliance with paragraphs
(2) (b), (c) and (d) is shown for that aircraft, aircraft engine,
propeller, or part thereof and the time that it is presented to
CASA for test.
(2) Each applicant must make all inspections and tests necessary to
determine:
(a) compliance with the applicable airworthiness requirements; and
(b) that the aircraft, aircraft engine or propeller and its materials
conform to the specifications in the type design; and
(c) that parts of the aircraft, aircraft engine or propeller conform to
the drawings in the type design; and
(d) that the manufacturing processes, construction and assembly
conform to those specified in the type design.
(3) For an aircraft with not more than 2 seats, a maximum take-off
weight not exceeding 750 kg and a 45 knots or less VS0 stall speed as
defined in FARs section 23.49 that is to be type certificated in the
primary category or intermediate category, an authorised person may
make any determination, inspection, flight test or ground test
necessary to establish whether the aircraft complies with the
applicable requirements of these regulations.
　
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