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aircraft.
(3) The manufacturer must submit a statement that the aircraft conforms
to the type design corresponding to the provisional type certificate
and has been found by the manufacturer to be in safe operating
condition under all applicable limitations.
(4) The aircraft must be flown at least five hours by the manufacturer.
(5) The aircraft must be supplied with a provisional aircraft flight manual
or other document and appropriate placards containing the limitations
mentioned in subregulation 21.081 (4) of these regulations and
regulation 262AO of CAR.
Source FARs section 21.221 modified.
21.223 Class II provisional certificates of airworthiness
(1) Except as provided in regulation 21.225, an applicant who holds a
Class II provisional type certificate for an aircraft is entitled to a Class
II provisional certificate of airworthiness for the aircraft if:
(a) the applicant meets the eligibility requirements of regulation
21.213; and
(b) CASA is satisfied that the requirements of this regulation are
satisfied and that there is no feature, characteristic, or condition
of the aircraft that would make the aircraft unsafe when operated
in accordance with the limitations mentioned in subregulation
21.083 (7) of these regulations and regulation 262AO of CAR.
(2) The applicant must show that a Class II provisional type certificate
for the aircraft has been issued to the manufacturer.
(3) The applicant must submit a statement by the manufacturer that the
aircraft has been manufactured under a quality system adequate to
ensure that the aircraft conforms to the type design corresponding
with the provisional type certificate.
(4) The applicant must submit a statement that the applicant has found
the aircraft to be in a safe operating condition under the applicable
limitations.
(5) The aircraft must be flown at least five hours by the manufacturer.
(6) The aircraft must be supplied with a provisional aircraft flight manual
containing the limitations mentioned in subregulation 21.083 (7) of
these regulations and regulation 262AO of CAR.
Source FARs section 21.223 modified.
Civil Aviation Safety Regulations 1998 (CASR)
CASR Office of Legal Counsel
1st Edition – January 2003 Civil Aviation Safety Authority
Part 21 — 89
21.225 Provisional certificates of airworthiness corresponding with
provisional amendments to type certificates
(1) An applicant is entitled to a Class I or a Class II provisional
certificate of airworthiness for an aircraft for which a provisional
amendment to the type certificate has been issued, if:
(a) the applicant meets the eligibility requirements of regulation
21.213; and
(b) CASA is satisfied that the requirements of this regulation are
satisfied and that there is no feature, characteristic, or condition
of the aircraft, as modified in accordance with the provisionally
amended type certificate, that would make the aircraft unsafe
when operated in accordance with the applicable limitations
mentioned in subregulation 21.085 (6) of these regulations and
regulation 262AO of CAR.
(2) The applicant must show that the modification was made under a
quality system adequate to ensure that the modification conforms to
the provisionally amended type certificate.
(3) The applicant must submit a statement that the applicant has found
the aircraft to be in a safe operating condition under the applicable
limitations.
(4) The aircraft must be flown at least five hours by the manufacturer.
(5) The aircraft must be supplied with a provisional aircraft flight manual
or other document and appropriate placards containing the limitations
mentioned in subregulation 21.085 (6) of these regulations and
regulation 262AO of CAR.
Source FARs section 21.225 modified.
Civil Aviation Safety Regulations 1998 (CASR)
Office of Legal Counsel CASR
Civil Aviation Safety Authority 1st Edition – January 2003
Part 21 — 90
Subpart 21.J Delegation option authorisation procedures
21.231 Applicability
(1) This Subpart prescribes requirements for:
(a) obtaining and using a delegation option authorisation for type,
production, and airworthiness certification (as applicable) of the
following:
(i) small aeroplanes and small gliders;
(ii) normal category rotorcraft;
(iii) turbojet engines of not more than 4.45 kN thrust;
(iv) turbopropeller and reciprocating engines with a power
rating of not more than 373 kW;
(v) propellers manufactured for use on engines covered by
subparagraph (iv); and
(b) issuing authorised release certificates for engines, propellers, and
parts of products covered by paragraph (a).
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