Commonwealth Consolidated Regulations Commonwealth Consolidated Regulations(regulation 6A)
| Column 1 Item No. | Column 2 Type of Aircraft | Column 3 Provisions of the Annex for noise levels | Column 4 Provisions of the Annex for test procedure |
|---|---|---|---|
| 1 | Subsonic jet aircraft requiring a runway length (with
no stopway or clearway) of 610 metres or less at maximum certificated mass for
airworthiness for which: (a) the application for a certificate of airworthiness for the prototype was accepted by the certificating authority; or (b) another equivalent prescribed procedure was carried out by the certificating authority; before 6 October 1977 | 2.2, 2.4,
2.5 | 2.2, 2.3, 2.6, Appendix 1 |
| 2 | Subsonic jet aircraft powered by engines
with a by-pass ratio of 2 or more and for which a certificate of airworthiness
for the individual aircraft was first issued before 1 March 1972 | 2.2,
2.4, 2.5 | 2.2, 2.3, 2.6 Appendix 1 |
| 3 | Subsonic jet aircraft powered by
engines with a by-pass ratio of less than 2: (a) for which: (i) the application for a certificate of airworthiness for the prototype was accepted by the certificating authority; or (ii) another equivalent prescribed procedure was carried out by the certificating authority; before 1 January 1969; and (b) for which a certificate of airworthiness for that aircraft was first issued before 1 January 1976 | 2.2, 2.4, 2.5 | 2.2, 2.3, 2.6, Appendix 1 |
| 4 | Subsonic
jet aircraft, including derived versions, requiring a runway length
(with no stopway or clearway) of 610 metres or less at maximum
certificated mass for airworthiness, for which: (a) the application for a certificate of airworthiness for the prototype was accepted by the certificating authority; or (b) another equivalent prescribed procedure was carried out by the certificating authority; on or after 6 October 1977 | 3.2, 3.4, 3.5 | 3.2, 3.3, 3.6, 3.7 Appendix 2 |
| 5 |
Derived version of a subsonic jet aircraft for which: (a) the application for a certificate of airworthiness for the prototype was carried out by the certificating authority before 6 October 1977, or (b) another equivalent prescribed procedure was carried out by the certificating authority before 26 November 1981 | 2.2, 2.4, 2.5 | 2.2,
2.3, 2.6, Appendix 1 |
| 6 | Propeller-driven aircraft, including
derived versions, of a maximum certified take-off mass exceeding 5,700
kg, for which: (a) the application for a certificate of airworthiness for the prototype was accepted by the certificating authority; or (b) another equivalent prescribed procedure was carried out by the certificating authority; before 6 October 1977 | 5.2, 5.4, 5.5 | 5.2,
5.3, 5.6, 5.7, Appendix 2 |
| 7 | Propeller-driven aircraft, including
derived versions, of a maximum certificated take-off mass exceeding
5,700 kg, requiring a runway length (with no stopway or clearway) of
610 metres or less at maximum certificated mass for airworthiness, and
for which: (a) the application for a certificate of airworthiness for the prototype was accepted by the certificating authority; or (b) another equivalent prescribed procedure was carried out by the certificating authority; on or after 6 October 1977 and before 1 January 1985 | 5.2, 5.4, 5.5 | 5.2, 5.3, 5.6, 5.7 Appendix 2 |
| 8 |
Propeller-driven aircraft of a maximum certificated take-off mass not
exceeding 9,000 kg for which: (a) the application for a certificate of airworthiness for the prototype was accepted by the certificating authority; or (b) another equivalent prescribed procedure was carried out by the certificating authority; before 1 January 1975 | 6.2, 6.3 | 6.2, 6.4, 6.5, Appendix 3 |
| 9 | Propeller-driven
aircraft of a maximum certificated take-off mass not exceeding 9,000
kg for which a certificate of airworthiness for that aircraft was
first issued before 1 January 1980 | 6.2, 6.3 | 6.2, 6.4, 6.5,
Appendix 3 |
| 10 | Helicopters designed exclusively for external load
carrying purposes for which: (a) the application for a certificate of airworthiness for the prototype was accepted by the certificating authority; or (b) another prescribed procedure was carried out by the certificating authority; on or after 1 January 1985 | 8.2, 8.4, 8.5 | 8.2, 8.3, 8.6, 8.7, Appendix 4 |
| 11 | Helicopters
for which: (a) the application for a certificate of airworthiness for the prototype was accepted by the certificating authority; or (b) another equivalent prescribed procedure was carried out by the certificating authority; before 1 January 1985 | 8.2, 8.4, 8.5 | 8.2,
8.3, 8.6, 8.7, Appendix 4 |
| 12 | Helicopters for which: (a) an application for a change of type design was accepted by the certificating authority; or (b) another equivalent prescribed procedure was carried out by the certificating authority; before 17 November 1988 | 8.2, 8.4, 8.5 | 8.2, 8.3, 8.6, 8.7, Appendix 4 |
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