Commonwealth Numbered Regulations

1991 No. 408 AIR NAVIGATION (AERODROME CURFEW) REGULATIONS (AMENDMENT) - REG 10

  10.1   Add at the end:

                     "SCHEDULE                      Paragraph 6(1)(aa)

DESCRIPTIONS OF AIRCRAFT, NOISE LEVELS
AND TESTING PROCEDURES
Column 1  Column 2              Column 3         Column 4

Item No.  Description           Paragraphs       Paragraphs of Part II

          of Aircraft           of Part II       of, and Appendices to,

                                of the Annexe    the Annexe, (test

                                (noise levels)   procedures)

1         Propeller-driven      5.2, 5.4, 5.5     5.2, 5.3, 5.6, 5.7

          aircraft of a maximum                   Appendix 2

certificated take-off
mass exceeding
5,700 kg for which:

   (a)  the application
for a certificate
of air worthiness
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
2         Propeller-driven         6.2, 6.3            6.2, 6.4, 6.5,

          aircraft of a                                Appendix 3

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 17 November 1988
3         Propeller-driven           10.2, 10.4        10.2, 10.3,

          aircraft and their                           10.5, 10.6,

          derivatives of a maximum   Appendix 6

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;
on or after
17 November 1988
4      Propellor-driven           3.2, 3.4, 3.5           3.2, 3.3,

       aircraft of a                                      3.6, 3.7,

       maximum certificated                               Appendix 2".

take-off mass
exceeding 9,000 kg