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of the aeroplane and the other by a person who holds a commercial pilot
(aeroplane) licence or an air transport pilot (aeroplane) licence with:
(i) an endorsement for that type of aeroplane; and
(ii) at least a co-pilot (aeroplane) instrument rating.
4.1C If the automatic pilot fitted to an aeroplane engaged:
(a) in charter operations; or
(b) in aerial work operations as an air ambulance or for a flying doctor
service;
loses a capability referred to in paragraph 4.1A, the aeroplane may, if the pilot
is satisfied that it is safe to do so, be operated under the Instrument Flight
Rules by a single pilot at any time within the period of 3 days commencing on
the day on which the automatic pilot loses the capability.
4.1D Paragraphs 4.1A, 4.1B and 4.1C apply in addition to, and not in derogation of,
paragraph 4.1.
4.2 A helicopter shall not be operated under the Instrument Flight Rules unless it is
equipped with:
(a) the flight and navigation instruments specified in Appendixes VII, VIII, or
IX to this section as applicable; and
(b) any other instruments, indicators or equipment specified in the helicopter
flight manual; and
(c) the minimum lighting equipment specified in Appendix V to this section;
and
(d) an approved automatic pilot, or automatic stabilisation system, for other
than night VFR flights except that in the case of such flight which will
involve more than 30 minutes flight over water or over land areas where
aircraft altitude cannot be maintained by reference to ground lighting, an
approved autostabilisation system or a 2 pilot crew shall be carried.
Note: Because of considerable variation in the individual stability characteristics of
different helicopter types and in the associated automatic pilot and automatic
stabilisation systems approved by the certification authority in the country of
certification, it is not possible to detail precise specifications for this equipment. This
consideration also applies to the flight crew complement. Accordingly each application
for approval to conduct I.F.R category operations will be individually assessed on the
basis of the specific helicopter type and its associated automatic pilot or
autostabilisation equipment and the proposed operating environment.
SECTION 20.18 -4-
Issue 9
Issue 9: 8 December 2004
Amdt No. 222
5 WINDSHIELD CLEAR VISION EQUIPMENT
An aircraft shall not be operated under the Visual or Instrument Flight Rules
unless it is equipped with a means of clearing precipitation from the outside of
the flight compartment windshield at a rate which will ensure that during heavy
precipitation each pilot has an unobstructed view through the windshield
except that, for aeroplanes less than 5 700 kg maximum take-off weight and
helicopters less than 2 750 kg maximum take-off weight, this equipment need
not be fitted if evidence can be produced to the satisfaction of CASA that the
windshield has been designed in such a manner that moderate rain conditions
do not unduly impair the view of the flight path in normal flight and while
taking-off or landing.
Note: Manually operated devices shall not be deemed to meet the requirements of this
paragraph.
6 RECORDING EQUIPMENT
6.1 An aircraft of maximum take-off weight:
(a) In excess of 5 700 kg and which is:
(i) turbine powered; or
(ii) of a type first certificated in its country of manufacture on or after 1
July 1965;
shall not be flown (except in agricultural operations) unless it is equipped
with an approved flight data recorder and an approved cockpit voice
recorder system;
(b) Less than or equal to 5 700 kg and which is:
(i) pressurised; and
(ii) turbine powered by more than 1 engine; and
(iii) of a type certificated in its country of manufacture for operation with
more than eleven places; and
(iv) issued with its initial Australian Certificate of airworthiness after 1
January 1988;
shall not be flown unless it is equipped with an approved cockpit voice
recorder system.
6.1A Paragraph 6.1 does not apply to an aircraft for which there is in force an
airworthiness certificate in the agricultural category or the restricted category.
6.2 The flight data recorder and cockpit voice recorder systems installed in an
aircraft under this section:
(a) must comply with the requirements of section 103.19 and 103.20
respectively; and
(b) will be considered for approval when CASA has equipment available
allowing replay of the recordings.
-5- SECTION 20.18
Issue 9
Issue 9: 8 December 2004
Amdt No. 222
6.3 Where an aircraft is required to be so equipped by this section, the flight data
　
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