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requirements specified in the certification standards that apply to the
aircraft.
10.6 The unit required to be carried on an aircraft under subparagraph 10.1 (b) may
be included in the number determined under paragraph 10.4.
Issue 6: 8 December 2004
Amdt No. 206
CIVIL AVIATION ORDERS
PART 20
SECTION 20.6
Issue 4
CONTINUATION OF FLIGHT BY MULTI-ENGINE
AIRCRAFT WITH 1 OR MORE ENGINES INOPERATIVE
SUBSECTIONS
2 Application 3 Requirements
2 APPLICATION
This section applies to all Australian aircraft.
3 REQUIREMENTS
3.1 When an engine of an aircraft fails in flight or where the rotation of an engine
of an aircraft is stopped in flight as a precautionary measure to prevent possible
damage, the pilot in command shall notify the nearest Air Traffic Services Unit
immediately, giving all relevant information and stating the action he or she
intends to take in regard to the conduct of the flight.
3.2 The pilot in command of a multi-engine aircraft in which 1 engine fails or the
rotation thereof is stopped, may proceed to an aerodrome of his or her selection
instead of the nearest suitable aerodrome if, upon consideration of all relevant
factors, he or she deems such action to be safe and operationally acceptable.
These factors shall include the following:
(a) nature of the malfunctioning and the possible mechanical difficulties
which may be encountered if the flight is continued;
(b) availability of the inoperative engine to be used;
(c) altitude, aircraft weight, and usable fuel at the time of engine stoppage;
(d) distance to be flown coupled with the performance availability should
another engine fail;
(e) relative characteristics of aerodromes available for landing;
(f) weather conditions en route and at possible landing points;
(g) air traffic congestion;
(h) type of terrain;
(i) familiarity of the pilot with the aerodrome to be used.
Issue 4: 8 December 2004
Amdt No. 207
SECTION 20.6 -2-
Issue 4
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Issue 4: 8 December 2004
CIVIL AVIATION ORDERS
PART 20
SECTION 20.7.0
Issue 4
AEROPLANE WEIGHT LIMITATIONS — GENERAL
SUBSECTIONS
2 Application
3 Definitions
4 Declared Density Altitude
Charts
Appendixes I, II and III
2 APPLICATION
This section applies to aeroplanes engaged in private, aerial work, charter and
regular public transport operations.
3 DEFINITIONS
Ambient Conditions: Atmospheric temperature, pressure and wind conditions
prevailing at a particular aerodrome during the period of 15 minutes preceding
the take-off of the aeroplane.
Forecast Conditions: Atmospheric temperature and pressure conditions
forecast for the aerodrome of destination, and its alternate if applicable, by an
authorised meteorological officer within:
(a) 1 hour of the time of take-off of the aeroplane engaged on a flight within
Australian Territory; and
(b) 2 hours of the time of take-off of an aeroplane engaged on an international
flight;
and used for the purpose of determining weight limitations of that aeroplane
for landing at that aerodrome on that flight.
Declared Conditions: Atmospheric temperature, pressure or density altitude
conditions declared by CASA as acceptable for a particular aerodrome for the
purpose of determining weight limitations for take-off or for landing.
Declared Weights: Weights determined for the use of declared conditions for a
particular aerodrome.
Developmental Air Service: An air service which due to the nature of
operational and economic considerations, has been declared by CASA to be a
developmental service.
Corrected Effective Operational Length: A length of runway — including
over-run — expressed in feet, corrected for slope, runway surface, and
approaches, declared by CASA as usable for take-off or landing by a particular
aeroplane. For the purpose of computing take-off and landing weights the
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Amdt No. 208
SECTION 20.7.0 -2-
Issue 4
corrected effective operational length shall be determined by reference to
Aeronautical Information Publications, subject to variations contained in
NOTAMS.
Main Runway: The runway with the greatest corrected effective operational
length.
Subsidiary Runway: Any runway on an aerodrome other than the main
runway.
4 DECLARED DENSITY ALTITUDE CHARTS
Declared density altitude charts are provided as follows:
Summer Season Appendix 1
Winter Season Appendix 2
Autumn-Spring Seasons Appendix 3
These charts shall be used when weights are determined by the use of declared
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