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assumption on which the aeroplane flight manual data is established, is a
permissible unserviceability, then the operations manual shall contain
information to permit such adjustments to take-off weights, landing weights or
distances required, as are necessary to maintain the intended level of safety of
operations.
Issue 4: 8 December 2004
Amdt No. 211
SECTION 20.7.2 -4-
Issue 4
7.2 The information required by paragraph 7.1 shall be subject to approval by
CASA before being used in operations.
8 COMPLIANCE
8.1 Procedures to show compliance with this section shall be determined by the
operator to the satisfaction of CASA and shall be included in the operations
manual.
8.2 A pilot in command shall be considered to have complied with this section if
the aeroplane he commands is operated in accordance with the relevant
procedures and at the weights permitted by an operations manual provided in
pursuance of the Civil Aviation Regulations 1988 for the particular operation.
Note: Documents which are required to be carried in an aircraft, such as the flight manual for
the aircraft, may form part of an operations manual.
Issue 4: 8 December 2004
Amdt No. 211
CIVIL AVIATION ORDERS
PART 20
SECTION 20.7.4
Issue 4
AEROPLANE WEIGHT AND PERFORMANCE LIMITATIONS —
AEROPLANES NOT ABOVE 5 700 KG — REGULAR PUBLIC
TRANSPORT OPERATIONS (SINGLE-ENGINE AEROPLANES ONLY),
CHARTER OPERATIONS, AERIAL WORK (EXCLUDING AGRICULTURAL)
OPERATIONS AND PRIVATE OPERATIONS
SUBSECTIONS
2 Application
3 Definitions
4 Take-off weight limitations
5 Landing weight limitations
6 Take-off distance required
7 Take-off climb performance
8 En-route climb performance
9 Landing climb performance
10 Landing distance required
12 Aeroplane configuration and
procedures
2 APPLICATION
This section applies to aeroplanes having a maximum take-off weight not in
excess of 5700 kg engaged in regular public transport operations (single-engine
aeroplanes only), private operations, aerial work operations (excluding
agricultural operations) and charter operations, unless CASA specifies that
sections 20.7.1 or 20.7.2 are to be applied.
3 DEFINITIONS
3.1 In this section:
approved foreign flight manual, in relation to an aeroplane, means the flight
manual approved by the relevant regulatory aviation authority of the country
where the aeroplane is, or was, manufactured.
landing distance available means the distance specified by CASA as being the
effective operational length available for use by aircraft for landing at
Government and Licensed Aerodromes or the distance available for landing on
an authorised landing or alighting area.
manufacturer’s data manual, in relation to an aeroplane, means a publication
(however described) produced by the manufacturer of the aeroplane as a guide
for the flight crew in the operation of the aeroplane.
pressure height means the height registered on an altimeter with the sub-scale
set to 1013.2 hPa.
Issue 4: 8 December 2004
Amdt No. 212
SECTION 20.7.4 -2-
Issue 4
take-off safety speed means the speed specified on the aeroplane take-off chart
being the minimum speed to which an aeroplane must be accelerated in
establishing the take-off distance required.
take-off distance available means the distance specified by CASA as being the
effective operational length available for use by aircraft for take-off at
Government or Licensed Aerodromes or the distance available for take-off on
an authorised landing or alighting area.
VS is the symbol used to denote the minimum speed in a stall or the minimum
steady flight speed in the aeroplane configuration in which VS is being used.
4 TAKE-OFF WEIGHT LIMITATIONS
4.1 An aeroplane must not take off at a weight in excess of the least of the weights
determined in accordance with subparagraphs (a) to (d):
(a) a weight at which the take-off distance required under subsection 6 for the
pressure height, temperature, runway slope (if in excess of 1%) and wind
component along the runway, is equal to or less than the take-off distance
available in the direction of take-off. Approved declared conditions may
be used instead of actual pressure height and temperature;
(b) a weight which will permit compliance with the take-off climb
requirements specified in subsection 7 taking into account ambient
temperature and pressure height. Approved declared temperature and
pressure height may be used instead of ambient conditions;
(c) a weight which will permit compliance with the en-route climb
requirements specified in subsection 8;
　
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