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Regulations 1998.
14.2 Procedures to be followed consistent with this Order, including procedures
anticipating engine failure at any time between the commencement of take-off
and completion of landing, must be specified in the Operator’s Operation
Manual. The procedures so specified must be such that they can be consistently
executed in service by flight crews of average skill and they must also be such
that the take-off flight path with all engines operating is above the one-engine
inoperative take-off flight path.
TRANSITIONAL AND SAVINGS
1. Clause 5 of Civil Aviation Amendment Order (No. 2) 2002 reads as follows:
“5 Transitional
5.1 An approval given under paragraph 13.3 of section 20.7.1B of the Civil
Aviation Orders (the Orders) to operate a twin-engined aeroplane on passenger
carrying regular public transport operations that was in force immediately
-13- SECTION 20.7.1B
Issue 5
Issue 5: 11 June 2005
Amendment No. 227
before the commencement of subsection 3B of section 82.0 of the Orders is
taken to continue in force as if subsection 13 of section 20.7.1B and
Appendixes I and II to that section were still in force.
5.2 A twin-engined aeroplane that was being operated in accordance with
paragraph 13.4 of section 20.7.1B, but not in accordance with an approval
given under paragraph 13.6, immediately before the commencement of
subsection 3B of section 82.0, may continue to be operated in accordance with
paragraph 13.4 as if subsection 13 of section 20.7.1B and Appendixes I and II
to that section were still in force.
5.3 A twin-engined aeroplane that was being operated in accordance with an
approval given under paragraph 13.6 of section 20.7.1B, that was in force
immediately before the commencement of subsection 3B of section 82.0, may
continue to be operated in accordance with that approval as if subsection 13 of
section 20.7.1B and Appendixes I and II to that section were still in force
together with the airworthiness directive issued by CASA and known as
AD/General/69.
SECTION 20.7.1B -14-
Issue 5
Issue 5: 11 June 2005
Amendment No. 227
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CIVIL AVIATION ORDERS
PART 20
SECTION 20.7.2
Issue 4
AEROPLANE WEIGHT AND PERFORMANCE LIMITATIONS —
MULTI-ENGINE AEROPLANES NOT ABOVE 5700 KG —
REGULAR PUBLIC TRANSPORT OPERATIONS
SUBSECTIONS
1 Application
2 Definitions
3 Take-off performance
limitations
4 Take-off obstacle clearance
limitations
5 Route limitations
6 Landing limitations
7 Unserviceable equipment
8 Compliance
1 APPLICATION
Unless CASA otherwise directs, this section applies to all multi-engine
aeroplanes having a maximum take-off weight not in excess of 5 700kg
engaged in regular public transport operations.
2 DEFINITIONS
In this section, terms and abbreviations have the meanings defined in section
20.7.1B, and in Part 101 except that:
take-off distance available means the length of take-off run available plus,
where clearway is provided, a maximum of 60 metres of clearway.
3 TAKE-OFF PERFORMANCE LIMITATIONS
3.1 No aeroplane shall take off at a weight in excess of the take-off weight
specified in the aeroplane flight manual for the take-off distance available. In
determining this weight, account shall be taken of the aerodrome pressure
altitude, ambient temperature, runway surface and slope, and the wind velocity
at the time of take-off.
3.2 No aeroplane shall take off at a weight such that, allowing for normal
consumption of fuel in flight to the destination and alternate aerodromes, the
weight on arrival would exceed the weight specified in the aeroplane flight
manual with respect to baulked landing climb performance. In determining this
weight, account shall be taken of the aerodrome pressure altitude and, for
aeroplanes having a maximum take-off weight exceeding 3 500 kg the ambient
temperature forecast for the estimated time of landing.
Issue 4: 8 December 2004
Amdt No. 211
SECTION 20.7.2 -2-
Issue 4
3.3 No aeroplane shall take off at a weight such that, allowing for normal
consumption of fuel in flight to the destination and alternate aerodromes, the
weight on arrival would require a landing distance, in accordance with the
aeroplane flight manual, greater than the landing distance available:
(a) on the most favourable runway under zero wind conditions, unless that
runway would be unusable due to an excessive crosswind forecast for the
estimated time of landing then;
(b) on the most suitable available runway, using wind components derived
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