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10.1 Subject to paragraphs 10.3 and 10.4, an aeroplane must not land unless the
landing distance available is equal to or greater than the distance required to
bring the aeroplane to a complete stop or, in the case of aeroplanes operated on
water, to a speed of 3 knots, following an approach to land at a speed not less
than 1.3VS maintained to within 50 feet of the landing surface. This distance is
to be measured from the point where the aeroplane first reaches a height of 50
feet above the landing surface and must be multiplied by the following factors:
(a) 1.15 for aeroplanes with maximum take-off weights of 2 000 kg or less;
(b) 1.43 for aeroplanes with maximum take-off weights of 4 500 kg or
greater;
(c) for aeroplanes with maximum take-off weights between 2 000 kg and
4500 kg, a factor derived by linear interpolation between 1.15 and 1.43
according to the maximum take-off weight of the aeroplane.
10.2 For aeroplanes operated on land, landing distances are to be determined for a
level short dry grass surface. For aeroplanes operated on water, landing
distances are to be determined on flat broken water.
10.3 Subject to paragraph 10.4, where there is an approved foreign flight manual or
a manufacturer’s data manual for an aeroplane that sets out the landing
distance required for that aeroplane, then that aeroplane must be operated so as
to comply with the requirements set out in paragraphs 10.1 and 10.2 or the
requirements relating to landing distance set out in either of those manuals.
Note: The data contained in some manufacturers’ data manuals is unfactored and makes no
allowance for degraded aircraft performance. Where there is a considerable difference
between the data in a manufacturer’s data manual and the data in the flight manual for the
aeroplane then the manufacturer’s data should be treated with caution.
Issue 4: 8 December 2004
Amdt No. 212
-5- SECTION 20.7.4
Issue 4
10.4 This subsection does not apply in the case of an emergency.
12 AEROPLANE CONFIGURATION AND PROCEDURES
12.1 An operator of a multi-engined aeroplane engaged in charter operations or
aerial work operations, and an operator of a single-engine aeroplane engaged in
RPT operations under the Instrument Flight Rules, must include in his or her
operations manual the procedures to be followed by the pilot in the event of an
engine failure.
Issue 4: 8 December 2004
Amdt No. 212
SECTION 20.7.4 -6-
Issue 4
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Issue 4: 8 December 2004
Amdt No. 212
CIVIL AVIATION ORDERS
PART 20
SECTION 20.9
Issue 7
AIR SERVICE OPERATIONS —
PRECAUTIONS IN REFUELLING, ENGINE AND
GROUND RADAR OPERATIONS
SUBSECTIONS
2 Application
3 Fuels and oils
4 Fuelling of aircraft
5 Starting and ground operations
of engines
6 Ground operation of aircraft
radar equipment
Appendix I
2 APPLICATION
2.1 Subject to paragraph 2.2, this section applies to:
(a) all Australian aircraft operating on aerodromes in Australian territory; and
(b) as far as practicable — all Australian aircraft operating outside Australian
territory.
2.2 This section does not apply to an aircraft that is being refuelled in accordance
with:
(a) section 20.10, except as set out in subparagraph 1A.1 (a) of section 20.10;
and
(b) section 20.10.1, except as set out in subparagraph 2.2 (a) of section
20.10.1.
3 FUEL AND OILS
3.1 The pilot in command of an aircraft shall ensure that the aircraft is not flown
unless the aviation fuel, aircraft engine lubricating oil, aircraft engine power
augmentation fluid and aircraft hydraulic system fluid used in connection with
the servicing or operation of the aircraft complies with the specification and
grade required or approved for the purpose by CASA.
Note 1: In respect of aircraft engine power augmentation fluid and aircraft hydraulic system
fluid the specification and grade specified for a particular purpose in a manual or manuals
promulgated by the aircraft or aircraft engine manufacturer may be considered as having been
approved by CASA.
Note 2: The pilot in command may assume that:
(a) aviation fuel; and
(b) aircraft engine lubricating oil; and
(c) aircraft engine power augmentation fluid; and
(a) aviation fuel; and
(d) aircraft hydraulic system fluid in the aircraft, other than that which he has
caused to be delivered into the aircraft, complies with the required specification
and grade.
Issue 7: 8 December 2004
Amdt No. 213
SECTION 20.9 -2-
Issue 7
3.3 All ground fuel stock shall be carefully checked for the presence of
　
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