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Note The distances and areas mentioned in the above definitions are normally declared to be
available by the national aviation authority. In Australia, they are specified in Aeronautical
Information Publications but may be the subject of a separate approval from CASA.
4 TAKE-OFF WEIGHT LIMITATIONS
4.1 For the purposes of paragraph 235 (2) (a) of the Regulations, the maximum
weight that an aeroplane to which this section applies may not exceed at
take-off is the least of the weights determined in accordance with
subparagraphs (a) to (d):
(a) a weight at which the take-off distance and accelerate-stop distance
required under subsection 6 for the aerodrome elevation, ambient
SECTION 20.7.1B -4-
Issue 5
Issue 5: 11 June 2005
Amendment No. 227
temperature, wind component along the runway, runway slope and runway
surface conditions at the time of take-off are equal to or less than the
take-off distance and accelerate-stop distance available in the direction of
take-off. Approved declared conditions may be used instead of the
ambient temperature and aerodrome elevation;
(b) a weight that will permit compliance with the take-off climb requirements
mentioned in subsection 7 taking into account either ambient temperature
and aerodrome elevation, or approved declared conditions;
(ba) a weight that will permit compliance with the obstacle clearance
requirements mentioned in paragraph 7.5 and subsection 12 for take-off
from a dry runway (whether it is dry or not), and taking into account either
wind conditions, ambient temperature and aerodrome elevation, or wind
conditions and approved declared conditions;
(c) a weight which will permit compliance with the en-route obstacle
clearance requirements specified in subsection 12;
(d) a weight which, allowing for normal consumption of fuel and oil in flight
to the destination and alternate aerodrome, will permit compliance with
the landing weight limitations mentioned in subsection 5.
5 LANDING WEIGHT LIMITATIONS
5.1 For the purposes of paragraph 235 (2) (b) of the Regulations, the maximum
weight which an aeroplane to which this section applies may not exceed at
landing is the least of the weights determined in accordance with
subparagraphs (a) to (c):
(a) a weight at which the landing distance required in accordance with
subsection 11 for the aerodrome elevation, wind component along the
runway, runway slope (when exceeding 1%) and runway surface
conditions at the time of landing, is equal to or less than the landing
distance available in the direction of landing;
(b) a weight which will permit compliance with the approach climb
requirements specified in subsection 9, taking into account forecast or
ambient temperature and aerodrome elevation or approved declared
conditions;
(c) a weight which will permit compliance with the landing climb
requirements specified in subsection 10 taking into account forecast or
ambient temperature and aerodrome elevation or approved declared
conditions.
6 ACCELERATE-STOP AND TAKE-OFF DISTANCE REQUIRED
6.1 For subparagraph 4.1 (a), and subject to paragraphs 6.3.4 and 6.4, the
accelerate-stop distance required is the distance set out in the flight manual.
6.2.1 For subparagraph 4.1 (a), and subject to paragraphs 6.3.4 and 6.4, the take-off
distance required is the distance set out in the flight manual.
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Issue 5
Issue 5: 11 June 2005
Amendment No. 227
6.2.2 Subject to paragraph 6.4, if the take-off distance required at the take-off weight
selected by the pilot in command is greater than the take-off run available, the
pilot in command must ensure that:
(a) if the flight manual sets out information about take-off run required — the
take-off run required does not exceed the take-off run available; or
(b) if the flight manual does not set out information about take-off run
required — the take-off distance required does not exceed the take-off run
available by more than the lesser of 60 metres or the length of clearway
included in the take-off distance available.
6.3.1 For a take-off from a wet or contaminated runway, V1 may be less than V1
appropriate to a dry runway but not less than V1 (wet).
6.3.2 V1 (wet) must:
(a) allow the aeroplane to reach a height at least 15 feet above the runway
after the aeroplane has:
(i) suffered an engine failure that is recognised by the pilot at V1 (wet);
and
(ii) travelled a distance along the runway equal to the take-off distance
required; and
(b) subject to paragraph 6.4, be determined from the flight manual or the
operations manual for the aircraft; and
(c) not be less than the minimum control speed on the ground (Vmcg).
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