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reductions specified in this paragraph.
Note The net flight path and the gross flight path may be considered identical when the
aeroplane is in the take-off configuration described in paragraph 7.1.
7.6 In this section:
commuter type aeroplane means:
(a) a SFAR 41 aeroplane; or
(b) an aeroplane that is certificated as a commuter category aircraft.
SFAR 41 aeroplane means an aeroplane that:
(a) is certificated as a normal category aircraft; and
(b) is such that an applicant under part 4 (c) of SFAR No. 41 would be
entitled to a type certificate amendment or a supplemental type certificate
that shows compliance with Annex 8 to the Chicago Convention in
relation to the aeroplane; and
(c) is operated in accordance with a flight manual that specifies performance
standards that are at least equivalent to the standards set out in Annex 8 to
the Chicago Convention.
SFAR No. 41 means Special Federal Aviation Regulation No. 41 of the United
States of America.
8 EN-ROUTE CLIMB PERFORMANCE
8.1 The en-route climb performance of an aeroplane with the critical engine
inoperative is to be determined taking into account all normal operating
altitudes, operating weights, and anticipated temperatures.
8.2 The en-route climb performance of a three- or four-engined aeroplane with the
2 most critical engines inoperative is to be determined taking into account all
normal operating altitudes, operating weights, and anticipated temperatures.
SECTION 20.7.1B -8-
Issue 5
Issue 5: 11 June 2005
Amendment No. 227
8.3 In determining the net flight path of an aeroplane to show compliance with
subsection 12, the gross climb gradients established in accordance with
paragraph 8.1 must be reduced by 1.1% for twin-engined aeroplanes, 1.3% for
three-engined aeroplanes and 1.4% for four-engined aeroplanes. Similarly the
gross climb gradients established in accordance with paragraph 8.2 must be
reduced by 0.3% for three-engined aeroplanes and 0.5% for four-engined
aeroplanes.
9 APPROACH CLIMB PERFORMANCE
9.1 For paragraph 5.1 (b), the approach climb requirements are met if, in the
approach configuration with the critical engine inoperative at a speed not more
than 1.5 VS, an aeroplane has a gross gradient of climb of at least:
(a) for a twin-engined aeroplane — 2.1%; or
(b) for a 3 engined aeroplane — 2.3% or
(c) for a 4 engined aeroplane — 2.4%.
10 LANDING CLIMB PERFORMANCE
10.1 For the purposes of subparagraph 5.1 (c), the landing climb requirements are
met if, in the landing configuration an aeroplane has a gross gradient of climb
of not less than 3.2% at a climbing speed not in excess of 1.3 VS with all
engines operating.
11 LANDING DISTANCE REQUIRED
11.1 For subparagraph 5.1 (a), the landing distance for a jet-engined aeroplane is:
(a) for an aeroplane engaged in regular public transport operations when
landing on a dry runway, or in charter operations when landing on a dry or
wet runway — 1.67 times the distance required to bring the aeroplane to a
stop on a dry runway; or
(b) for an aeroplane engaged in regular public transport operations when
landing on a wet runway:
(i) 1.92 times the distance required to bring the aeroplane to a stop on a
dry runway; or
(ii) the distance set out in the flight manual or operations manual for
operations conducted on wet runways.
11.1.1 For the purposes of subparagraph 5.1 (a), the landing distance required in
relation to a propeller driven aeroplane that is engaged in regular public
transport, or charter, operations is:
(a) for a landing at a destination aerodrome:
(i) when the runway is dry — a distance equal to 1.43 times the distance
required to bring the aeroplane to a stop; or
(ii) when the runway is wet — a distance equal to 1.67 times the
distance required to bring the aeroplane to a stop; and
-9- SECTION 20.7.1B
Issue 5
Issue 5: 11 June 2005
Amendment No. 227
(b) for a landing at an alternate aerodrome — 1.43 times the distance required
to bring the aeroplane to a stop.
11.1.2 Subject to paragraph 11.2, the landing distance required under paragraph 11.1
or 11.1.1 must be determined using information set out in the flight manual.
11.2 For a landing on a contaminated runway, the landing distance required is:
(a) subject to paragraph 11.3, the distance set out in the flight manual or the
operations manual for operations conducted on contaminated runways; or
(b) the distance approved by CASA for operations conducted on runways
covered by slush, snow or a depth of water.
11.3 For subparagraph 4.1 (d) and paragraph 5.1, an aeroplane engaged in private,
　
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