曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

conditions.
Issue 4: 8 December 2004
Amdt No. 208
-3- SECTION 20.7.0
Issue 4
APPENDIX I
Issue 4: 8 December 2004
Amdt No. 208
SECTION 20.7.0 -4-
Issue 4
APPENDIX II
Issue 4: 8 December 2004
Amdt No. 208
-5- SECTION 20.7.0
Issue 4
APPENDIX III
Issue 4: 8 December 2004
Amdt No. 208
SECTION 20.7.0 -6-
Issue 4
THIS PAGE INTENTIONALLY LEFT BLANK
Issue 4: 8 December 2004
Amdt No. 208
CIVIL AVIATION ORDERS
PART 20
SECTION 20.7.1
Issue 4
AEROPLANE WEIGHT LIMITATIONS —
AEROPLANES ABOVE 5700 KG —
ALL OPERATIONS (PISTON ENGINED)
SUBSECTIONS
1 Application
2 Take-off Weight Limitations
3 Landing Weight Limitations
Appendixes 1 and 2
1 APPLICATION
This section applies to piston-engined aeroplane types having a maximum
permissible all-up weight in excess of 5 700 kg and which were registered in
Australia prior to 1 June 1963.
2 TAKE-OFF WEIGHT LIMITATIONS
2.1 An aeroplane shall not take-off at a weight in excess of the weights determined
in accordance with subparagraphs 2.1.1 to 2.1.4 of these Orders:
2.1.1 The permissible all-up weight as specified in its Certificate of Airworthiness.
2.1.2 The maximum take-off weight specified in the relevant Aeroplane Flight
Manual for the altitude above sea level of the aerodrome concerned.
2.1.3 The lesser weight of either:
(a) the permissible landing weight at the destination aerodrome calculated in
accordance with paragraph 3 of these Orders plus the weight of fuel that
would normally be consumed in flying from the departure aerodrome to
the destination aerodrome; or
(b) the permissible landing weight at the alternate aerodrome calculated in
accordance with paragraph 3 of these Orders plus the weight of fuel that
would normally be consumed in flying from the departure aerodrome to
the alternate aerodrome.
Note: Subparagraph (b) will apply only when the flight plan includes an alternate aerodrome.
2.1.4 The weight calculated from the relevant current CASA Take-off Weight Chart
or approved Company Take-off Weight Chart for the aerodrome type
concerned in conjunction with either:
(a) the corrected effective operational length of the runway to be used for
take-off under ambient conditions; or
Issue 4: 8 December 2004
Amdt No. 209
SECTION 20.7.1 -2-
Issue 4
(b) the appropriate seasonal declared density altitude taken in conjunction
with either:
(i) the corrected effective operational length of the runway for take-off
under no wind conditions; or
(ii) the corrected effective operational length of any subsidiary runway
for take-off under the minimum head-wind component that may
result when the main runway cannot be used due to excessive crosswind
component, whichever gives the lesser weight.
Note: The weight calculated in accordance with subparagraph (b) (ii) above shall not apply to
a subsidiary runway which is listed in the Operations Manual as being unsuited for take-off
by the type of aeroplane concerned when using declared weight. When it is desired to use a
subsidiary runway which has been so listed in the Operations Manual the take-off weight
shall be calculated using the methods specified in subparagraph (a) of this paragraph.
2.2 Where, prior to the take-off, a significant change occurs in the value of any
factor used in computing the permissible take-off weight which would have the
effect of requiring a reduced all-up weight from that already computed, then a
new all-up weight shall be calculated using the new value for the factor(s)
concerned and the weight so determined shall be the maximum weight to be
used for take-off.
2.3 Take-off weight charts which enable compliance with this Order are available
on application to CASA. Instructions for the use of these charts are provided at
Appendix 1.
3 LANDING WEIGHT LIMITATIONS
3.1 Except in an emergency, an aeroplane shall not land at a weight in excess of
the least of the weights determined in accordance with subparagraphs 3.1.1 to
3.1.3 of these Orders.
3.1.1 The maximum permissible landing weight as specified in its Certificate of
Airworthiness.
3.1.2 The maximum landing weight specified in the relevant Aeroplane Flight
Manual for the altitude above sea level of the aerodrome concerned.
3.1.3 The weight calculated from the relevant CASA Landing Weight Chart or the
approved Company Landing Weight Chart for the aeroplane type concerned in
conjunction with the forecast pressure and temperature or the appropriate
seasonal declared density altitude with either:
(a) the corrected effective operational length of the main runway for landing
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：澳大利亞CAO(13)