CIVIL AVIATION ORDERS PART 20 SECTION 20.7.1 Issue 4 AEROPLANE WEIGHT LIMITATIONS — AEROPLANES ABOVE 5700 KG — ALL OPERATIONS (PISTON ENGINED) SUBSECTIONS
1 2 1 Application Take-off Weight Limitations APPLICATION 3 Landing Weight Limitations Appendixes 1 and 2
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 2.1.1 2.1.2 2.1.3
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: The permissible all-up weight as specified in its Certificate of Airworthiness. The maximum take-off weight specified in the relevant Aeroplane Flight Manual for the altitude above sea level of the aerodrome concerned. 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
飞行翻译公司 www.aviation.cn 本文链接地址：200701.pdf
1 2 1 Application Take-off Weight Limitations APPLICATION 3 Landing Weight Limitations Appendixes 1 and 2
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 2.1.1 2.1.2 2.1.3
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: The permissible all-up weight as specified in its Certificate of Airworthiness. The maximum take-off weight specified in the relevant Aeroplane Flight Manual for the altitude above sea level of the aerodrome concerned. 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
飞行翻译公司 www.aviation.cn 本文链接地址：200701.pdf
自定义标签： 
