CIVIL AVIATION ORDERS PART 20 SECTION 20.7.2 Issue 4 AEROPLANE WEIGHT AND PERFORMANCE LIMITATIONS — MULTI-ENGINE AEROPLANES NOT ABOVE 5700 KG — REGULAR PUBLIC TRANSPORT OPERATIONS SUBSECTIONS
1 2 3 4 Application Definitions Take-off performance limitations Take-off obstacle clearance limitations APPLICATION 5 6 7 8 Route limitations Landing limitations Unserviceable equipment Compliance
1
Unless CASA otherwise directs, this section applies to all multi-engine aeroplanes having a maximum take-off weight not in excess of 5 700kg engaged in regular public transport operations.
2 DEFINITIONS
In this section, terms and abbreviations have the meanings defined in section 20.7.1B, and in Part 101 except that: take-off distance available means the length of take-off run available plus, where clearway is provided, a maximum of 60 metres of clearway.
3 TAKE-OFF PERFORMANCE LIMITATIONS
3.1
No aeroplane shall take off at a weight in excess of the take-off weight specified in the aeroplane flight manual for the take-off distance available. In determining this weight, account shall be taken of the aerodrome pressure altitude, ambient temperature, runway surface and slope, and the wind velocity at the time of take-off. No aeroplane shall take off at a weight such that, allowing for normal consumption of fuel in flight to the destination and alternate aerodromes, the weight on arrival would exceed the weight specified in the aeroplane flight manual with respect to baulked landing climb performance. In determining this weight, account shall be taken of the aerodrome pressure altitude and, for aeroplanes having a maximum take-off weight exceeding 3 500 kg the ambient temperature forecast for the estimated time of landing.
Issue 4: 8 December 2004 Amdt No. 211
3.2
飞行翻译公司 www.aviation.cn 本文链接地址：200702.pdf
1 2 3 4 Application Definitions Take-off performance limitations Take-off obstacle clearance limitations APPLICATION 5 6 7 8 Route limitations Landing limitations Unserviceable equipment Compliance
1
Unless CASA otherwise directs, this section applies to all multi-engine aeroplanes having a maximum take-off weight not in excess of 5 700kg engaged in regular public transport operations.
2 DEFINITIONS
In this section, terms and abbreviations have the meanings defined in section 20.7.1B, and in Part 101 except that: take-off distance available means the length of take-off run available plus, where clearway is provided, a maximum of 60 metres of clearway.
3 TAKE-OFF PERFORMANCE LIMITATIONS
3.1
No aeroplane shall take off at a weight in excess of the take-off weight specified in the aeroplane flight manual for the take-off distance available. In determining this weight, account shall be taken of the aerodrome pressure altitude, ambient temperature, runway surface and slope, and the wind velocity at the time of take-off. No aeroplane shall take off at a weight such that, allowing for normal consumption of fuel in flight to the destination and alternate aerodromes, the weight on arrival would exceed the weight specified in the aeroplane flight manual with respect to baulked landing climb performance. In determining this weight, account shall be taken of the aerodrome pressure altitude and, for aeroplanes having a maximum take-off weight exceeding 3 500 kg the ambient temperature forecast for the estimated time of landing.
Issue 4: 8 December 2004 Amdt No. 211
3.2
飞行翻译公司 www.aviation.cn 本文链接地址：200702.pdf
自定义标签： 
