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CIVIL AVIATION ORDERS PART 20 SECTION 20.7.4 Issue 4 AEROPLANE WEIGHT AND PERFORMANCE LIMITATIONS — AEROPLANES NOT ABOVE 5 700 KG — REGULAR PUBLIC TRANSPORT OPERATIONS (SINGLE-ENGINE AEROPLANES ONLY), CHARTER OPERATIONS, AERIAL WORK (EXCLUDING AGRICULTURAL) OPERATIONS AND PRIVATE OPERATIONS SUBSECTIONS
2 3 4 5 6 7 2 Application Definitions Take-off weight limitations Landing weight limitations Take-off distance required Take-off climb performance APPLICATION 8 9 10 12 En-route climb performance Landing climb performance Landing distance required Aeroplane configuration and procedures

This section applies to aeroplanes having a maximum take-off weight not in excess of 5700 kg engaged in regular public transport operations (single-engine aeroplanes only), private operations, aerial work operations (excluding agricultural operations) and charter operations, unless CASA specifies that sections 20.7.1 or 20.7.2 are to be applied.
3 DEFINITIONS

3.1

In this section: approved foreign flight manual, in relation to an aeroplane, means the flight manual approved by the relevant regulatory aviation authority of the country where the aeroplane is, or was, manufactured. landing distance available means the distance specified by CASA as being the effective operational length available for use by aircraft for landing at Government and Licensed Aerodromes or the distance available for landing on an authorised landing or alighting area. manufacturer’s data manual, in relation to an aeroplane, means a publication (however described) produced by the manufacturer of the aeroplane as a guide for the flight crew in the operation of the aeroplane. pressure height means the height registered on an altimeter with the sub-scale set to 1013.2 hPa.

Issue 4: 8 December 2004 Amdt No. 212


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