# The Air Navigation (Overseas Territories) Order 2001, Paragraph 11: Weight and performance of public transport helicopters classified as helicopters of performance group A in their certificate of airworthiness


For the purposes of article 36(1), a helicopter registered in the Territory in respect of which there is in force under this Order a certificate of airworthiness in which the helicopter is designated as being of performance group A shall not fly for the purpose of public transport unless the weight of the helicopter at the commencement of take off is such that the following conditions are satisfied:
(1) The weight does not exceed the maximum take off weight specified for the altitude and the air temperature at the site from which the take off is to be made.
(2) The landing weight of the helicopter will not exceed the maximum landing weight specified for the altitude and the expected air temperature for the estimated time of landing at the site at which it is intended to land and at any alternate site.

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Source: https://www.legislation.gov.uk/uksi/2001/2128/schedule/14/paragraph/11 (the official version)
Page: https://openlegislation.uk/air-navigation-overseas-territories-order-2001/schedule-14/paragraph-11
Contains public sector information licensed under the Open Government Licence v3.0. Source: legislation.gov.uk, The National Archives.