Mission Range. The Aircraft shall be capable of carrying a Zero Fuel Weight of [DELETED] kg over a guaranteed still air stage distance of not less than [DELETED] nautical miles when operated under the conditions defined below: 3.1.1 The departure airport conditions are such as to allow the required take-off weight to be used without any restriction. The destination airport conditions are such as to allow the required landing weight to be used without any restriction. 3.1.2 An allowance of [DELETED] kg of fuel is included for engine start and taxi-out at departure airport. 3.1.3 An allowance of [DELETED] kg of fuel is included for take-off and climb to [DELETED] ft above the departure airport with acceleration to climb speed in ISA conditions.
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Mission Range. The Aircraft shall be capable of carrying a Zero Fuel Weight of [DELETED] kg over a guaranteed still air stage distance of not less than [DELETED] nautical miles when operated under the conditions defined below:
3.1.1 The departure airport conditions are such as to allow the required take-off weight to be used without any restriction. The destination airport conditions are such as to allow the required landing weight to be used without any restriction.
3.1.2 An allowance of [DELETED] kg of fuel is included for engine start and taxi-out at departure airport.
3.1.3 An allowance of [DELETED] kg of fuel is included for take-off and climb to [DELETED] ft above the departure airport with acceleration to climb speed in ISA [DELETED] conditions.
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