Common use of Mission Range Clause in Contracts

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] 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. 3.1.4 Climb from [DELETED] ft above the departure airport up to optimum cruise altitude using maximum climb thrust, cruise at a fixed Mach number of [DELETED] at a pressure altitude of [DELETED] ft, / [DELETED] ft, and descent to [DELETED] ft above the destination airport are conducted in ISA conditions. Climb and descent speeds below [DELETED] ft shall be [DELETED] knots CAS. 3.1.5 An allowance of [DELETED] kg of fuel is considered for approach and landing at destination airport. 3.1.6 An allowance of [DELETED] kg of fuel is considered for taxi in at the destination airport.

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. 3.1.4 Climb from [DELETED] ft above the departure airport up to optimum cruise altitude using maximum climb thrust, cruise at a fixed Mach number of [DELETED] at a pressure altitude of [DELETED] ft, / [DELETED] ft, and descent to [DELETED] ft above the destination airport are conducted in ISA conditions. Climb and descent speeds below [DELETED] ft shall be [DELETED] knots CAS. 3.1.5 An allowance of [DELETED] kg of fuel is considered for approach and landing at destination airport. 3.1.6 An allowance of [DELETED] kg of fuel is considered for taxi in at the destination airport. 3.1.7 Stage distance is defined as the distance covered during cruise, climb and descent as described in Paragraph 3.

Mission Range. The Aircraft shall be capable of carrying a Zero Fuel Weight of [DELETED] kg 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 DELETED]ft above the departure airport with acceleration to climb speed in ISA conditions. 3.1.4 Climb from [DELETED] ft DELETED]ft above the departure airport up to optimum cruise altitude using maximum climb thrust, cruise at a fixed Mach number of [DELETED] at DELETED]at a pressure altitude of [DELETED] ftDELETED]ft, / [DELETED] ftDELETED]ft, and descent to [DELETED] ft DELETED]ft above the destination airport are conducted in ISA conditions. Climb and descent speeds below [DELETED] ft DELETED]ft shall be [DELETED] knots CAS. 3.1.5 An allowance of [DELETED] kg of fuel is considered for approach and landing at destination airport. 3.1.6 An allowance of [DELETED] kg of fuel is considered for taxi in at the destination airport. 3.1.7 Stage distance is defined as the distance covered during cruise, climb and descent as described in Paragraph 3.