Climb. The Aircraft climbs from ***feet above the departure airport altitude to ***feet altitude at *** KCAS. The Aircraft then accelerates at a rate of climb of *** feet per minute to a climb speed of *** KCAS. The climb continues at *** KCAS until ***Mach number is reached. The climb continues at ***Mach number to the initial cruise altitude. The temperature is standard day during climb. Maximum climb thrust is used during climb. Cruise: The Aircraft cruises at ***Mach number. The initial cruise altitude is ***feet. A step climb or multiple step climbs of ***feet altitude may be used when beneficial to minimize fuel burn. The temperature is standard day during cruise. The cruise thrust is not to exceed maximum cruise thrust except during a step climb when maximum climb thrust may be used.
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Climb. The Aircraft climbs from ***feet above the departure airport altitude to ***feet altitude at *** KCAS. The Aircraft then accelerates at a rate of climb of *** feet per minute to a climb speed of *** *KCAS. The climb continues at *** KCAS until ***Mach number is reached. The climb continues at ***Mach number to the initial cruise altitude. The temperature is standard day ISA+***°C during climb. Maximum climb thrust is used during climb. Cruise: The Aircraft cruises at ***Mach number. The initial cruise altitude is ***feet. A step climb or multiple step climbs of ***feet altitude may be used when beneficial to minimize fuel burn. The temperature is standard day ISA+***°C during cruise. The cruise thrust is not to exceed maximum cruise thrust except during a step climb when maximum climb thrust may be used.
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Climb. The Aircraft climbs from ***feet above the departure airport altitude to ***feet altitude at *** KCAS. The Aircraft then accelerates at a rate of climb of *** feet per minute to a climb speed of *** KCAS. The climb continues at *** KCAS until ***Mach number is reached. The climb continues at ***Mach number to the initial cruise altitude. The temperature is standard day ISA+***°C during climb. Maximum climb thrust is used during climb. Cruise: The Aircraft cruises at ***Mach number. The initial cruise altitude is ***feet. A step climb or multiple step climbs of ***feet altitude may be used when beneficial to minimize fuel burn. The temperature is standard day ISA+***°C during cruise. The cruise thrust is not to exceed maximum cruise thrust except during a step climb when maximum climb thrust may be used.
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Climb. The Aircraft climbs from **** feet above the departure airport altitude to **** feet altitude at the recommended speed of *** KCAS. The Aircraft then accelerates at a rate of climb of *** feet per minute to a the recommended climb speed of *** KCASfor minimum block fuel. The climb continues at the recommended climb speed for minimum block fuel until *** KCAS until ***Mach number is reached. The climb continues at **** Mach number to the initial cruise altitude. The temperature is standard day ISA***°C during climb. Maximum climb thrust is used during climb. Cruise: The Aircraft cruises at **** Mach number. The initial cruise altitude is **** feet. A step climb or multiple step climbs of **** feet altitude may be used when beneficial to minimize fuel burn. The temperature is standard day ISA***°C during cruise. The cruise thrust is not to exceed maximum cruise thrust except during a step climb when maximum climb thrust may be used.
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Climb. The Aircraft climbs from **** feet above the departure airport altitude to **** feet altitude at **** KCAS. The Aircraft then accelerates at a rate of climb of **** feet per minute to a climb speed of **** KCAS. The climb continues at **** KCAS until **** Mach number is reached. The climb continues at **** Mach number to the initial cruise altitude. The temperature is standard day during climb. Maximum climb thrust is used during climb. Cruise: The Aircraft cruises at **** Mach number. The initial cruise altitude is ****feet. A step climb or multiple step climbs of ****feet altitude may be used when beneficial to minimize fuel burn. The temperature is standard day during cruise. The cruise thrust is not to exceed maximum cruise thrust except during a step climb when maximum climb thrust may be used.
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