Common use of Climb Clause in Contracts

Climb. The Aircraft climbs from 1,500 feet above the departure airport altitude to 10,000 feet altitude at 283 KCAS. The Aircraft then accelerates at a rate of climb of 500 feet per minute to a climb speed of 356 KCAS. The climb continues at 356 KCAS until 0.84 Mach number is reached. The climb continues at 0.84 Mach number to the initial cruise altitude. The temperature is ISA+10 degrees C during climb. Maximum climb thrust is used during climb. Cruise: The Aircraft cruises at 0.84 Mach number. The initial cruise altitude is 29,000 feet. A step climb or multiple step climbs of 4,000 feet altitude may be used when beneficial to minimize fuel burn.

Climb. The Aircraft climbs from 1,500 [***] feet above the departure airport altitude to 10,000 [***] feet altitude at 283 [***] KCAS. The Aircraft then accelerates at a rate of climb of 500 [***] feet per minute to a the recommended climb speed of 356 KCASfor minimum block fuel. The climb continues at 356 KCAS the recommended climb speed for minimum block fuel until 0.84 0.78 Mach number is reached. The climb continues at 0.84 0.78 Mach number to the initial cruise altitude. The temperature is ISA+10 degrees C standard day during climb. Maximum climb thrust is used during climb. Cruise: The Aircraft cruises at 0.84 0.79 Mach number. The initial cruise altitude is 29,000 37,000 feet. A step climb or multiple step climbs of 4,000 2,000 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.

Climb. The Aircraft climbs from 1,500 feet above the departure airport altitude to 10,000 feet altitude at 283 250 KCAS. The Aircraft then accelerates at a rate of climb of 500 feet per minute to a the recommended climb speed of 356 KCASfor minimum block fuel. The climb continues at 356 KCAS the recommended climb speed for minimum block fuel until 0.84 0.78 Mach number is reached. The climb continues at 0.84 0.78 Mach number to the initial cruise altitude. The temperature is ISA+10 degrees C standard day during climb. Maximum climb thrust is used during climb. Cruise: The Aircraft cruises at 0.84 Mach numberthe Long Range Cruise (LRC) speed. The initial cruise altitude is 29,000 36,000 feet. A step climb or multiple step climbs of 4,000 2,000 feet altitude may be used when beneficial to minimize fuel burn. The temperature is standard day during cruise.

Climb. The Aircraft climbs from 1,500 feet above the departure airport altitude to 10,000 feet altitude at 283 250 KCAS. The Aircraft then accelerates at a rate of climb of 500 feet per minute to a the recommended climb speed of 356 KCASfor minimum block fuel. The climb continues at 356 KCAS the recommended climb speed for minimum block fuel until 0.84 0.78 Mach number is reached. The climb continues at 0.84 0.78 Mach number to the initial cruise altitude. The temperature is ISA+10 degrees C standard day during climb. Maximum climb thrust is used during climb. Cruise: The Aircraft cruises at 0.84 Mach numberthe Long Range Cruise (LRC) speed. The initial cruise altitude is 29,000 34,000 feet. A step climb or multiple step climbs of 4,000 2,000 feet altitude may be used when beneficial to minimize fuel burn. The temperature is standard day during cruise.