Common use of Climb Clause in Contracts

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 the recommended climb speed for minimum block fuel. The climb continues at the recommended climb speed for minimum block fuel until 0.78 Mach number is reached. The climb continues at 0.78 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 0.79 Mach number. The initial cruise altitude is 37,000 feet. A step climb or multiple step climbs of 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.

Appears in 2 contracts

Samples: Supplemental Agreement (Alaska Air Group Inc), Purchase Agreement (Alaska Air Group Inc)

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Climb. The Aircraft climbs from [***] 1,500 feet above the departure airport altitude to [***] 10,000 feet altitude at [***] the recommended speed of 250 KCAS. The Aircraft then accelerates at a rate of climb of [***] 500 feet per minute to the recommended climb speed for minimum block fuel. The climb continues at the recommended climb speed for minimum block fuel until 0.78 0.85 Mach number is reached. The climb continues at 0.78 0.85 Mach number to the initial cruise altitude. The temperature is standard day ISA+10°C during climb. Maximum climb thrust is used during climb. Cruise: The Aircraft cruises at 0.79 0.85 Mach number. The initial cruise altitude is 37,000 at least 32,000 feet. A step climb or multiple step climbs of 2,000 feet altitude may be used when beneficial to minimize fuel burn. The final cruise altitude shall not exceed 40,000 feet. The temperature is standard day ISA+10°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.

Appears in 1 contract

Samples: Purchase Agreement (China Southern Airlines Co LTD)

Climb. The Aircraft climbs from [***] 1,500 feet above the departure airport altitude to [***] 10,000 feet altitude at [***] 250 KCAS. The Aircraft then accelerates at a rate of climb of [***] 500 feet per minute to the recommended climb speed for minimum block fuel. The climb continues at the recommended climb speed for minimum block fuel until 0.78 0.85 Mach number is reached. The climb continues at 0.78 0.85 Mach number to the initial cruise altitude. The temperature is standard day ISA+10°C during climb. Maximum climb thrust is used during climb. Cruise: The Aircraft cruises at 0.79 Mach numberthe Long Range Cruise (LRC) speed. The initial cruise altitude is 37,000 36,000 feet. A step climb or multiple step climbs of 2,000 feet with a final step climb of 3,000 feet altitude may be used when beneficial to minimize fuel burn. The temperature is standard day ISA+10°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.

Appears in 1 contract

Samples: Supplemental Agreement (Lan Airlines SA)

Climb. The Aircraft climbs from [***] 1,500 feet above the departure airport altitude to [***] 10,000 feet altitude at [***] 250 KCAS. The Aircraft then accelerates at a rate of climb of [***] 500 feet per minute to the recommended climb speed for minimum block fuel. The climb continues at the recommended climb speed for minimum block fuel until 0.78 Mach number is reached. The climb continues at 0.78 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 0.79 Mach numberthe Long Range Cruise (LRC) speed. The initial cruise altitude is 37,000 34,000 feet. A step climb or multiple step climbs of 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.

Appears in 1 contract

Samples: Supplemental Agreement (American Airlines Inc)

Climb. The Aircraft climbs from [***] 1,500 feet above the departure airport altitude to [***] 10,000 feet altitude at [***] 250 KCAS. The Aircraft then accelerates at a rate of climb of [***] 500 feet per minute to the recommended climb speed for minimum block fuel. The climb continues at the recommended climb speed for minimum block fuel until 0.78 0.85 Mach number is reached. The climb continues at 0.78 0.85 Mach number to the initial cruise altitude. The temperature is standard day ISA+10°C during climb. Maximum climb thrust is used during climb. Cruise: The Aircraft cruises at 0.79 Mach numberthe Long Range Cruise (LRC) speed. The initial cruise altitude is 37,000 feet. A step climb or multiple step climbs of 2,000 feet altitude may be used when beneficial to minimize fuel burn. The temperature is standard day ISA+10°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.

Appears in 1 contract

Samples: Supplemental Agreement (Lan Airlines SA)

Climb. The Aircraft climbs from [***] 1,500 feet above the departure airport altitude to [***] 10,000 feet altitude at [***] 250 KCAS. The Aircraft then accelerates at a rate of climb of [***] 500 feet per minute to the recommended climb speed for minimum block fuel. The climb continues at the recommended climb speed for minimum block fuel until 0.78 0.85 Mach number is reached. The climb continues at 0.78 0.85 Mach number to the initial cruise altitude. The temperature is standard day ISA+10°C during climb. Maximum climb thrust is used during climb. Cruise: The Aircraft cruises at 0.79 Mach numberthe Long Range Cruise (LRC) speed. The initial cruise altitude is 37,000 39,000 feet. A step climb or multiple step climbs of 2,000 feet altitude may be used when beneficial to minimize fuel burn. The temperature is standard day ISA+10°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.

Appears in 1 contract

Samples: Supplemental Agreement (Lan Airlines SA)

Climb. The Aircraft climbs from [***] 1,500 feet above the departure airport altitude to [***] 10,000 feet altitude at [***] the recommended speed of 250 KCAS. The Aircraft then accelerates at a rate of climb of [***] 500 feet per minute to the recommended climb speed for minimum block fuel. The climb continues at the recommended climb speed for minimum block fuel until 0.78 0.85 Mach number is reached. The climb continues at 0.78 0.85 Mach number to the initial cruise altitude. The temperature is standard day ISA+10°C during climb. Maximum climb thrust is used during climb. Cruise: The Aircraft cruises at 0.79 0.85 Mach number. The initial cruise altitude is 37,000 at least 33,000 feet. A step climb or multiple step climbs of 2,000 feet altitude may be used when beneficial to minimize fuel burn. The final cruise altitude shall not exceed 40,000 feet. The temperature is standard day ISA+10°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.

Appears in 1 contract

Samples: Purchase Agreement (China Southern Airlines Co LTD)

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Climb. The Aircraft climbs from [***] 1,500 feet above the departure airport altitude to [***] 10,000 feet altitude at [***] 250 KCAS. The Aircraft then accelerates at a rate of climb of [***] 500 feet per minute to the recommended climb speed for minimum block fuel. The climb continues at the recommended climb speed for minimum block fuel until 0.78 0.79 Mach number is reached. The climb continues at 0.78 0.79 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 0.79 Mach numberthe Long Range Cruise (LRC) speed. The initial cruise altitude is 37,000 36,000 feet. A step climb or multiple step climbs of 2,000 feet altitude may be used when beneficial to minimize fuel burn. The temperature is standard day during cruise. CEA-PA-4076-LA-1302574 Attachment to Letter Agreement No. LA-1302574 LEAP-1B28 Engines The cruise thrust is not to exceed maximum cruise thrust except during a step climb when maximum climb thrust may be used.

Appears in 1 contract

Samples: Purchase Agreement (China Eastern Airlines Corp LTD)

Climb. The Aircraft climbs from [***] 1,500 feet above the departure airport altitude to [***] 10,000 feet altitude at [***] 250 KCAS. The Aircraft then accelerates at a rate of climb of [***] 500 feet per minute to the recommended climb speed for minimum block fuel. The climb continues at the recommended climb speed for minimum block fuel until 0.78 0.79 Mach number is reached. The climb continues at 0.78 0.79 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 0.79 Mach numberthe Long Range Cruise (LRC) speed. The initial cruise altitude is 37,000 35,000 feet. A step climb or multiple step climbs of 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.

Appears in 1 contract

Samples: Purchase Agreement (China Eastern Airlines Corp LTD)

Climb. The Aircraft climbs from [***] 1,500 feet above the departure airport altitude to [***] 10,000 feet altitude at [***] 250 KCAS. The Aircraft then accelerates at a rate of climb of [***] 500 feet per minute to the recommended climb speed for minimum block fuel. The climb continues at the recommended climb speed for minimum block fuel until 0.78 0.85 Mach number is reached. The climb continues at 0.78 0.85 Mach number to the initial cruise altitude. The temperature is standard day ISA+10°C during climb. Maximum climb thrust is used during climb. Cruise: The Aircraft cruises at 0.79 Mach numberthe Long Range Cruise (LRC) speed. The initial cruise altitude is 37,000 36,000 feet. A step climb or multiple step climbs of 2,000 feet altitude may be used when beneficial to minimize fuel burn. The temperature is standard day ISA+10°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.

Appears in 1 contract

Samples: Supplemental Agreement (Lan Airlines SA)

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