Common use of Climb Clause in Contracts

Climb. The Aircraft climbs from *** feet above the departure airport altitude to *** feet altitude at the recommended speed of *** KCAS. Attachment to Letter Agreement Xx. XXX-XX-00000-XX-0000000 CFM56-7B*** Engines 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 *** Mach number is reached. The climb continues at *** Mach number to the initial cruise altitude. The temperature is ***°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 ***°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.

Climb. The Aircraft climbs from *** feet above the departure airport altitude to *** feet altitude at the recommended speed of *** KCAS. Attachment to Letter Agreement Xx. XXX-XX-00000-XX-0000000 CFM56-7B*** Engines 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 *** Mach number is reached. The climb continues at *** Mach number to the initial cruise altitude. The temperature is ***°C 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 ***°C standard day during cruise. P.A. No. PA-1951 AERO-B-BBA4-M12-0362C SS12-0153 Attachment to Letter Agreement Xx. XXX-XX-0000-XX-0000000 *** 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 *** feet above the departure airport altitude to *** feet altitude at the recommended speed of *** KCAS. Attachment to Letter Agreement Xx. XXX-XX-00000-XX-0000000 CFM56-7B*** Engines The Aircraft then accelerates at a rate of climb of *** feet per minute to the recommended climb speed for minimum block fuel. Attachment to Letter Agreement Xx. XXX-XX-00000-XX-0000000 CFM56-7B*** Engines The climb continues at the recommended climb speed for minimum block fuel until *** Mach number is reached. The climb continues at *** Mach number to the initial cruise altitude. The temperature is ***°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 ***°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.

Climb. The Aircraft climbs from *** feet above the departure airport altitude to *** feet altitude at the recommended speed of *** KCAS. Attachment to Letter Agreement Xx. XXX-XX-00000-XX-0000000 CFM56-7B*** Engines 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 *** Mach number is reached. The climb continues at *** Mach number to the initial cruise altitude. The temperature is ***°C 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 ***°C standard day during cruise. P.A. No. 3860 AERO-B-BBA4-M09-0771B SS09-0285 Attachment A4 UAL-PA-03860-LA-1209430 Trent 1000*** Engines 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 *** feet above the departure airport altitude to *** feet altitude at the recommended speed of *** KCAS. P.A. No. 3860 AERO-B-BBA4-M09-0771B SS09-0285 Attachment to Letter Agreement Xx. XXXA4 UAL-XX-00000PA-03860-XX-0000000 CFM56-7BLA-1209430 Trent 1000*** Engines 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 *** Mach number is reached. The climb continues at *** Mach number to the initial cruise altitude. The temperature is ***°C 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 ***°C 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 *** feet above the departure airport altitude to *** feet altitude at the recommended speed of *** KCAS. Attachment to Letter Agreement Xx. XXX-XX-00000-XX-0000000 CFM56-7B*** Engines The Aircraft then accelerates at a rate of climb of *** feet per minute to the recommended climb speed for minimum block fuel. AERO-B-BBA4-M12-0320C SS12-0153 Attachment to Letter Agreement No. UAL-PA-03784-LA-1207868 *** The climb continues at the recommended climb speed for minimum block fuel until *** Mach number is reached. The climb continues at *** Mach number to the initial cruise altitude. The temperature is ***°C 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 ***°C 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 *** feet above the departure airport altitude to *** feet altitude at the recommended speed of *** KCAS. Attachment to Letter Agreement Xx. XXX-XX-00000-XX-0000000 CFM56-7B*** Engines 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 *** Mach number is reached. The climb continues at *** Mach number to the initial cruise altitude. The temperature is ***°C 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. P.A. No. PA-1951 AERO-B-BBA4-M12-0362C SS12-0153 Attachment to Letter Agreement Xx. XXX-XX-0000-XX-0000000 *** The temperature is ***°C 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 *** feet above the departure airport altitude to *** feet altitude at the recommended speed of *** KCAS. Attachment to Letter Agreement Xx. XXX-XX-00000-XX-0000000 CFM56-7B*** Engines 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 *** Mach number is reached. The climb continues at *** Mach number to the initial cruise altitude. The temperature is ***°C 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 ***°C standard day during cruise. P.A. No. 3860 AERO-B-BBA4-M09-0774C SS09-0285 Attachment A2 UAL-PA-03860-LA-1209430 Trent 1000-*** Engines 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 *** feet above the departure airport altitude to *** feet altitude at the recommended speed of *** KCAS. Attachment to Letter Agreement Xx. XXX-XX-00000-XX-0000000 CFM56-7B*** Engines 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 *** Mach number is reached. The climb continues at *** Mach number to the initial cruise altitude. P.A. No. PA-1951 AERO-B-BBA4-M12-0362C SS12-0153 Attachment to Letter Agreement Xx. XXX-XX-0000-XX-0000000 *** The temperature is ***°C 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 ***°C 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 *** feet above the departure airport altitude to *** feet altitude at the recommended speed of *** KCAS. P.A. No. 03776 AERO-B-BBA4-M12-0254 SS12-0083 Attachment A to Letter Agreement Xx. XXX-XX-00000-XX-0000000 CFM56-7B*** Engines 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 *** Mach number is reached. The climb continues at *** Mach number to the initial cruise altitude. The temperature is ***°C 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 ***°C 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.