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 the recommended speed of 262 KCAS. The Aircraft then accelerates at a rate of climb of 300 feet per minute to a climb speed of 320 KCAS. The climb continues at 320 KCAS until 0.8223 Mach number is reached. The climb continues at 0.8223 Mach number to the initial cruise altitude. The temperature is ISA+5°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.

Climb. The Aircraft climbs from 1,500 feet above the departure airport altitude to 10,000 feet altitude at the recommended speed of 262 245 KCAS. The Aircraft then accelerates at a rate of climb of 300 feet per minute to a climb speed of 320 270 KCAS. The climb continues at 320 270 KCAS until 0.8223 Mach number 17,500 feet is reached. The climb continues at 0.8223 0.56 Mach number to the initial cruise altitude. The temperature is ISA+5°C ISA during the climb. Maximum climb thrust is used during throughout the climb. Cruise: The Aircraft cruises at 0.84 an average speed of 0.76 Mach number. The initial cruise altitude is 29,000 35,000 feet. The temperature is ISA during cruise. The cruise thrust is not to exceed maximum cruise thrust.

Climb. The Aircraft climbs from 1,500 feet above the departure airport altitude to 10,000 feet altitude at the recommended speed of 262 250 KCAS. The Aircraft then accelerates at a rate of climb of 300 500 feet per minute to a the recommended climb speed of 320 KCASfor minimum block fuel. The climb continues at 320 KCAS the recommended climb speed for minimum block fuel until 0.8223 0.79 Mach number is reached. The climb continues at 0.8223 0.79 Mach number to the initial cruise altitude. The temperature is ISA+5°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 35,000 feet.

Climb. The Aircraft climbs from 1,500 feet above the departure airport altitude to 10,000 feet altitude at the recommended speed of 262 250 KCAS. The Aircraft then accelerates at a rate of climb of 300 500 feet per minute to a the recommended climb speed of 320 KCASfor minimum block fuel. The climb continues at 320 KCAS until 0.8223 Mach number is reached. The the recommended climb continues at 0.8223 Mach number speed for minimum block fuel to the initial cruise altitude. The temperature is ISA+5°C standard day 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 feetthe Long Range Cruise (LRC) speed.

Climb. The Aircraft climbs from 1,500 feet above the departure airport altitude to 10,000 feet altitude at the recommended speed of 262 250 KCAS. The Aircraft then accelerates at a rate of climb of 300 500 feet per minute to a the recommended climb speed of 320 KCASfor minimum block fuel. The climb continues at 320 KCAS the recommended climb speed for minimum block fuel until 0.8223 0.78 Mach number is reached. The climb continues at 0.8223 0.78 Mach number to the initial cruise altitude. The temperature is ISA+5°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 38,000 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.

Climb. The Aircraft climbs from 1,500 feet above the departure airport altitude to 10,000 feet altitude at the recommended speed of 262 250 KCAS. The Aircraft then accelerates at a rate of climb of 300 500 feet per minute to a the recommended climb speed of 320 KCASfor minimum block fuel. The climb continues at 320 KCAS until 0.8223 Mach number is reached. The the recommended climb continues at 0.8223 Mach number speed for minimum block fuel to the initial cruise altitude. The temperature is ISA+5°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 32,000 feet.