Maximum Range Guarantee Clause Samples

Maximum Range Guarantee. When operated under the conditions specified below with the fixed quantities and allowances specified in paragraph 3.5.3, the maximum still air range (stage length) out of Phoenix shall be not less than [***] nautical miles when carrying a fixed payload of [***] lb equivalent to [***] passengers at [***] lb. The maximum take-off weight out of Phoenix (PHX) is based on the conditions specified in paragraph 2.0 and is in compliance with FAR 25 take-off requirements. The mission is flown in ISA conditions throughout. Climb is made starting at [***] ft to [***] ft pressure altitude using a climb speed schedule of [***] KCAS/ [***] M ([***] KCAS is maintained until the altitude where [***] M is reached). 18 Supplement 3 to MPA 497 Mesa Air Group, Inc. Initials Buyer_____ Bombardier_____ 147 Cruise is at [***] ft pressure altitude at an average cruise Mach number of [***] M. Thrust during cruise is not to exceed maximum cruise thrust. Descent is made from [***] ft pressure altitude to sea level using a descent speed schedule of [***] M / [***] KCAS. The fixed fuel reserves, per paragraph 3.5.3, are [***] lb.

Maximum Range Guarantee. When operated under the conditions specified below with the fixed quantities and allowances specified in Article 3.5.3, the maximum still air range (stage length) shall be not less than 1375 nautical miles (1583 statute miles) when carrying a fixed payload of 11000 lb (50 passengers). Take-off is at a fixed weight of 53000 lb at brake release. The mission is flown in ISA+15oC conditions throughout. A fixed allowance of 181 lb of fuel is considered for 1.8 minutes take-off and acceleration time to 250 KCAS initial climb speed at 1500 feet above sea level. Climb is made starting at 1500 feet to 31000 feet pressure altitude using a climb speed schedule of 250 KCAS/ 0.70 M. Cruise is at 31000 feet pressure altitude at an average cruise Mach number of 0.74 M. Thrust during cruise is not to exceed maximum cruise thrust. Step climb is made starting at 31000 feet to 33000 feet pressure altitude using a climb speed schedule of 250 KCAS/ 0.70 M. Cruise is at 33000 feet pressure altitude at an average cruise Mach number of 0.74 M. Thrust during cruise is not to exceed maximum cruise thrust. Descent is made from 33000 feet to 1500 feet pressure altitude using a descent speed schedule of 0.70 M / 250 KCAS.

Maximum Range Guarantee. For a mission with an equivalent still air range (stage length) of 1541 nautical miles, when operated under the conditions specified below with the fixed quantities and allowances specified in article 2.5.2, the block fuel burnt shall not be more than 12329 lb when carrying a fixed payload of 15400 lb representative of 70 passengers at 220 lb. The mission is flown in ISA conditions throughout. Climb is made starting at sea level to 37000 ft pressure altitude using a climb speed schedule of 250 KCAS/ 0.70 M. Initial cruise is at 37000 feet pressure altitude at a cruise Mach number of 0.77 M. Thrust during initial cruise is not to exceed maximum cruise thrust. A step climb from 37000 feet to 39000 feet pressure altitude is made using a climb speed of 0.70 M. Final cruise is at 39000 ft pressure altitude at cruise Mach number of 0.77 M. Thrust during final cruise is not to exceed maximum cruise thrust. Descent is made from 39000 ft pressure altitude to sea level using a descent speed schedule of 0.70 M / 250 KCAS. Usable reserve fuel remaining at the end of the approach and landing phase is 2831 lb. This fuel is based on the reserve profile as specified in article 2.5.2.