Cruise Range Sample Clauses

Cruise Range. The still air range at an initial cruise altitude of [*] feet on an [*] day at [*] Mach number, starting at a gross weight of [*] kilograms and consuming [*] kilograms of fuel, and using not more than maximum cruise thrust (except maximum climb thrust may be used during a step climb) and using the conditions and operating rules defined below, shall not be less than the following guarantee value: NOMINAL: [*] Nautical Miles TOLERANCE: [*] Nautical Miles GUARANTEE: [*] Nautical Miles Conditions and operating rules: A step climb or multiple step climbs of [*] feet altitude may be used when beneficial to minimize fuel burn.

Cruise Range. 2.1.1 The still air range at an initial cruise altitude of **** feet on a standard day at **** Mach number, starting at a gross weight of **** pounds and consuming **** pounds of fuel, and using not more than maximum cruise thrust (except maximum climb thrust may be used during a step climb) and using the conditions and operating rules defined below, shall not be less than the following guarantee value: Conditions and operating rules: A step climb or multiple step climbs of **** feet altitude may be used when beneficial to minimize fuel burn.

Cruise Range. The still air range at an initial cruise altitude of *** feet on a standard day at *** Mach number, starting at a gross weight of *** pounds and consuming *** pounds of fuel, and using not more than maximum cruise thrust (except maximum climb thrust may be used during a step climb) and using the conditions and operating rules defined below, shall not be less than the following guarantee value: NOMINAL: *** Nautical Miles TOLERANCE: *** Nautical Miles GUARANTEE: *** Nautical Miles Conditions and operating rules: A step climb or multiple step climbs of *** feet altitude may be used when beneficial to minimize fuel burn.

Cruise Range. The still air range at an initial cruise altitude of *** feet on a standard day at *** Mach number, starting at a gross weight of *** pounds and consuming *** pounds of fuel, and using not more than maximum cruise thrust (except maximum climb thrust may be used during a step climb) and using the conditions and operating rules defined below, shall not be less than the following guarantee value: NOMINAL: *** Nautical Miles TOLERANCE: *** Nautical Miles GUARANTEE: *** Nautical Miles

Cruise Range. The still air range at an initial cruise altitude of [**] on an [**] day at [**] number, starting at a gross weight of [**] and [**], and using not more than maximum cruise thrust (except maximum climb thrust may be used during a step climb) and using the conditions and operating rules defined below, will not be less than the following guarantee value: NOMINAL: [**] TOLERANCE: [**] GUARANTEE: [**] Conditions and operating rules: A step climb or multiple step climbs of [**] may be used when beneficial to maximize range.

Cruise Range. The still air range at an initial cruise [***], shall not be less than the following guarantee value: Conditions and operating rules: [***].

Cruise Range. The still air range at an initial cruise altitude of 36,000 feet on a standard day at 0.78 Mach number, starting at a gross weight of 150,000 pounds and consuming 20,000 pounds of fuel, and using not more than maximum cruise thrust (except maximum climb thrust may be used during a step climb) and using the conditions and operating rules defined below, shall not be less than the following guarantee value: NOMINAL: 1,800 Nautical Miles TOLERANCE: -35 Nautical Miles GUARANTEE: 1,765 Nautical Miles Conditions and operating rules: A step climb or multiple step climbs of 2,000 feet altitude may be used when beneficial to minimize fuel burn. Attachment to Letter Agreement No. CEA-PA-4077 LA-1302564 CFM56-7B26E Engines

Cruise Range. The still air range at an initial cruise altitude of *** feet on a standard day at *** Mach number, starting at a gross weight of *** pounds and consuming *** pounds of fuel, and using not more than maximum cruise thrust (except maximum climb thrust may be used during a step climb) and using the conditions and operating rules defined below, shall not be less than the following guarantee value: NOMINAL: *** Nautical Miles TOLERANCE: *** Nautical Miles GUARANTEE: *** Nautical Miles P.A. No. PA-1951 AERO-B-BBA4-M12-0362C SS12-0153 Attachment to Letter Agreement Xx. XXX-XX-0000-XX-0000000 *** Conditions and operating rules: A step climb or multiple step climbs of *** feet altitude may be used when beneficial to minimize fuel burn.

Cruise Range. The still air range at an initial cruise altitude of 35,000 feet on a standard day at 0.78 Mach Number, starting at a gross weight of 150,000 pounds and consuming 35,000 pounds of fuel, and using not more than maximum cruise thrust (except maximum climb thrust may be used during a step climb) and using the conditions and operating rules defined below, shall not be less than the following guarantee value: NOMINAL: 3,185 Nautical Miles TOLERANCE: -65 Nautical Miles GUARANTEE: 3,120 Nautical Miles Conditions and operating rules: A step climb of 4,000 feet altitude may be used when beneficial to minimize fuel burn. The Manufacturer's Empty Weight (MEW) is guaranteed not to exceed the value in Section 03-60-00 of Detail Specification D6-38808-42-1 plus one percent.

Cruise Range. The still air range at an initial cruise altitude of 36,000 feet on a standard day at 0.85 Mach number, starting at a gross weight of 213,190 kilograms and consuming 68,040 kilograms of fuel, and using not more than maximum cruise thrust (except maximum climb thrust may be used during a step climb) and using the conditions and operating rules defined below, shall not be less than the following guarantee value: NOMINAL: [***] TOLERANCE: [***] GUARANTEE: [***] Conditions and operating rules: A step climb or multiple step climbs of 2,000 feet altitude may be used when beneficial to minimize fuel burn.