Specific Range Sample Clauses

Specific Range. 1.5.1 The nautical miles per pound of fuel at an A319 Aircraft gross weight of 145,000 lb at a pressure altitude of 35,000 ft in ISA+10(degree)C conditions at a true Mach number of 0.78 will be not less than a guaranteed value of 0.0833 nm/lb.
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Specific Range. The average nautical miles per kilogram of fuel (Average SR) at the weights and altitudes defined below in ISA conditions at a true Mach number of *** Weight Pressure Altitude *** *** *** *** *** *** *** *** *** *** shall be not less than a guaranteed value of : Average SR ***
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Specific Range. 1.2.1 The nautical miles per pound of fuel at an Original A320 Aircraft gross weight of ** at a pressure altitude of ** conditions at a true Mach number of ** will be not less than a guaranteed value of **
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Specific Range. 4.3.1. The nautical miles per kilogram of fuel at an Aircraft gross weight of * at a pressure altitude of * in ISA+10 degrees C conditions at a true Mach number of * shall be not less than *
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Specific Range. The Specific Range at a cruise weight of […***…] at a pressure altitude of […***…] in ISA conditions at a True Mach number of […***…] using thrust not exceeding maximum cruise thrust shall be not less than a guaranteed value of […***…]. For information: The corresponding nominal Specific Range with […***…] fuel burn deterioration is equal to […***…]. The corresponding nominal Specific Range with […***…] fuel xxxx-up and […***…] fuel burn deterioration is equal to […***…]. 3 […***…]
Sample 1Sample 2
Specific Range. The nautical miles per kilogram of fuel at an Aircraft gross weight of "A" kg at a pressure altitude of "B" feet in ISA conditions at an airspeed or true Mach number of "C" shall be not less than a value of "D" nautical miles per kilogram.
Sample 1
Specific Range. 1.2.1 The nautical miles per pound of fuel at an Aircraft gross weight of [...***...] lb. at a pressure altitude of [...***...] ft in ISA+10(degrees) C conditions at a true Mach number of [...***...] will be not less than a guaranteed value of [...***...] nm/lb.
Sample 1
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Specific Range. At the three conditions presented below, the specific range of the Aircraft with a maneuver margin to FAA-approved buffet boundary of not less than 1.3g, with thrust not in excess of maximum cruise thrust is guaranteed to be no less than the values presented below:
Sample 1

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