Specific Range Sample Clauses

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 ***

Specific Range. The nautical miles per pound of fuel at an Aircraft gross weight of ** at a pressure altitude of ** conditions at a true Mach number of ** shall be not less than a guaranteed value of **.

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 ▇▇▇▇-up and […***…] fuel burn deterioration is equal to […***…]. 3 […***…] 3.1 […***…] The Aircraft shall be capable of carrying a […***…] of not less than […***…] over a still air stage distance of […***…] (assumed representative of […***…] with a 23 kt tailwind) when operated under the conditions defined below: 3.1.1 The departure airport conditions are as defined in Paragraph 2.1.3 above. The destination airport conditions are such as to allow the required […***…]. Pressure altitude is […***…]. 3.1.2 […***…] HAL - A320 Family HAL A321 PA – LA 9A […***…] *** Confidential Treatment Requested 3.2 […***…] 3.2.1 When carrying a […***…] of […***…] over a still air stage distance of […***…] (assumed representative of […***…] with a 23 kt tailwind) and when operated under the conditions defined in Paragraph 3.1 above the block […***…] shall be not more than a guaranteed value of […***…]. 3.2.2 When carrying a […***…] of […***…] over a still air stage distance of […***…] (assumed representative of […***…] with a 23 kt tailwind) and when operated under the conditions defined in Paragraph 3.1 above the block […***…] shall be not more than a guaranteed value of […***…]. Such a guarantee assumes that the required […***…] is permissible and is based on a fixed estimated Operating Weight Empty of […***…]. 3.3 […***…] The Aircraft shall be capable of carrying a […***…] of not less than […***…] over a still air stage distance of […***…] (assumed representative of […***…] with a 68 kt headwind) when operated under the conditions defined below: 3.3.1 The departure airport conditions are as defined in Paragraph 2.1.4 above. The destination airport conditions are such as to allow the required […***…]. Pressure altitude is […***…]. 3.3.2 […***…] HAL - A320 Family HAL A321 PA – LA 9A […***…] *** Confidential Treatment Requested 3.4 […***…] 3.4.1 When carrying a […***…] of […***…] over a still air stage distance of […***…] (assumed representative of […***…] with a 68 kt headwind) and when operated under the conditions defined in Paragraph 3.3 above the block […***…] shall ...

Specific Range. The nautical miles per pound of fuel at an New A321 (CFM Powered) Aircraft gross weight of ** at a pressure altitude of **in ** at a true Mach number of ** shall be not less than a guaranteed value of **.

Specific Range. The average nautical miles per kilogram of fuel (Average SR) at the weights and altitudes defined below in *** conditions at a true Mach number of *** Weight Pressure Altitude *** *** shall be not less than a guaranteed value of : Average SR = ***

Specific Range. 1.4.1 The nautical miles per pound of fuel at a New A321 (IAE Powered) Aircraft gross weight of ** at a pressure altitude of ** at a true Mach number of ** shall be not less than a guaranteed value of **. 1.4.2 The nautical miles per pound of fuel at a New A321 (IAE Powered) Aircraft gross weight of ** at a pressure altitude of ** at a true Mach number of ** shall be not less than a guaranteed value of **.

Specific Range. The nautical miles per kilogram of fuel at an Aircraft gross weight of * kg at a pressure altitude of * ft in ISA+10 degrees C conditions at a true Mach number of * shall be not less than * nm/kg.

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:

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 * 4.3.2. 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 Long Range Cruise Mach number of * shall be not less than * 4.3.3. 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 * 4.3.4. 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 Long Range Cruise Mach number shall be not less than * nm/kg. LETTER AGREEMENT NO 2 5. MANUFACTURER'S WEIGHT EMPTY GUARANTEE The Seller guarantees a Manufacturer's Weight Empty of not more than * This is the Manufacturer's Weight Empty of the Aircraft as defined in the paragraph 1 above, which will be derived from the weighing of the Aircraft and is subject to adjustment as defined in paragraph 8 below.