Common use of Specific Range Clause in Contracts

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 be not more than a guaranteed value of […***…]. 3.4.2 When carrying a […***…] of […***…] over a still air stage distance of […***…] (assumed representative of […***…] with a 68 kt headwind) and HAL - A320 Family HAL A321 PA – LA 9A […***…] *** Confidential Treatment Requested when operated under the conditions defined in Paragraph 3.3 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 […***…]. 3.5 […***…] The Aircraft shall be capable of carrying a […***…] of not less than […***…] over a still air stage distance of […***…] (assumed representative of […***…] with a 67 kt headwind) when operated under the conditions defined below: 3.5.1 The departure airport conditions are such as to allow […***…]. Pressure altitude is […***…]. The destination airport conditions are such as to allow […***…]. Pressure altitude is […***…]. […***…] HAL - A320 Family HAL A321 PA – LA 9A […***…] *** Confidential Treatment Requested

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 9B […***…] *** 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 9B […***…] *** 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 be not more than a guaranteed value of […***…]. 3.4.2 When carrying a […***…] of […***…] over a still air stage distance of […***…] (assumed representative of […***…] with a 68 kt headwind) and HAL - A320 Family HAL A321 PA – LA 9A 9B […***…] *** Confidential Treatment Requested when operated under the conditions defined in Paragraph 3.3 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 […***…]. 3.5 […***…] The Aircraft shall be capable of carrying a […***…] of not less than […***…] over a still air stage distance of […***…] (assumed representative of […***…] with a 67 kt headwind) when operated under the conditions defined below: 3.5.1 The departure airport conditions are such as to allow the […***…]. Pressure altitude is […***…]. The destination airport conditions are such as to allow the […***…]. Pressure altitude is […***…]. […***…] HAL - A320 Family HAL A321 PA – LA 9A 9B […***…] *** Confidential Treatment Requested