Mission Payload. The payload for a stage length of [*] nautical miles in still air (equivalent to a distance of [*] nautical miles with a [*] wind, representative of a [*] route in [*]) using the conditions and operating rules defined below, shall not be less than the following guarantee value: NOMINAL: [*]0 Kilograms TOLERANCE: [*] Kilograms GUARANTEE: [*] Kilograms
Mission Payload. The A340-300 Aircraft shall be capable of carrying a guaranteed Payload of not less than ** over a still air stage distance of ** when operated under the conditions defined below:
3.19.1 The departure airport conditions ** are as defined in paragraph 2.3.2 above. The destination airport conditions are such to allow the required Landing Weight to be used without any restriction. Pressure altitude is **.
3.19.2 An allowance of ** of fuel and ** is considered for engine start-up and taxi-out.
3.19.3 An allowance of ** of fuel and ** is included for take-off and climb to ** pressure altitude with acceleration to climb speed at a temperature of **. No credit is taken for the distance covered in these segments.
Mission Payload. The payload for a stage length of *** nautical miles in still air (representative of a *** route in summer) using the conditions and operating rules defined below, will not be less than the following *** value: NOMINAL: *** pounds TOLERANCE: *** pounds ***: *** pounds Conditions and operating rules:
Mission Payload. The payload for a stage length of [****] nautical miles in still air (representative of a [****]) using the conditions and operating rules defined below, will not be less than the following [****]: [****]: [****] The above [****]. [****]:
Mission Payload. The payload for a stage length of *** in still air (representative of a *** route in the winter season) using the conditions and operating rules defined below, shall not be less than the following guarantee value: *** Conditions and operating rules: *** The following obstacle definition is based on a straight out departure where obstacle height and distance are specified with reference to the liftoff end of the runway:
Mission Payload. The payload for a stage length of 2,712 nautical miles in still air (equivalent to a distance of 2,313 nautical miles with a 68 knot headwind, representative of a Los Angeles to Honolulu route in Winter) using the conditions and operating rules defined below, shall not be less than the following guarantee value: NOMINAL: [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] TOLERANCE: GUARANTEE: Conditions and operating rules:
Mission Payload. The payload for a stage length of *** nautical miles in still air (equivalent to a distance of *** nautical miles with a *** knot headwind, representative of a *** to *** route in ***) using the conditions and operating rules defined below, shall not be less than the following guarantee value: NOMINAL: ***Pounds TOLERANCE: ***Pounds GUARANTEE: ***Pounds Conditions and operating rules:
Mission Payload. The payload for a stage length of 4,626 nautical miles in still air (equivalent to a distance of 4,277 nautical miles with a 38 knot headwind, representative 71 Attachment to Letter Agreement No. 6-1162-DSF-082 CF6-80C2BIF Engines Page 7 of an Anchorage to Taipei route) using the conditions and operating rules defined below, shall not be less than the following guarantee value:
Mission Payload. The payload for a stage length of [*CTR] nautical miles in still air (representative of a [*CTR]) using the conditions and operating rules defined below, shall not be less than the following guarantee value: [*CTR] Conditions and operating rules:
Mission Payload. The payload for a stage length of *** nautical miles in still air (equivalent to a distance of *** nautical miles with a *** knot headwind, representative of a Xiamen to Harbin route) using the conditions and operating rules defined below, shall not be less than the following guarantee value:
