Common use of Mission Payload Clause in Contracts

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: Stage Length: The stage length is defined as the sum of the distances for the climbout maneuver, climb, cruise, and descent. Takeoff: The airport altitude is *** feet. The airport temperature is ***°F. The takeoff runway available (TORA) is *** feet. The takeoff distance available (TODA) is *** feet. The accelerate-stop distance available (ASDA) is *** feet. The lineup allowance adjustment to TORA and TODA is *** feet. The lineup allowance adjustment to ASDA is *** feet. The runway slope is *** percent uphill. 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: Distance Height

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: Stage Length: The stage length is defined as the sum of the distances for the climbout maneuver, climb, cruise, and descent. Takeoff: The airport altitude is *** feet. The airport temperature is ***°F. The takeoff runway available (TORA) is *** feet. The takeoff distance available (TODA) is *** feet. The accelerate-stop distance available (ASDA) is *** *feet. The lineup allowance adjustment to TORA and TODA is *** feet. The lineup allowance adjustment to ASDA is *** feet. The runway slope is *** percent uphill. 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: Distance Height

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: Stage Length: The stage length is defined as the sum of the distances for the climbout maneuver, climb, cruise, and descent. Takeoff: The airport altitude is *** feet. The airport temperature is ***°F. The takeoff runway available (TORA) is *** feet. The takeoff distance available (TODA) is *** feet. The accelerate-stop distance available (ASDA) is *** feet. The lineup allowance adjustment to TORA and TODA is *** feet. The lineup allowance adjustment to ASDA is *** feet. The runway slope is *** percent uphilldownhill. 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: Distance HeightBoeing / United Air Lines, Inc. Proprietary

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: Stage Length: The stage length is defined as the sum of the distances for the climbout maneuver, climb, cruise, and descent. Takeoff: The airport altitude is *** feet. The airport temperature is ***°F. The takeoff runway available (TORA) is *** *feet. The takeoff distance available (TODA) is *** *feet. The accelerate-stop distance available (ASDA) is *** feet. The lineup allowance adjustment to TORA and TODA is *** feet. The lineup allowance adjustment to ASDA is *** feet. The runway slope is *** percent uphilldownhill. 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: Distance Height