Common use of Takeoff Clause in Contracts

Takeoff. 2.1.1 The FAA approved takeoff field length at a gross weight at the start of the ground roll of 187,700 pounds, at a temperature of 86°F, at a sea level altitude, with an alternate forward center of gravity limit of 15 percent of the mean aerodynamic chord, and using maximum takeoff thrust, shall not be more than the following guarantee value: [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT]t 2.1.2 The FAA approved takeoff gross weight at the start of ground roll, at a temperature of 95°F, at an altitude of 607 feet and satisfying the conditions defined below, with an alternate forward center of gravity limit of 15 percent of the mean aerodynamic chord, and using maximum takeoff thrust, shall not be less than the following guarantee value: [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] Conditions: The takeoff runway available (TORA) is 12,816 feet. The takeoff distance available (TODA) is 12,816 feet. The accelerate-stop distance available (ASDA) is 12,816 feet. The runway slope is 0.03 percent downhill.

Takeoff. 2.1.1 The FAA approved takeoff field length at a gross weight at the start of the ground roll of 187,700 154,500 pounds, at a temperature of 86°F, at a sea level altitude, with an alternate forward center of gravity limit of 15 percent of the mean aerodynamic chord, and using maximum takeoff thrust, shall not be more than the following guarantee value: [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT]tTREATMENT] 2.1.2 The FAA approved takeoff gross weight at the start of ground roll, at a temperature of 95°F, at an altitude of 607 feet and satisfying the conditions defined below, with an alternate forward center of gravity limit of 15 percent of the mean aerodynamic chord, and using maximum takeoff thrust, shall not be less than the following guarantee value: [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] Conditions: The takeoff runway available (TORA) is 12,816 feet. The takeoff distance available (TODA) is 12,816 feet. The accelerate-stop distance available (ASDA) is 12,816 feet. The runway slope is 0.03 percent downhill.

Takeoff. 2.1.1 The FAA approved takeoff field length at a gross weight at the start of the ground roll of 187,700 pounds, at a temperature of 86°F, at a sea level altitude, with an alternate forward center of gravity limit of 15 percent of the mean aerodynamic chord, and using maximum takeoff thrust, shall not be more than the following guarantee value: [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT]tTREATMENT] 2.1.2 The FAA approved takeoff gross weight at the start of ground roll, at a temperature of 95°F, at an altitude of 607 feet and satisfying the conditions defined below, with an alternate forward center of gravity limit of 15 percent of the mean aerodynamic chord, and using maximum takeoff thrust, shall not be less than the following guarantee value: [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] Conditions: The takeoff runway available (TORA) is 12,816 feet. The takeoff distance available (TODA) is 12,816 feet. The accelerate-stop distance available (ASDA) is 12,816 feet. The runway slope is 0.03 percent downhill.