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 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: [*CTR*] 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: [*CTR*]

Takeoff. 2.1.1 The FAA approved takeoff field length at a gross weight at the start of the ground roll of 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: [GUARANTEE: *CTR*]* Feet 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*** feet, from a *** foot runway, 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: [GUARANTEE: *CTR*]* Pounds

Takeoff. 2.1.1 The FAA approved takeoff field length at a gross weight at the start of the ground roll of 154,500 187,700 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: [*CTR*]: 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: [*CTR*]: