Takeoff. 2.1.1 The FAA approved takeoff field length at a gross weight at the start of the ground roll of *** pounds, at a temperature of ***°F, at a sea level altitude, with an alternate forward center of gravity limit of *** percent of the mean aerodynamic chord, and using maximum takeoff thrust, shall not be more than the following guarantee value: GUARANTEE: *** Feet
Takeoff. The FAA approved takeoff field length at a gross weight at the start of the ground roll of 174,200 pounds, at a temperature of 30°C, 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: 7,950 Feet
Takeoff. 2.1.1 The FAA approved takeoff gross weight at the start of ground roll, at a temperature of ***, at an altitude of ***, from a *** runway, satisfying the conditions defined below, and using maximum takeoff thrust, shall not be less than the following guarantee value: *** Conditions: ***
Takeoff. 2.1.1 The FAA-approved takeoff field length at a gross weight at the start of the ground roll of *** pounds, at a temperature of ***°F, at a sea level altitude, with an alternate forward center of gravity limit of *** percent of the mean aerodynamic chord, and using maximum takeoff thrust, will not be more than the following *** value: NOMINAL: *** feet TOLERANCE: *** feet ***: *** feet
Takeoff. Based on the TLC or Octopus software this module provides take-off performance from a given airfield. Computation accounts for elements such as, but not limited to, runway conditions, inoperative items and provides direct information to the pilot. • Landing Based on the TLC or Octopus software this module provides landing performance on a given airfield. Computation accounts for elements such as, but not limited to, runway conditions, inoperative items and provides direct information to the pilot.
Takeoff. The most senior applicant within the same classification will be awarded the position first until the vacancies within the classification have been filled. Should there be no applicants within the Takeoff positions, the job will be awarded to the applicant according to 24.01. CORRUGATOR SINGLE FACE/KNIFE OPERATOR DOUBLE BACKER UTILITY CLAMP TRUCK STACKER Vacancies will be posted. For the purpose of Job Postings and the Line of Progression the Single Face Operator and Knife Operator will be considered the same classification. Vacancies will be awarded by seniority in the same classifi- cation and then by seniority in the classification immediately below and so on. Should there be no applicant within the line, the applicant will be awarded the job according to 24.01.
Takeoff. 2.1.1 The FAA approved takeoff gross weight at the start of ground roll, at a temperature of [*CTR] at an [*CTR], from a [*CTR] runway, and satisfying the conditions defined below, and using maximum takeoff thrust, shall not be less than the following guarantee value: GUARANTEE: [*CTR] Conditions: The runway slope is [*CTR]. 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
Takeoff. 2.1.1 The FAA approved takeoff gross weight at the start of ground roll, at a temperature of ***, at an altitude of ***, from a *** runway, satisfying the conditions defined below, and using maximum takeoff thrust, shall not be less than the following guarantee value: *** Conditions: 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. ***
Takeoff. 2.1.1 The FAA-approved takeoff gross weight at the start of groundroll, at a temperature of. , at an altitude of , with an alternate forward center of ravit limit of [*CTR] takeoff thrust, and using the conditions defined below, will not be less than the following guarantee value: GUARANTEE: [*CTR] Condtiions: The takeoff runway available (TORA) is [*CTR] The takeoff distance available (TODA) is [*CTR] The accelerate-stop distance available (ASDA) is - [*CTR] The lineup allowance adjustment to TORA and TODA is II [*CTR] The lineup allowance adjustment to ASDA is - . The runway slope [*CTR] The minimum level off height is - .
Takeoff. 2.1.1 The FAA approved takeoff gross weight at the start of ground roll, at a temperature of [****], at an altitude of [*****], from a [****] meter runway, and satisfying the conditions defined below, and using maximum takeoff thrust, shall not be less than the following guarantee value: [*******************************] [*******************************] [*******************************] Conditions: The stopway is [********]. The runway slope is [**************]. 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
