Takeoff. The FAA approved takeoff field length at a gross weight at the start of the ground roll of [***] pounds, at a temperature of [***]°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: [***] Feet
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:
2.1.2 The FAA approved takeoff gross weight at the start of ground roll, at a temperature of ***°F, at an altitude of *** feet, from a *** foot runway, with an alternate forward center of gravity limit of *** percent of the mean aerodynamic chord, and using maximum takeoff thrust, shall not be less than the following guarantee value:
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. 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. 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. 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. 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 field length at a gross weight at the start of the ground roll of *** pounds, at a temperature of ***°F, at a *** altitude, based on the certified alternate forward center of gravity limit, and using maximum takeoff thrust, shall not be more than the following guarantee value: NOMINAL: *** Feet TOLERANCE: ***Feet GUARANTEE: ***Feet
2.1.2 The FAA approved takeoff gross weight at the start of ground roll, at a temperature of ***°F, at an altitude of *** feet, from a *** foot runway, and satisfying the conditions defined below, based on the certified alternate forward center of gravity limit, and using maximum takeoff thrust, shall not be less than the following guarantee value: NOMINAL: *** Pounds TOLERANCE: ***Pounds GUARANTEE: ***Pounds 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: 1. *** feet *** feet 2. *** feet *** feet 3. *** feet *** feet 4. *** feet *** feet P.A. No. 03860 AERO-B-BBA7-M13-0469 SS13-0250 Attachment to Letter Agreement Xx. XXX-XX-00000-XX-0000000 GEnx-1B*** Engines
Takeoff. 2.1.1 The FAA approved takeoff field length at a gross weight at the start of the ground roll of [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] kilograms, at a temperature of [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT], at a sea level altitude, with an alternate forward center of gravity limit of per cent of the mean aerodynamic chord, and using maximum takeoff thrust, shall not be more than the following guarantee value: GUARANTEE: [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] Meters
2.1.2 The FAA approved takeoff field length at a gross weight at the start of the ground roll of [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] kilograms, at a temperature of [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT], at a sea level altitude, with an alternate forward center of gravity limit of per cent of the mean aerodynamic chord, and using maximum takeoff thrust, shall not be more than the following guarantee value: GUARANTEE: [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] Meters Engine derated to CFM56-7B24 thrust level. Attachment to Letter Agreement No. 6-1162-DME-1153 CFM56-7B27/B1 Engines Page 3
2.1.3 The FAA approved takeoff gross weight at the start of ground roll, at a temperature of [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT], at an altitude of feet and satisfying the conditions defined below, with an alternate forward center of gravity limit of [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] percent of the mean aerodynamic chord, and using maximum takeoff thrust, shall not be less than the following guarantee value: GUARANTEE: [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] Kilograms Conditions: The takeoff runway available (TORA) is [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] meters. The takeoff distance available (TODA) i...
Takeoff. 2.1.1 The FAA approved takeoff gross weight at the start of ground roll, at a temperature of [***********], at an altitude of [***********] and satisfying the conditions defined below, with an alternate forward center of gravity limit of [***********] of the mean aerodynamic chord, and using maximum takeoff thrust, shall not be less than the following guarantee value: GUARANTEE: [***********] Conditions: The takeoff runway available (TORA) is [***********]. The takeoff distance available (TODA) is [***********]. The accelerate-stop distance available (ASDA) [***********]. The lineup allowance adjustment to TORA and TODA [***********]. The lineup allowance adjustment to ASDA 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:
1. [***********] 13 feet 2. [***********] 24 feet 3. [***********] 60 feet
2.1.2 The FAA approved takeoff gross weight at the start of ground roll, at a temperature of [***********], at an altitude of [***********] and satisfying the conditions defined below, with an alternate forward center of gravity limit of [***********] of the mean aerodynamic chord, and using maximum takeoff thrust, shall not be less than the following guarantee value: GUARANTEE: [***********] “[***]” This information is subject to confidential treatment and has been omitted and filed separately with the commission
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 ***, at a sea level altitude, with an alternate forward center of gravity limit of *** percent of the mean aerodynamic chord, and using maximum ***, shall not be more than the following guarantee value: NOMINAL: * ** Feet TOLERANCE: * ** Feet GUARANTEE: * ** Feet
2.1.2 The FAA approved *** at the start of ground roll, at a temperature of ***, at an altitude of *** feet, from a *** foot runway, with an alternate forward center of gravity limit of *** percent of the mean aerodynamic chord, and using maximum ***, shall not be less than the following guarantee value: NOMINAL: * ** Pounds TOLERANCE: * ** Pounds GUARANTEE: * ** Pounds
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: ***
