Take-Off Weight Clause Samples
The Take-Off Weight clause defines the maximum allowable weight of an aircraft at the moment it begins its takeoff roll. This includes the combined weight of the aircraft, fuel, passengers, cargo, and any other onboard items. In practice, this clause ensures that the aircraft does not exceed safety or regulatory limits, which could compromise performance or violate aviation standards. Its core function is to maintain operational safety and compliance by clearly specifying weight restrictions for flight operations.
Take-Off Weight. When operated under the conditions defined below (representative of […***…]): Pressure altitude : […***…] Ambient temperature : […***…] Take-Off Run Available (TORA) : […***…] Take-Off Distance Available (TODA) : […***…] Accelerate-Stop Distance Available (ASDA) : […***…] Line-up distance TORA / TODA / ASDA : […***…] Slope : […***…] Wind : […***…] Runway condition : […***…] Obstacles (height / distance from end of TORA) : […***…] : […***…] the permissible take-off weight at the start of ground run shall be not less than a guaranteed value of: […***…]
Take-Off Weight. 2.3.1 When operated under the following conditions (**) Pressure altitude :** Ambient temperature :** Take-off run available :** Take-off distance available :** Accelerate-stop distance available :** Slope :** Wind :** Line-up allowance T▇▇ :** Line-up allowance ASD :** Obstacles (Height/Distance above/from start of TODA): ** ** ** ** ** ** ** ** ** ** ** Confidential Treatment Requested. the maximum permissible take-off weight at the start of Take-off Distance Available will **
2.3.2 When operated under the following conditions (**) Pressure altitude :** Ambient temperature :** Take-off run available :** Take-off distance available :** Accelerate-stop distance available :** Slope :** Wind :** Line-up allowance T▇▇ :** Line-up allowance ASD :** Obstacles (Height/Distance above/from end of TODA): ** ** ** ** ** ** the maximum permissible take-off weight at the start of Take-off Distance Available will **.
2.3.3 When operated under the following conditions (**) Pressure altitude :** Ambient temperature :** Take-off run available :** Take-off distance available :** Accelerate-stop distance available :** Slope :** Wind :** Line-up allowance T▇▇ :** Line-up allowance ASD :** Obstacles (Height/Distance above/from end of TODA ** ** ** ** ** ** ** ** Confidential Treatment Requested. the maximum permissible take-off weight at the start of Take-off Distance Available will **. Note: This guarantee is based on an adapted take-off rating
2.3.4 When operated under the following conditions (**) Pressure altitude :** Ambient temperature :** Take-off run available :** Take-off distance available :** Accelerate-stop distance available :** Slope :** Wind :** Line-up allowance T▇▇ :** Line-up allowance ASD :** Obstacles (Height/Distance above/from start of TODA) :** the maximum permissible take-off weight at the start of Take-off Distance Available will **.
2.3.5 When operated under the following conditions (**) Pressure altitude :** Ambient temperature :** Take-off run available :** Take-off distance available :** Accelerate-stop distance available :** Slope :** Wind :** Line-up allowance T▇▇ :** Line-up allowance ASD :** Obstacles (Height/Distance above/from start of TODA): ** ** ** ** ** ** ** ** ** ** ** ** Confidential Treatment Requested. the maximum permissible take-off weight at the start of Take-off Distance Available will **
2.3.6 When operated under the following conditions (**) Pressure altitude : ** Ambient temperature : ** Take-off run available : ** Take-off d...
Take-Off Weight. When the A321 Aircraft is operated in departure airport conditions [*CTR*] as follows: Pressure altitude [*CTR*] Temperature [*CTR*] Take-Off Run Available (TORA) [*CTR*] Take-Off Distance Available (TODA) [*CTR*] Accelerate Stop Distance Available (ASDA) [*CTR*] Slope [*CTR*] Wind [*CTR*] Obstacles [*CTR*] (height and distance from beginning of TORA) [*CTR*] the FAR approved Take-Off Weight of the A321 Aircraft at the start of ground run shall be not less than:
Take-Off Weight. When the A319 Aircraft is operated in departure airport conditions [(*CTR)] as follows: Pressure altitude : [*CTR] Temperature : [*CTR] Take-Off Run Available (TORA) : [*CTR] Take-Off Distance Available (TODA) : [*CTR] CT1001520_Amended & Restated LA11A_AAL_A320Family_EXECUTION LA 11A - 2 of 11 [*CTR]=[CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] Accelerate Stop Distance Available (ASDA) : [*CTR] Slope : [*CTR] Wind : [*CTR] Obstacles : [*CTR] (height and distance from beginning of TORA) : [*CTR] the FAR approved Take-Off Weight of the A319 Aircraft at the start of ground run shall be not less than:
Take-Off Weight. 2.3.1 When operated under the following conditions (representative of *****): Ambient temperature : ***** Line-up allowance ▇▇▇ : ***** Line-up allowance ASD : ***** Pressure altitude : ***** Take-off run available : ***** Take-off distance available : ***** Accelerate-stop distance available : ***** Slope: ***** Wind: ***** Obstacles: : ***** (Height/Distance above/from start of TODA) ***** the maximum permissible take-off weight at the start of Take-off Distance Available shall be not less than a guaranteed value of *****.
2.3.2 When operated under the following conditions (representative of *****): Ambient temperature : ***** Line-up allowance ▇▇▇ : ***** Line-up allowance ASD : ***** Pressure altitude : ***** Take-off run available : ***** Take-off distance available : ***** Accelerate-stop distance available : ***** Slope: ***** Wind: ***** Obstacles: : ***** (Height/Distance above/from start of TODA) ***** the maximum permissible take-off weight at the start of Take-off Distance Available shall be not less than a guaranteed value of *****. ***** CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT.
Take-Off Weight. 2.3.1 When operated under the following conditions (representative of *****): Ambient temperature : ***** Line-up allowance ▇▇▇ : ***** Line-up allowance ASD : ***** Pressure altitude : ***** Take-off run available : ***** Take-off distance available : ***** Accelerate-stop distance available : ***** Slope: ***** Wind: ***** Obstacles: : ***** (Height/Distance above/from start of TODA) ***** the maximum permissible take-off weight at the start of Take-off Distance Available shall be not less than a guaranteed value of *****.
2.3.2 When operated under the following conditions (representative of *****): Ambient temperature : ***** Line-up allowance ▇▇▇ : ***** Line-up allowance ASD : ***** Pressure altitude : ***** Take-off run available : ***** Take-off distance available : ***** Accelerate-stop distance available : ***** Slope: ***** Wind: ***** Obstacles: : ***** (Height/Distance above/from start of TODA) ***** the maximum permissible take-off weight at the start of Take-off Distance Available shall be not less than a guaranteed value of *****. ***** CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT.