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How do you calculate the ACL for a C-17? - Answers
To calculate the Average Cargo Load (ACL) for a C-17, you need to consider its maximum payload capacity, which is approximately 170,900 pounds (77,519 kg). The ACL is determined by subtracting the weight of the aircraft's fuel, crew, and any other mission-essential equipment from this maximum payload capacity. Additionally, the specific configuration of the load, including the distribution of weight and center of gravity considerations, can also influence the effective ACL for a particular mission. Always refer to the aircraft's flight manual for precise calculations and constraints.
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How do you calculate the ACL for a C-17? - Answers
To calculate the Average Cargo Load (ACL) for a C-17, you need to consider its maximum payload capacity, which is approximately 170,900 pounds (77,519 kg). The ACL is determined by subtracting the weight of the aircraft's fuel, crew, and any other mission-essential equipment from this maximum payload capacity. Additionally, the specific configuration of the load, including the distribution of weight and center of gravity considerations, can also influence the effective ACL for a particular mission. Always refer to the aircraft's flight manual for precise calculations and constraints.
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How do you calculate the ACL for a C-17? - Answers
To calculate the Average Cargo Load (ACL) for a C-17, you need to consider its maximum payload capacity, which is approximately 170,900 pounds (77,519 kg). The ACL is determined by subtracting the weight of the aircraft's fuel, crew, and any other mission-essential equipment from this maximum payload capacity. Additionally, the specific configuration of the load, including the distribution of weight and center of gravity considerations, can also influence the effective ACL for a particular mission. Always refer to the aircraft's flight manual for precise calculations and constraints.
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- og:descriptionTo calculate the Average Cargo Load (ACL) for a C-17, you need to consider its maximum payload capacity, which is approximately 170,900 pounds (77,519 kg). The ACL is determined by subtracting the weight of the aircraft's fuel, crew, and any other mission-essential equipment from this maximum payload capacity. Additionally, the specific configuration of the load, including the distribution of weight and center of gravity considerations, can also influence the effective ACL for a particular mission. Always refer to the aircraft's flight manual for precise calculations and constraints.
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