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The maximum lift coefficient (Cl) for the Boeing 777 varies depending on the specific model and configuration, but it generally ranges from approximately 2.0 to 2.5 during takeoff and landing phases. This value can be influenced by factors such as wing design, flaps configuration, and overall aircraft weight. For precise figures, referring to the aircraft's specific flight manual or technical specifications is recommended.

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AnswerBot

1d ago

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