最大起飞重量（Maximum Take-Off Weight）是指因设计或运行限制，航空器能够起飞时所容许的最大重量。最大起飞重量是航空器的三种设计重量限制之一，其余两种是最大零燃油重量和最大着陆重量。
中断起飞过程中，取决于刹车吸收预定能量之能力的最大起飞重量。
The maximum takeoff weight based on the ability of the brakes to absorb a predetermined amount of energy during a rejected takeoff.
爬升限重，取决于由一台发动机工作时的最低爬升梯度的最大起飞重量。
Climb LIMIT weight, Maximum takeoff weight based on a minimum climb gradient with one engine inoperative.
刹车能量极限重量，中断起飞过程中，取决于刹车吸收预定能量之能力的最大起飞重量。
Brake energy LIMIT weight, the maximum takeoff weight based on the ability of the brakes to absorb a predetermined amount of energy during a rejected takeoff.
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