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.
在一发不工作起飞后的爬升中为保证足够的梯度能力和操纵裕度所飞的速度。
The speed flown after takeoff during engine-out climbout maneuvers to assure adequate gradient capability and maneuver margin.
在一发不工作起飞后的爬升中为保证足够的梯度能力和操纵裕度所飞的速度。
The speed flown after takeoff during engine-out climbout maneuvers to assure adequate gradient capability and maneuver margin.
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