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As a result, the maximum takeoff weight was increased to .
But the maximum takeoff weight was not increased for the E-model.
Increased maximum takeoff weight allows aircraft to carry more fuel and have longer range.
The new design was required to have an empty weight less than half its maximum takeoff weight.
Maximum takeoff weight for the F-18 is twenty-three thousand kilograms.
The maximum takeoff weight of an aircraft is unlimited.
Benefits include improved range and endurance and an increased maximum takeoff weight.
Climb to flight level 450 at maximum takeoff weight is possible without a step climb.
Increased maximum takeoff weight, strengthened fuselage with enlarged cabin, 172 built.
"These airplanes have 1:1 thrust-to-weight ratio at maximum takeoff weight!
Consequently, anything that can be done to improve the single-engine-inoperative climb performance will bring about an increase in maximum takeoff weight.
It also has an increased maximum takeoff weight, allowing for more cargo and greater range (up to 1,500 nm).
VLJs are defined in the industry as having a maximum takeoff weight of not more than 10,000 pounds.
When it stood at the end of the runway, ready to roll, it was over its approved maximum takeoff weight for the given conditions.
The new model was designed to a lower maximum takeoff weight with a modified wing and a lightened airframe.
The Comet 4 was considered the definitive series, having a longer range, higher cruising speed and higher maximum takeoff weight.
It is greater than the maximum takeoff weight due to the fuel that will be burned during the taxi and runup operations.
The only major development of the Dash 7 was the Series 150, which featured a higher maximum takeoff weight and greater fuel capacity, boosting range.
Maximum takeoff weights remained the same, but there was a slight reduction in payload because of the heavier engines.
The fuel capability of this plane increased by 1072 pounds and so did the maximum takeoff weight by 750 pounds.
Upgraded civil transport version with composite rotor blades and with higher maximum takeoff weight.
This increased commonality will allow a higher maximum takeoff weight, which will increase the range (or payload) of the A350-800 compared to initial plans.
Although uncommon, it can exceed the maximum takeoff weight (MTOW).
The more powerful engine did not increase the maximum takeoff weight but allowed operations at higher altitudes, and its lower output speed helped reduce propeller noise.
Many of the vortex generator kits available for light twin-engine airplanes bring with them the added benefit of an increase in maximum takeoff weight.
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