class A aircraft takeoff

#34. The climb limited take-off mass can be increased by:

• Aselecting a lower VR.
• Ba lower flap setting for take-off and selecting a higher V2.
• Cselecting a lower V1.
• Dselecting a lower V2.

#1. For a given take-of mass, the maximum brake energy limit speed (VMBE), as an indicated airspeed, will:

• ADecrease with increasing altitude, and decrease with increasing temperature.
• BIncrease with increasing altitude and increase with increasing temperature.
• CDecrease with increasing altitude, and increase with increasing temperature.
• DNot change with altitude, but decrease with increasing temperature.

#2. Provided all other parameters stay constant, Which of the following statements will decrease the take-off ground run?

• ADecreased take-off mass, increased pressure altitude, increased temperature.
• BDecreased take-off mass, increased density, increased flap setting.
• CIncreased pressure altitude, increased outside air temperature, increased take-off mass.
• DIncreased outside air temperature, decreased pressure altitude flap setting.8