Take Off Climb

#1. The net flight path climb gradient after take-off compared to the gross climb gradient is:

• Alarger.
• Bequal.
• Cdepends on type of aircraft
• Dsmaller.

#2. Given that the characteristics of a three engine turbojet aeroplane are as follows: Thrust = 50,000 N per engine g = 10 m/s² Drag = 72,569 N Minimum gross gradient (2nd segment) = 2.7% The maximum take-off mass under segment two conditions in the net take-off flight path conditions is:

• A101,596 kg
• B286,781 kg
• C74,064 kg
• D209,064 kg

#3. During the flight preparation the climb limited take-off mass (TOM) is found to be much greater than the field length limited TOM using 5° flap. In what way can the performance limited TOM be increased? There are no limiting obstacles.

• ABy selecting a higher flap setting.
• BBy selecting a higher V2.
• CBy selecting a lower V2.
• DBy selecting a lower flap setting.