CPL POF RECAP 1

If a weight of 200kg acts over a 30mm arm what is the force?

• 6000kgmm

• 60kgmm

• 5kgmm

• Force cannot be in kgmm

What would the pressure altitude be, for an airfield with an elevation of 1368ft and a QNH of 1008?

• 1518

• 1218

• 1488

• 1248

Aileron use before a stall..

• Will prevent a wing drop

• Could lead to a wing drop

• Will have no effect on the wing drop stall

• Will instantly lead to a spin.

At 18,000ft, pressure compared to sea level would be..

• 25%

• 75%

• 50%

• 15%

How can we reduce induced drag?

• Winglets, taper, low AR, wing fences

• Drooping wings, washout, slats, high weight

• High AR, winglets, taper

• Dihedral, forward Center of gravity, low weight

What is the point called where air moving over the aerofoil comes to rest?

• Transition Point

• Stagnation point

• Separation point

• Center of pressure

If an aircraft increases altitude with a constant IAS, what happens to radius and rate of turn?

• Rate of turn decreases and radius increases

• Rate of turn increases and radius of turn increases

• Rate of turn decreases and radius of turn decreases

• Rate of turn increases and radius of turn decreases

In a venturi, increase in speed will cause:

• Decrease in dynamic pressure. Increase in static pressure

• Increase in dynamic pressure. Increase in static pressure

• Decrease in dynamic pressure and decrease in static pressure.

• Increase in dynamic pressure and decrease in static pressure.

At 60 degrees AoB the aircraft will experience a load factor of:

• 1G as gravity is always constant

• 2G

• The load factor is dependent on the IAS

• 3G

As an unstalled aerofoil increases its AOA

• The COP moves forward and the separation point moves aft

• The COP moves aft and the separation point moves forward

• The COP moves forward and the separation point moves forward

• The COP moves aft and the separation point moves aft