EVALUATION Q.T : K.A 200 ENGLISH

What is the purpose of the rudder boost system?

• A. It provides yaw dampening

• B.It boosts the rudder against a failed engine

•   C. It prevents the pilot from excessive yaw inputs

• Both A and B are correct

- The stall warning system provides..

• Stall warning to the aircraft mechanic to assist with control rigging

• Pre-stall warning to the pilot

•    Post-stall warning to the pilot

• Stall information is used to determine flap position

During a ground start of the right engine, the IGNITION ON light should illuminate:

• At 10% N1 rpm.

• When the condition lever is moved to LO IDLE.

• At a stabilized 12% N1.

• When the start switch is moved to the IGNITION and ENGINE START position.

Choose the correct statement:

     

• Use of flap improves climb performance.

• The right inboard flap is the master flap.

• The flap position transmitter and limit switches are on the left inboard flap.

• It is advisable to extend approach flap in turbulence to facilitate speed control and stability.

Oil brands:

 

• May be mixed but only in an emergency.

• May be mixed provided they are both natural oils.

• May not be mixed at all.

• May be mixed provided they are both synthetic oils.

Fuel is heated before entering the FCU by:

 

• Hot air from the engine oil cooler.

• An electric element and heated tank vents.

• Fuel heater .

• Anti-ice boots.

Fuel is transferred from the aux tank to the Nacelle by.

• Gravity

• Compressed air

• Electrically

• Jet pump

The fuel quantity indicating system is....

• A mechanical type which reads in imperial gallons

• A capacitance type that is compensated for specific gravity and reads in pounds

•   An electrical indicating system using variable resistors and reads in pounds

• A capacitance system compensating for specific density and reads in pounds

An emergency exit door is installed....

  

• On the left fuselage in the centre of the cabin compartment

• On the right fuselage at the forward end of the passenger compartment

• On the right fuselage at the rear of the passenger compartment

• There is no emergency exit provision on the aircraft

The cabin pressure is controlled by:

   

• A.Modulation of inflow air by the flow control packages on each firewall.a;

• B.Modulation of the outflow air by the cabin pressure controller through the outflow valve.

• A combination of A and B.

• Modulation of the outflow by the cabin pressure controller through the outflow valve and the safety valve