25

Question 1

The ideal air-fuel mixture ratio for kerosene is:

Answer 1

Greater than 15:1

Question 2

The component of a gas turbine engine which directs the airflow into the compressor is:

Answer 2

The inlet guide vanes

Question 3

Pilot input to the flight management computer (FMC) is made via the control/display unit (CDU). Which of the following statements is incorrect concerning the use and function of the
CDUs?

Answer 3

Both pilots can simultaneously enter information

Question 4

You have both the LOC and GS engaged. Which mode is displayed?

Answer 4

ILS on the EHSI

Question 5

The master warning system is subdivided into Warnings, Cautions and Advisories. After the system has been activated, it is common practice to press the Master or Warning Caution Light.
What happens when this is done?

Answer 5

The Master Warning or Master Caution light will go out

Question 6

You are conducting a couped ILS in APP mode and you wish to disengage the APP mode after LOC and G/s is captured. To do this you would:

Answer 6

Turn off the AP and both FD’s

Question 7

You have armed the AT. Which of the following correctly sets out the different modes which will engage it?

Answer 7

N1, SPD, VNAV, FLCH, GA

Question 8

You are in VNAV mode. Which of the following is the correct function of the IAS/MACH SELECTOR?

Answer 8

Pushing it alternately changes Speed Window between current IAS/MACH and a blank display

Question 9

Concerning A/P rudder control, which statement is correct?

Answer 9

The A/P always controls the rudder together with the ailerons and elevator whenever at least two A/Ps are engaged during a multi A/P ILS

Question 10

In which of the following EHSI modes is TCAS not displayed?

Answer 10

PLAN only

Question 11

Concerning the Autopilot (A/P) system and its control over the aircraft, which of the following statements is correct?

Answer 11

The A/P controls the aileron and elevator and adds rudder only during a multi A/P
approach

Question 12

Your FD has just failed in pitch mode. What will be the result?

Answer 12

Only the pitch command bars will disappear

Question 13

On the ground and in the air, the position of the rudder is shown on the flight deck. How is this achieved?

Answer 13

On the EICAS status display

Question 14

An aircraft lands with the auto brakes armed. When will the brakes be applied?

Answer 14

After main landing gear truck untilt and wheel spinup have occurred

Question 15

Leading and trailing edge flaps are:

Answer 15

Extended and retracted simultaneously

Question 16

With reference to the cancellation of GPWS warnings and alerts when in the excessive terrain closure rate mode and not in the landing configuration:

Answer 16

The warning is silenced when the closure rate envelope penetration no longer exists but the alert requires a barometric altitude gain to be silenced