1) The flight director is on a localizer when the radio deviation signal is lost the aircraft would Report

continue on flying on the localizer

fly parallel to the localizer

drift of from the localizer on the same heading

2) Cat-2 autoland DH limits are Report

below 200 feet but not less than 100 ft

below 500 feet but not less than 400 ft.

below 300 feet and not less than 200 ft.

3) Cat-1 autoland DH limits are Report

not less than 100 ft.

not less than 200 ft.

below 200 ft but not less than 100 ft.

4) When GA is initiated? Report

Auto throttle disengages at 2000 ft/min rate and wings will level

Auto throttle remains engaged allowing pilot to control the throttles

Auto throttle remains engaged giving correct G/A thrust

5) The controlling signal in pitch channel in the Flare mode are Report

integrated pitch and radio altitude.

G/S deviation and radio altitude.

integrated pitch and G/S deviation

6) During autoland failure of one channel is detected Report

all channels will disconnect in triplex system.

all channels will disconnect in dulpex system.

all channels will disconnect in dual-dual system.

7) In triplex autoland system failure of one channel will Report

disconnect all channels

disconnect the failure channel and continue autoland approach

disconnect the failure channel and continue with a manual approach

8) During the flair mode the A/T throttle will Report

retard throttle to idle.

disconnect autothrottle

select reverse thrust.

9) Roll out mode occurs Report

after flare

before flare

at alert height

10) Basic monitoring is function of Report

voting

signal comparison

signal summing

11) In series rudder system Report

the pilot cannot input to the system

the pilot can input to the system

yaw damping is only possible signal input

12) In parallel rudder system, Report

the pilot can input on rudder pedals

The rudder pedals move in response to rudder movement

The rudder pedals are disconnected

13) The aileron/rudder signal is demodulated in the rudder channel amplifier. This means it is Report

AC

DC

DC output whose polarity is related to the phase of AC input

14) An increase in mach number will cause the Report

Cof P to move rearwards giving less downwash on the tail plane

Cof P to move rearwards giving more downwash on the tail plane

Cof P to move forwards giving less downwash on the tail plane

15) If one FMS fails in a duel system Report

system operation will not be affected

FMS CDU on fail side goes blank

FMS display transfers automatically from serviceable computer

16) To carry out FMS database update on FMS Report

use database loader

insert new EPROM

insert new data on CDU

17) To know the valid database on FMS Report

perform bite check

call up relevant page on CDU

call up relevant current status

18) Magnetic heading errors will be Report

positive if easterly

negative if easterly

negative if northerly

19) What will happen with a flux valve in a turn? Report

It will move once the aircraft is established on a new heading

Move as the aircraft moves

Stay fixed on magnetic north

20) A helicopter autopilot uses Report

radio altitude for height hold and barometric altitude for altitude hold

barometric altitude for height hold and radio altitude for altitude hold

barometric altitude for both height and altitude hold

EASA Questions Module 13 Set 6

Set 1

Set 2

Set 3

Set 4

Set 5

Set 6

Set 7

Set 8

Set 9

Set 10

Set 11

Set 12