1) An autoland failure monitoring system must ensure that Report

the automatic pilot will automatically disengage whenever any failure is detected

the automatic pilot will automatically cause the aircraft to overshoot if any failure is detected

the aircraft will continue its automatic landing in the event of single failure

2) The effective gain of the glide path receiver Report

is increased as the aircraft descends

remains constant as the aircraft descends

is decreased as the aircraft descends

3) During an automatic landing , the aircraft descent rate is sensed by Report

pitch rate gyros

radio altimeters

vertical accelerometers

4) An autopilot with two separate power supplies is Report

fail passive

fail operational

fail redundant

5) On touchdown, autopilot Report

remains engaged ready for G/A

drives the throttles forward

disconnects after a short time

6) When will the decision height aural warning sound Report

at D.H

before D.H.

after D.H.

7) Automatic steering of the aircraft after touch down is affected by Report

the area navigation system

the runway localiser

the airfield marker beacon

8) The flare manoeuvre may be controlled by signals from Report

radio altimeter

the glide slope receiver

the localiser receiver

9) A triplex system looses one channel, the system is now Report

fail passive

fail operational

fail redundant

10) A fail passive system in the event of failure will Report

produce a significant out of trim condition

produce no significant out of trim condition

ensure the aircraft can still land automatically

11) A triplex system loses one channel, the system becomes a Report

simplex system

duplex system

dual-dual system

12) The two parameters used for category classification are Report

radio height/runway visual range

localiser and glideslope

decision height and runway visual range

13) What is the controlling factor in the automatic flare mode? Report

Decision height

Radio altimeter

Glideslope signal

14) C A T-3b allows Report

approach land and runway guidance with zero D H and R V R

approach land and R V R in the order of 50 meters

approach land and runway guidance with taxing visibility in the order of 50 meters

15) The definition of fail operational is the ability of a system to Report

disconnect and leave the aircraft in trim

continue to control after any first fault

disconnect but leave the aircraft out of trim

16) What is added to the flare computation at touchdown? Report

Nose down bias

Nose up bias

No signal

17) What controls are used in response to the P F D (Primary Flight Display) ? Report

Ailerons

Throttles

Nosewheel steering or rudder pedals

18) The ground run monitor (G R M) presents Report

distance to go

ground speed and distance to go

take off speed and distance to go

19) For a Vertical Gyro which is moved in pitch, which gimble would be moved to correct the pitch movement? Report

Lateral

Longitudinal

Normal

20) Versine is used in which channel? Report

Pitch

Roll

Yaw

EASA Questions Module%2013 Set%202

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