1) When can the F M S be engaged with the autothrottle Report

only with the Flight Director selected

With either the Flight Director or the Digital Control System (D F C S) engaged

only after take off

2) A full authority Digital Engine Control System (F A D E C) consists of Report

Electronic engine control unit only

Electronic engine control unit and all its sensors

Electronic engine control unit and throttle position transmitter

3) A 'F A D E C' system does not have the following system? Report

An automatic starting capability

Control of thrust reverser operation

Automatic control of engine fire extinguishers

4) Which is the correct sequence for an autoland? Report

Glideslope capture, altitude hold and flare

Localiser capture, glideslope capture, attitude hold and flare

Localiser capture, glideslope capture, flare and attitude hold

5) The wheel height at which the approach path has been visually assessed as satisfactory to continue the approach to a landing is know as the Report

decision height

intercept height

alert height

6) The I C A O weather category 3 A is Report

operation down to and along the surface of the runway without external reference

operation down to 60 m and 800 m

operation down to and along the surface of the runway with R V R of 200m

7) A category II facility performance I L S has an intercept height of Report

15 m

60 m

0 m

8) The facility performance I L S intersect height is the point Report

where the aeroplane receives the first glide path signal

the localiser and glide path signals cross each other

where the aeroplanes first receives both the localiser and glide path signals

9) The average risk of autoland should not contribute a rate of fatal accidents per landing greater than Report

1 x 10-6

1 x 10-7

1 x 10-8

10) Before an aeroplane is able to make an automatic landing the Report

ground radio aids must be at least C A T II

ground radio aids must be at C A T III

I L S system must be working

11) For an aeroplane to be certified for automatic landing an autothrottle system is Report

mandatory

a matter of choice for the operator

dependent upon the operation of the aeroplane at slow speed

12) The overshoot or go around mode is initiated Report

automatically

by a selector on the throttle control panel

by pushing the throttles forward to maximum

13) The aeroplanes autopilot is programmed to leave the glide slope at Report

300 ft

the decrab phase

start of flare phase

14) Overshoot or go-around mode can be initiated Report

only when the autopilot is engaged

at any time after autoland has been engaged

at any time

15) The following modes may be retained when overshoot has been initiated after the selection of autoland Report

I L S localiser and I A S

I A S and glide slope

I A S and steering or heading

16) If go-around has been initiated after autoland has been selected, the aeroplane will Report

increase speed

rotate nose up

increase speed and rotate nose up

17) V NAV (Vertical NAVigation) can be selected Report

Alone

Only if A / P and F / D selected

Only if A / T selected

18) If during autoland the L O C signal is lost at 400 ft in final approach Report

the system degrades to C A T II

the autoland is continued

a go-around is initiated

19) The order of autoland approach is Report

L O C, G S, A T T H O L D, F L A R E

G S, L O C, A T T H O L D, F L A R E

L O C, G S, F L A R E, A T T H O L D

20) Purpose of an autoland decrabbing manoeuvre is to Report

assist with localiser tracking

assist with glideslope tracking

point the aircraft down the runway at touch down

EASA Questions Module 13 Set 2

Set 1

Set 2

Set 3

Set 4

Set 5

Set 6

Set 7

Set 8

Set 9

Set 10

Set 11

Set 12