1) Krueger flaps make up part of the Report

wing upper surface leading edge

wing lower surface trailing edge

wing lower surface leading edge

2) Electronic stab trim switches are found on the Report

control column

flight control panel

3) Emergency electronic equipment for the cabin is referred to in Report

BCARs

JAR OPS subpart M

maintenance manual

4) Carbon microphones require Report

DC supply

AC supply

no supply

5) A CVR is found to be unserviceable Report

flight can continue with serviceable FDR provided they are not combined

flights must not continue after four days

flights must not continue after 72 hours

6) The maximum azimuth coverage by a MLS facility is Report

+/- 35 degrees

+/-40 degrees

+/-60 degrees

7) Fibre glass parts are protected from lightning strikes and dangerous voltages by Report

non conductive paint

conductive paint

earth primary conductors

8) The pseudo-random code used by all civilian GPS users is Report

the y code

the p code

the c/a code

9) On localiser approach the radio deviation signal is lost Report

the aircraft flies in a circle

aircraft flies off centre line on pre-set heading

aircraft flies heading with increasing drift angle

10) Q' feel for the stabiliser requires Report

pitot only

static only

pitot and static

11) When the aircraft nose yaws to the left, the yaw damper will apply corrective rudder to Report

the right

the left

the left with some aileron assistance

12) A yaw damper will apply rudder proportional to Report

amount of aircraft disturbance

attitude of aircraft

rate of yaw

13) In a turn, wing spoilers may be deployed Report

to act as an airbrake, interacting with the ailerons

in unison with both the up going and down going ailerons

to assist the up going aileron

14) Glideslope deviation signals are Report

DC polarity sensitive

AC phase sensitive

DC positive going only

15) A triplex system loses one channel Report

pilot can continue with autoland

pilot can use auto approach

pilot must make a full manual approach and land

16) A series actuator in a helicopter autopilot system has Report

full authority

50% authority

10% authority

17) Stall warning will be given Report

before stall

after stall

at stall

18) With on-board maintenance (OBM) systems, the purpose of central maintenance function (CMF) is to Report

log relevant maintenance data

transmits to the CMC

provides details of defect action

19) How are spoilers normally operated? Report

Hydraulic actuator

Air pistons

Electrical motors

20) The purpose of a force trim release system in an helicopter is to permit the Report

pilot to move the cyclic stick to obtain desired new attitude without having to maintain the opposing forces of the artificial feel system forces

pilot to move the collective to obtain a power change

appropriate cyclic actuator to be over powered

EASA Questions Module 13 Set 5

Set 1

Set 2

Set 3

Set 4

Set 5

Set 6

Set 7

Set 8

Set 9

Set 10

Set 11

Set 12