1) Vortex generators Report

Move the transition point forward (leading edge)

Move the transition point rearward (trailing edge)

Advance the onset of flow separation.

2) Leading edge flaps (Slats) Report

decreases the stalling angle of the wing.

increases the stalling angle of the wing.

does not affect the stalling angle.

3) Krueger flaps are attached to Report

the leading edge.

the trailing edge.

either the leading or training edge.

4) An aircraft with sweepback wing will Report

increase lateral stability.

decrease lateral stability.

not affect lateral stability.

5) A plain flap Report

is attached to the leading edge of the wing.

forms part of lower trailing edge.

does not increase the wing area on deployment.

6) A split flap, when deployed Report

increases drag with little lift coefficient increase, from intermediate to fully down.

is used only on high speed aircraft.

increases lift without a corresponding increase in drag.

7) ATA ?Zone 320? refers to Report

central fuselage.

vertical stabiliser.

horizontal stabiliser.

8) When a bonding test is carried out, the desired maximum resistance between a component and earth should be Report

0.005 ohms.

1/50 ohms.

50 milliohms.

9) What prevents the nose cone of an aircraft from a lighting strike Report

Earthing Strap.

Bonding Strip.

10) Tension is the stress of Report

crush or compression.

elongating or stretch.

twisting.

11) A Fuselage Station is a Report

lateral point on aircraft wing.

lateral point on aircraft fuse.

longitudinal point on the aircraft fuselage.

12) Longitudinal measurements on the fuselage is called Report

Fuselage stations

Wing Stations

Buttline

13) Composite materials are bonded by Report

aluminium wire.

special paint.

copper wire.

14) ATA Zone 100 refers to Report

upper fuselage.

lower fuselage.

Wing.

15) The bonding lead to a remote aircraft component must be Report

0.5 in wide.

22 AWG.

0.25 in wide and 22 AWG.

16) A force applied on an I-Beam causes what type of stress on the beam Report

Tension.

Bending.

Shear

17) A radome is protected from static electricity build-up by Report

bonding strips.

special conductive grease.

conductive paint.

18) Precise points on an aircraft can be located by a means of Report

frame stations, vertical lines and lateral lines.

longitudinal, vertical and lateral lines.

frame stations, water lines and buttock lines.

19) Which of the following is an example of a fail safe structure Report

Spar.

Longeron.

Stringer.

20) Damage tolerant design Report

Is applied only to secondary structure.

Allows for certain damage to the structure to go un-repaired between scheduled maintenance.

Allows for damage to structure by distributing loads to other structure.

EASA Questions Module 11 Set 1: Theory Of Flight

Set 1: Theory of flight

Set 2: Airframe Structures

Set 3: Aeroplanes-Fuselage

Set 4: Cabin Pressurisation

Set 5: Instruments

Set 6: Avionic system

Set 7: Avionic system

Set 8: Navigation

Set 9: Electrical Power

Set 10: Electrical System

Set 11: Battery

Set 12: Equip & Furnishing

Set 13: Fire Protection

Set 14: Fuel Systems

Set 15: Hydraulic Power

Set 16: Ice & Rain

Set 17: Flight Controls

Set 18: Flight Controls_1

Set 19: Landing Gear

Set 20: Lights

Set 21: Oxygen

Set 22: Pneumatic

Set 23: Water & Waste