1) What protects the aircraft fibreglass panels against lighting strikes Report

Bonding

Conductive paint

Non - Conductive paint

2) What aircraft structural member could take a compression load Report

Strut

Cable

Beam

3) What type fuselage uses stringers in construction Report

Truss type

Monocoque

Semi-monocoque

4) Wing stations are measured Report

outboard from the wing root.

outboard from the fuselage centreline.

inboard from the wing tip

5) Tie rods are designed to withstand what type of load Report

Tensile

Bending

Compression

6) What colour code is used to identify primary structure Report

Red

Green

Yellow

7) Which of the following is the primary structure Report

Frame.

Skin.

Stringer.

8) A work card numbered 500376; what does it indicate Report

A Job 376, located on the left wing (Zone 500).

A job 376, located on the right wing (Zone 500)

A job 500, located on the right wing (Zone 376)

9) Fuselage station numbers are measured in Report

Inches

Feet

Meters

10) Which parts of the aircraft are classified as secondary structure Report

These parts of the airframe are highly stressed but if damaged will not cause failure of the aircraft.

These parts of the airframe are highly stressed and if damaged may cause failure of the aircraft and loss of life.

These are lightly stressed parts such as fairings, wheel shields and minor component brackets etc.

11) An aircraft structure with built‑in redundancy is called Report

failsafe.

double safe.

Auxilary

12) 'Stress' is the Report

Property of a material to resist fracture.

Load per unit area acting on a material.

Deformation of a material caused by applied load.

13) What type of component or structure is required to be replaced at a specified period, based on number of cycles, flying hours, or calender, regardless of its physical condition Report

Fail safe

Condition monitored

Safe Life

14) If you are unable to identify a structure classification as either Primary or Secondary, what action should you adopt Report

Upgrade it to primary.

Grade it as secondary.

Paint it red and stamp it as tertiary.

15) Safe-life is Report

The sharing of loads between adjacent members.

The minimum number of flying hours that should elapse before a major structural failure occurs.

The maximum number of flying hours that should elapse before a major structural failure occurs.

16) When a beam is under bending load, it is subjected to Report

Torsion and Tension stress

Tension and Compression stress

Tension and Shear stress

17) The Airworthiness Notice that refers to structural survey is Report

Notice 65.

Notice 79.

Notice 89.

18) Who is authorised to call for a structural survey inspection Report

Operator.

Manufacturer.

Maintenance engineer.

19) Wing stations are measured from Report

Water Line (WL).

Zone Line (ZL).

Buttock Line (BL).

20) Zone 323 is located Report

between rear spar and trailing edge.

between front and rear spar.

at the tip of vertical stabiliser.

EASA Questions Module%2011 Set%202:%20airframe%20structures

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