11.3.2 - Wings - 3q

Question 1

What is meant by ‘Cantilever’?

Answer 1

Question 2

Spars are made from what type of material?

Answer 2

Question 3

Why are Spars tapered?

Answer 3

Question 4

A Wing Spar is subject to what forces? (2)

Answer 4

Question 5

The Spar Web in a wing spar is subject to what loads?

Answer 5

Question 6

The Upper and Lower Cap of a wing spar takes what loads?

Answer 6

Question 7

Monospar used where?

Answer 7

Question 8

When talking about Fail Safe in terms of a wing spar, what is meant?

Answer 8

Question 9

Why are wings fitted in planks?

Answer 9

Question 10

What is meant by Aerodynamic balance?

Answer 10

Question 11

Internal balance panels use what?

Answer 11

Question 12

Flight control attachments are what type of design?

Answer 12

Question 13

A Krueger flap is what type of device?

Answer 13

Question 14

L/E slat is attached to what?

Answer 14

Question 15

What is the point of the Mid Spar?

Answer 15

Question 16

The final coat of sealant in an integral fuel tank is a what?
And name the 3 layers?

Answer 16

Question 17

The L/G front trunnion is attached to what?

Answer 17

Question 18

Upper Wing Skin is made of what material for what reason?

Answer 18

Question 19

Answer 19

Both A and B are correct

Question 20

Answer 20

Incorrect

Question 21

Answer 21

Ribs

Question 22

Answer 22

Leading edge of the wing

Question 23

Answer 23

Reduce drag

Question 24

Answer 24

a cantilever wing

Question 25

Answer 25

an area between two spar caps

Question 26

Answer 26

slat track

Question 27

Answer 27

shear forces are greatest at the root

Question 28

Answer 28

Ribs

Question 29

Answer 29

usual airliner wing

Question 30

Answer 30

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