11.2 B Airframe Structures Flashcards

1
Q

Define longeron

A

Main longitudinal member of fuselage or nacelle

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2
Q

What’s the name given for a member that takes a tensile load?

A

Tie road
(Tension rod)

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3
Q

What load does a strut take?

A

Compression load

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4
Q

In a semi-monocoque stressed skin, what are the loads shared between?

A

Skin and framework

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5
Q

What is the purpose of the aircraft frame?

A

Gives cross- sectional shape, often circular

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6
Q

Maintains the contour of the covering, can be a stress bearing component, what is it?

A

Rib

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7
Q

Describe a spar

A

The main spa wise member of an aerofoil

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8
Q

What member assist sheet material in carrying loads along their length?

A

Stringer

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9
Q

What is a bulkhead?

A

A partition within the structure

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10
Q

What is a pressure bulkhead?

A

Forms the boundary of a pressurised structure

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11
Q

How do you know where certain components like frames and ribs are positioned?

A

Station numbers

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12
Q

Explain safe life

A

The period in which a component is extremely unlikely to fail

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13
Q

What is the purpose of using a crack stopper?

A

Placed at right angles to the crack, which reduces the rate of further cracking

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14
Q

What is the difference between aerodynamic and static loading?

A

Aerodynamic = when in flight
Static = when stationary

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15
Q

What are the two types of fuselage construction?

A

. Monocoque
. Truss

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16
Q

How does the truss type work?

A

Made of members like beams, struts etc then covered in fabric

17
Q

What are the two sections of a monocoque classification?

A

. True monocoque
. Semi - monocoque

18
Q

What are the main memebersin a true monocoque construction?

A

. Formers, frame, bulkheads and skin

19
Q

What takes the primary stress in a true monocoque construction?

20
Q

How is a semi- monocoque differ from a true- monocoque construction?

A

The skin is reinforced by longitudinal members, therefore both take the loads

21
Q

What is the main advantage of a semi- monocoque structure?

A

Can withstand considerable damage and still be strong

22
Q

What construction are floor boards?

A

Honeycomb composite construction

23
Q

Floorboards have a foam tape on the underside where they contacts structure, what about in wet areas?

A

The edges are sealed up

24
Q

How are the two wings attached to each others?

A

By the wing box

25
What is the wing box designed to do?
Provides support and rigidity to the wings
26
How is the horizontal stabiliser attached to the fuselage
Box section
27
How is the vertical stabiliser attached to the rear stabiliser?
By large machined fittings
28
The engine pylon is made of a frame and skin but how is it formed to make nacelle and strut?
Riveted and bonded together
29
What is the purpose of nacelles?
They are streamlined enclosures used to house engine and it’s components
30
Due to weight what is the preferred rivet type to join metal parts together?
Solid shank rivets
31
When would you use a blind rivet?
When access to joint is only available from one side
32
What marking do close tolerance bolt have on its head?
A raised or recessed triangle
33
What would you do if a bolt had no head markings?
Do NOT Use as probably a commercial grade bolt
34
What is the most effective assembly method?
Adhesive bonding (Foam cores can also be used)
35
What are the three types of surface protection?
1. Pretreatment 2. Paint coatings 3. Special coating
36
What 2 sections can paint coatings be subdivided into?
1. Primers 2. Top coat
37
For special coatings what is type 1 and type 2?
Type 1- water repellent (silicone free) Type 2- heavy duty corrosion preventative
38
What are the two conditions for water used to clean an aircraft?
. Water between 7 and 8 PH . Chloride level less than 100ppm
39
For an aircraft symmetry check what equipment would you use for small aircraft vs large aircraft?
Small aircraft = steel tale Large aircraft = check the floor