11.2 A Airframe Structures Flashcards

1
Q

What 3 provisions are made in the initial design phase?

A

. Fail safe load transfer
. Damage tolerance
. Fatigue indexing

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

What is the fail safe method?

A

Duplication of certain structural members to ensure that if one member failed, the other would take the load

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

What is the main disadvantage of fail safe?

A

Additional weight required

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

Explain what damage tolerance is

A

The structure is designed so that damage can be detected in normal inspections before failure occurs

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

What is the ultimate static load?

A

A value of load at which the material fractures

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

What are the three aircraft classifications?

A

. Primary structure
. Secondary structure
. Tertiary structure

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

Define primary structure

A

A critical load bearing structure that causes failure of structural integrity

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

Define secondary structure

A

Not a primary load carrying structure
And failure would not reduce the structural integrity, but need to be repaired asap.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

Define tertiary structure

A

Not load carrying and does not form any integral portion

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

What is an aircraft 5 main structural points?

A

. Fuselage
. Wings
. Stabilisers
. Flight control surfaces
. Landing gears

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

What are the 6 stresses that affect an aircraft structure?

A

. Tension
. Compression
. Torsion
. Shear
. Bending
. Hoop stress

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

What causes hoop stress?

A

Due to pressurisation
. Compartment stretches longitudinally
. Circumference expands

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

What measurement do airbus vs boeing use in reference planes?

A

. Boeing = inches
. Airbus = cm/mm

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

What three aircraft axis do the body coordinates run along for AIRBUS.

A

. Vertical
. Lateral
. Longitudinal

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

What three body coordinates do BOEING use?

A

. Body station
. Body buttock lines
. Body waterlines

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

What is the definition of the body station?

A

A vertical plane at a right angle to the body centreline

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
17
Q

What is the definition of the body buttock lines?

A

Vertical planes parallel to the body centreline

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
18
Q

What is the defection of the body waterline?

A

Horizontal planes at a right angle to the body station and buttock lines

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
19
Q

On a Boeing aircraft what are the 3 wing coordinates?

A

. Wing reference plane
. Wing buttock lines
. Wing stations

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
20
Q

Where is the wing reference plane?

A

The same as the dihedral of the wing

21
Q

Where is the wing buttock line?

A

A vertical plane at a right angle to the wing reference plane

22
Q

Where is the wing station?

A

A vertical plane at a right angle to the wing reference plane and the rear spar

23
Q

What am I describing… a horizontal plane, parallel to the body waterline

A

The fin waterline

24
Q

Where a you find the rudder station?

A

At a right angle to the rudder hinge centreline

25
Why do we have major, sub major and zones?
To locate assemblies and sub assemblies, doors and panels
26
How many major zones are there?
8
27
Zone 100?
Lower half of fuselage
28
Zone 200?
Upper half fuselage
29
Zone 300?
Empennage (Aft fuselage and horiz and vertical stab)
30
Zone 400?
Power plants and struts
31
Zone 500?
Left wing
32
Zone 600?
Right wing
33
Zone 700?
Landing gear and landing gear doors
34
Zone 800?
The doors
35
If I had a zone or 631, hay does the individual numbers mean?
600= major zone . right wing 30= sub major zone 1 = zone
36
How does aircraft lower drain valves work?
Spring load When aircraft is depressurised = open When pressurised = closed
37
What is the basic protection on the aircraft from a lightening strike?
All metal structure Protects from EMF
38
What are the steps you must take when your aircraft is struck with lightening?
. General walk around . If damage is found the a detailed inspection
39
What are the two types of lightening damage?
. Direct . Burns, distortion etc . Indirect . Electrical damage
40
What is the size of a normal lightening burn?
1/8 inch
41
What is the size of a high intensity lightening burn?
1/4 inch
42
Do lightening strikes travel from the front to the back or back to the front?
Front to back
43
What is the purpose of bonding an aircraft?
Keep the aircraft and all components at the same electrical conductivity And provides a low resistance return path
44
If binding is done correctly what should be the measurement of resistance?
No higher than 0.025 ohums
45
What is the process of grounding?
Connects single wire electrical systems to the aircraft metallic structure (Direct line for electricity to escape safety)
46
When grounding how many terminals can be on one stud?
No more than 4
47
In vapour areas how many grounds just be installed?
2
48
How must grounds be separated?
By AC, DC and shields