Module 11.2a Airframe structures Flashcards

1
Q

What are the 5 stresses acting on an aircraft?

A
  • Tension
  • Shear
  • Torsional
  • Compressive
  • Bending
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2
Q

What are primary structural parts?

A

They have a critical role in aircraft integrity.

i.e. If they fail people die

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3
Q

What are secondary structure parts?

A

All non-primary structural parts

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4
Q

What is the final structure classification?

A

Tertiary

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5
Q

What is hoop stress?

A

Hoop stress is the circumferential stress caused by the pressurisation of the aircraft on the fuselage

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6
Q

The hoop stress will be _____ the value of the longitudinal stress

A

Twice

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7
Q

What is fatigue caused by?

A

Cyclic or alternating loading

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8
Q

What is the failsafe concept?

A

Duplication of certain structural parts so that if one break the other will bare the load carried by the other

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9
Q

If a failure occurs on a failsafe part, is the part still failsafe?

A

No, not anymore

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10
Q

What is the safe life of a component?

A

The safe life is the number of hours or cycles a part is safe for. This means that within this time period the part should not fail

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11
Q

What are the five main structural units?

A
  • Fuselage
  • Wings
  • Stabilisers
  • Flight control surfaces
  • Landing gears
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12
Q

How does the zonal ident system work?

A
  • 1st major zone
  • 2nd sub major zone
  • 3rd zone
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13
Q

How are panels identified?

A

Panels have a 3 digit zonal ident followed by two characters

  • 1st inbd to oubd, forward to aft, top to bottom
  • 2nd Left to right
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14
Q

What are body stations/ fuselage stations?

A

They are sections in the vertical plane that are perpendicular to the centre line

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15
Q

What are buttock lines?

A

Buttock lines are lines in the vertical plane that run parallel to the centre line

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16
Q

What are waterlines?

A

Waterlines are sections that run in the horizontal plane perpendicular to buttock and fuselage stations

17
Q

What are wing stations?

A

Sections in the vertical plane that run from leading edge to trailing and start at a reference buttock line or wing rib 1

18
Q

How are the horizontal and vertical stabilisers given wing station co-ordinates?

A

Equal to wing co-ordinates

19
Q

To prevent loss of air during pressurisation what valves are fitted to aircraft?

A

Bilge-like valves

20
Q

What position are bilge-like valves set too when the aircraft is depressurised?

A

Set too open

21
Q

Where is ventilation required?

A

Ventilation is required in areas where moisture or flammable fumes may build up

22
Q

How is fluid directed to drain valves?

A

Longitudinal and cross drain paths

23
Q

What are the two types of damage from lightning strikes?

A

Direct and indirect

24
Q

Why is bonding necessary?

A

For continuity throughout the aircraft and to ensure the is no difference in potential on the fuselage

25
Why are electrical system onboard grounded to the structure?
So current returns on single wire systems, to stop damage if system is overloaded
26
If bonding is correct what should the resistance measurement not exceed?
0.025 ohms
27
What is major zone 100?
Lower half of fuselage
28
What is major zone 200?
Upper half of fuselage
29
What is major zone 300?
Empennage
30
What is major zone 400?
Powerplants and struts
31
What is major zone 500?
Left wing
32
What is major zone 600?
Right wing
33
What is major zone 700?
Landing gear + gear doors
34
What is major zone 800?
Doors