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
Q

Why are electrical system onboard grounded to the structure?

A

So current returns on single wire systems, to stop damage if system is overloaded

26
Q

If bonding is correct what should the resistance measurement not exceed?

A

0.025 ohms

27
Q

What is major zone 100?

A

Lower half of fuselage

28
Q

What is major zone 200?

A

Upper half of fuselage

29
Q

What is major zone 300?

A

Empennage

30
Q

What is major zone 400?

A

Powerplants and struts

31
Q

What is major zone 500?

A

Left wing

32
Q

What is major zone 600?

A

Right wing

33
Q

What is major zone 700?

A

Landing gear + gear doors

34
Q

What is major zone 800?

A

Doors