13.11.3 Pressurisation Flashcards

1
Q

What is anoxia?

A

Complete absence of oxygen in the blood

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

What would be the common symptoms of anoxia at 5,000 to 8,000 feet?

A

Some loss of night vision

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

What are the most common problems caused by barotrauma (as the aircraft climbs or descends, gases trapped within bodies expand or contract)?

A

Aerotitus (air trapped in the middle ear)

Air trapped in paranasal sinuses by a blocked eustachian tube or sinuses

Pain experienced in the gastrointestinal tract or even the teeth (barodontalgia)

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

In pressurised passenger aircraft, what is the acceptable rate of change of altitude in the cabin?

A

300 feet per minute

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

What is the cabin altitude limit for use in pressurised aircraft and why?

A

8,000 feet

Vast majority of people suffer no discomfort due to anoxia at altitudes up to this height

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

How is control of cabin pressure and rate of change of cabin pressure obtained?

A

Regulating the rate at which cabin air escapes from the cabin to atmosphere

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

What is a dump valve?

A

Manually operated device by which the pressure differential can be rapidly reduced to zero

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

What is positive differential pressure?

A

Condition in an aircraft where the pressure in the cabin is greater than local atmospheric pressure

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

What is an alternative name for an outflow valve?

A

Discharge valve

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

What are the typical maximum differential pressures for:

Jet transport aircraft

Turbo prop transport aircraft

Turbo–charged twin engine aircraft

A

Jet transport aircraft – 8–9.5 psi

Turbo prop transport aircraft – 5.5 psi

Turbo–charged twin engine aircraft – 4.5 psi

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

What is negative differential pressure?

A

Cabin pressure is less than the local atmospheric pressure

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

What is the normal maximum value of negative differential pressure of aircraft?

A

0.5 psi

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

What is pressure altitude?

A

Altitude in the Standard Atmosphere corresponding to a particular pressure

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

What is density altitude?

A

Altitude in the Standard Atmosphere corresponding to a particular value of air density

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

How is the negative differential pressure controlled?

A

Inward relief valves

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

How does the depressurising solenoid operate on the ground?

A

Solenoids are energised by weight on wheels switch

Bleed air through an ejector causes suction through depressurising solenoid from discharge valves, thus ensuring the discharge valves remain open

17
Q

What functions does a discharge valve fulfil?

A

Discharge valve
Safety valve
Inward relief valve
Ditching

18
Q

Explain the operation of the safety valve function of the pressurisation system?

A

Should cabin pressure become excessive due to failure of the pressure control equipment

Increased differential pressure across the pressure relief valve diaphragm opens the internal control valve

Air in the control chamber is allowed to bleed to atmosphere

Upper diaphragm moves as a result of this reduced control chamber pressure

Valve opens wide to allow the excess cabin pressure to be relieved to atmosphere

19
Q

What is the aircraft ideal rate of climb relative to cabin pressurisation?

A

Adjusted to arrive at the selected flight altitude slightly after the aircraft cabin reaches the height selected on the pressure controller

20
Q

What is isobaric control?

A

Cabin altitude reaches controller setting

Conditions are stabilised in the cabin with regard to pressure

Discharge valves will open and close to maintain the pressure to the equivalent controller setting

21
Q

Prior to descent, what is the cabin altitude selector set to and why?

A

Landing airfield height

Cabin pressure and atmospheric pressure will be equal on landing

22
Q

What three parameters is the pressure controller looking at and which is the overriding parameter?

A

Rate of change

Cabin altitude

Maximum differential pressure (most important parameter)

23
Q

What three instruments are normally used to monitor the cabin pressurisation system?

A

Cabin altimeter

Cabin altitude rate of change indicator

Differential pressure gauge

24
Q

What is the purpose of the cabin altitude warning light fitted to the instrument panel?

A

Indicate when cabin altitude reaches and exceeds 10,000 feet

25
Q

While in cruise, what change in aircraft height will cause no change to the corresponding cabin altitude?

A

Climb or descent of less than 500 feet

26
Q

Where pressurisation systems are tested, what must all persons on board be?

A

Medically fit

Free from colds and sinus troubles

27
Q

What pressure is the proof pressure test carried out at?

A

1.33 times the maximum operating differential pressure

28
Q

When might a proof test be required following major repairs or alterations to structural design?

A

Only if the CAA and manufacturer require it

29
Q

When ground testing a pressure cabin, what will the cabin rate of change indicator show as the differential pressure increases?

A

A rate of descent

30
Q

Why is it ideal when the aircraft rate of climb is adjusted to arrive at the selected flight altitude slightly after the aircraft cabin reaches its predetermined height?

A

If aircraft climbs too steeply, it will reach the maximum differential altitude before the cabin has a chance to reach its set altitude

In effect the cabin’s rate of climb will then have to match the aircraft’s rate of climb to keep within the safe envelope

31
Q

Why does the cabin altitude need to rise slower than the aircraft altitude?

A

Effect of rapid altitude changes on the human body is to cause physical pain and discomfort in the inner ear

Due to the pressure difference across the ear drum

32
Q

Which valve prevents differential pressures exceeding a safe maximum?

A

Outflow valve (in conjunction with the cabin pressure controller)

Cabin safety valve

33
Q

With an electronic pressurisation schedule, how much deviation in aircraft altitude would result in cabin altitude variation? How?

A

500 ft

Cabin altitude controller will compare the cabin altitude to that of the selected landing altitude