Pressurisation Flashcards

1
Q

Max pressure differential for a jet transport

A

9 psi

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2
Q

Max cabin alt (normal)

A

8,000ft

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3
Q

At what height does the cabin alt warning system activate

A

10,000ft

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4
Q

Cabin o2 automatically drops at

A

14,000ft

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5
Q

Max cabin alt in an emerg

A

15,000ft

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6
Q

Pax comfort roc and rod of the cabin

A

Roc = 500fpm

Rod = 300fpm

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7
Q

Max roc and rod for the cabin

A

1800fpm

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8
Q

Max negative differential pressure

A

1/2 psi

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9
Q

Pressurised areas of the a/c

A

F/d
Fwd and aft cabins
Fwd and aft cargo holds

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10
Q

Unpressurised areas of the a/c

A
Radome 
Nose u/c bay
Centre section torque box 
Main u/c bay
Tail cone
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11
Q

Discharge/ outflow valves purpose and are controlled by - pressurisation

A

Controls pressurisation to allow for a varying rate of air being discharged to the atmosphere

Controlled by the pressure controller when in automatic or manual by the flight crew

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12
Q

Safety valve - pressurisation

A

Outwards pressure relief valve for when the max diff has been exceeded

Valve will open at 0.25 psi above the max diff

Normally occurs when the pressure controller is unserviceable

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13
Q

Inwards relief valve

A

Fitted to prevent excessive negative differential pressure - open if the pressure outside the a/c exceeds that of inside by 0.5

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14
Q

Dump valve

A

Allows the crew to dump all cabin pressure - operated manually

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15
Q

Pressure controller

A

As the cabin altitude changes, the controller automatically sends a signal to the outflow valves - regulate the release of air - maintain the a/c at the preselected levels

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16
Q

What happens when ditching - pressurisation

A

Slated ditching control will close the outflow valves in the event of l/d on water

17
Q

Min system instrumentation for pressurisation

A

Cabin altimeter - reads cabin pressure

Cabin VSI

Cabin diff pressure - diff between the cabin and atmospheric pressure

18
Q

What are the aural/visual warnings when the cabin alt exceeds 10,000

A

Horn and a red light on the centralised panel - visual and aural CABIN ALT warning
Or
Warning caption on the EICAS or ECAM

19
Q

At what height does the AUTO FAIL light on the pressure controller panel illuminate

A

13,850ft

20
Q

When is the pressurisation system ground tested and checked

A

Initial proof testing
When specified in the manual
After actual or suspected malfunction
After repairs and modifications to the hull

21
Q

Ground testing and system checking of the pressurisation system include testing

A
Pressure controllers and temp control 
Max diff control 
Safety valve check 
Leak rate check 
General functioning
22
Q

Rate/proportional control is maintained during (pressurisation)

A

Climb and descent

Cabin climbs and descends proportionally

23
Q

Why do we put a bit of pressure in while taxing

A

Makes for a smooth transition and stops crap getting in

Set to about 0.1psi - doors can’t open until this has been dumped