ATA 36 Pneumatic Bleed Systems Flashcards

1
Q

To which systems do the pneumatic bleed air deliver?

A
  • ECS
  • Cabin pressurisation system
  • The leading edge de-icing system
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2
Q

When does the HP bleed air valve close?

A

At 76 psi

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3
Q

At which temperature does the pressure regulating/shutoff valve and the HP valve close?

A

If the temperature exceeds 288°C

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4
Q

At which pressure does the pressure regulating/shutoff valve and the HP valve close?

A

43,5 psi

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5
Q

What is the minimum line pressure to open the X-valve?

A

10 psi

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6
Q

Where is the control switch panel 13VU located?

A

In the flight compartment overhead panel

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7
Q

How is bleed air leak detected in the wings?

A

By a dual loop sensing element (fire wire) on each side

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8
Q

How is the fire wire supplied with power?

A

From the 28 VDC LH or RH Main Bus

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9
Q

How can you test the sensing element (fire wire)?

A

By using the BLD LEAK switch on TEST 1 panel

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10
Q

Where is the bleed air detector control unit located?

A

Under the cabin floor

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11
Q

How many Volts does the fire wire use?

A

9V

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12
Q

What is the fire wire made of?

A

A stainless steel capillary with a coaxial nickel centre wire.the space between the centre wire and the inside of the capillary is filled with a temperature sensitive material.

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13
Q

How is the manual temp mode operated?

A

By adjusting the dual temp control valve mechanically

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14
Q

Through which valve is automatic pressurisation adjusted?

A

An electro pneumatic outflow valve located in the rear pressure bulkhead

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15
Q

How can the pilots control pressurisation manually?

A

They can switch to MAN-mode on pressurisation control panel to use the pneumatic outflow (safety) valve. PRESS DUMP in case of aircraft overpressurisation

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16
Q

Can you test the compartment pressure control?

A

Yes, a self test is performed whenever electrical power is applied and the A/C is on ground.

17
Q

Where is pressurisation fault indicated?

A

On the front of the pressure control unit (on the centre pedestal)