Pressurization Flashcards

1
Q

“Big” P3 components:

A

Pressurization and Heating

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2
Q

“Little” P3 components:

A

Pneumatic systems

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3
Q

Describe the motion of Uncontrolled Pressurization Airflow (P3):

A

1) In from engines
2) Forward to mixing plenum
3) Rearward into cabin

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4
Q

Describe the motion of Controlled Pressurization Outflow:

A

Exits through Outflow Valve at rear pressure bulkhead and ducts into the unpressurized tailcone, then overboard

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5
Q

Describe the Ambient Air Intakes:

A

Located in fire shield under intake screens.

Used to moderate temperature of P3 air once airborne.

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6
Q

Describe the Ambient Air Sensor:

A

Samples ambient air temp to meter ambient airflow into system

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7
Q

Pressurization Control Unit- Flow Pack

A

Admits hot P3 air for pressurization and heating.

Admits cool ambient air to moderate high P3 temps.

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8
Q

Bleed Air Valves

A

Valve to control pressurization airflow.
Located on the flow pack.
Valve is controlled by cockpit bleed air switch.
-In open, power applied to open environmental valves on pressurization flow packs.
-In middle and down positions, power is removed from these valves, they close, and there is no pressurization or heating from that engine.

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9
Q

Max. differential pressure:

A

200: 6.1 psid
B200: 6.6 psid

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10
Q

Max flight time with cracked windshield:

A

25 hours

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11
Q

Max altitude and pressure differential with cracked windshield:

A

25,000’

4 psid

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12
Q

R/L BL AIR OFF

A

indicates switch position of bleed air valves. NOT in the open position

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13
Q

Safety Valve

A
Hooked to Dump Solenoid (NC)
Capped.
Pressure dump Capability.
Overpressure protection
Negative differential relief
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14
Q

Outflow Valve

A
Vented into cabin pressure
Hooked to Preset Solenoid (NO)
Pressurization outflow control
Overpressure protection
Negative differential relief

Pressure controller provides vacuum to outflow valve to control airflow leaving pressure vessel

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15
Q

Schrader Valve

A

Located in Safety Valve and Outflow Valve. Compares cabin pressure to tailcone. If differential pressure exceeds 6.5 PSID (B200) valve will cycle to relieve excess pressure. I.e. Overpressure protection

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16
Q

Ram Air Inlet Door

A

Located at forward end of pressure vessel.
Held closed by permanent and electromagnet.
Opens to admit outside air once cabin air PSID is reduced to less than 1 by selecting DUMP with the pressurization switch.

17
Q

Ambient Air Valve

A

Located on Pressurization Control Unit (Flow Pack). Controls cooling airflow, by valve movement. Controlled by Ambient Temp Sensor. Valve closes around 0F (electric) or -30F (pneumatic)

18
Q

Cabin Pressurization Switch

A

In (PRESS) position, power is removed from system:

  • Dump valve is closed
  • Preset valve is open
  • Door seal valve is open
  • Ram air door held closed by electromagnet

In (TEST) on ground, the left main gear safety switch is bypassed, causing the above (i.e. pressurization)

19
Q

Pressurization Controller

A

Upper chamber vented to monitor pressure altitude.

Sealed lower chamber contains aneroid (for cabin alt), and adjusts vacuum on outflow valve.

20
Q

Cracked Windshield

A

Descend to 25,000 or less
Reduce cabin pressure to 4.0 psid
DO NOT DUMP
Oxy masks as necessary

21
Q

Pressurization Control CB

A
Pressurization switch (pedestal)
Outflow control solenoid valve (NO)
Safety control solenoid valve (NC)
Cabin door solenoid valve (NO)
Ram Air Door electromagnet
Left Landing Gear Safety switch
22
Q

Bleed Air Control CB

A
Bleed Air Valve switches
Bleed Air Off lights
Environmental flow packs
Pneumatic shutoff valves
Rudder Boost Control