Environmental, Pressurization, & Pneumatics Flashcards

1
Q

What is the maximum altitude for flight and maintain the Pressurization System within normal operating limits

A

35,000, this will have the cabin differential at 6.6 PSI and maintaining a cabin pressure of 10,380 (comply with AR 95-1)

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2
Q

In a LOAD SHED condition, is it possible to maintain flight at 35,000 feet, when considering pressurization

A

Yes, The left bleed air valve is fully functional and one engine should be capable of maintaining pressurization.

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3
Q

What is the maximum cabin differential pressure for the MC-12

A

6.6 PSI

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4
Q

What is the minimum N1 to operate the air conditioning

A

62 % N1 on the right engine, less than that the Air Cond N1 Low advisory light will illuminate and the air conditioner will be inoperative.

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5
Q

After selecting the bleed air valve to pneumatic and environmental off after illumination of a single [L or R BLEED FAIL] red master warning annunciator, the annunciator will?

A

Remain illuminated

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6
Q

What is regulated pneumatic air pressure used for?

A

surface de-ice,
vacuum,
hydraulic head pressure,
door seal,
bleed air warning,
flight hour meter.

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7
Q

Regulated pneumatic air is ____ psi with overpressure relief at ____ psi?

A

18, 21.

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8
Q

P3 air is _____ degrees off the 4th stage compressor and cools to ____ degrees above ambient before entering the 18 psi pressure regulator.

A

700 degrees

70 degrees

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9
Q

What device controls the flow of bleed air and ambient air.

A

The Flow Control Unit (FCU)

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10
Q

The flow control unit regulates _____________ into the pressure vessel.

a. Inflow air.
b. Outflow air.
c. Ram air.
d. Vacuum air.

A

a. Inflow air.

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11
Q

What are the five primary components in the Pressurization System.

A
Pressurization Controller
System Switches
Indicators
Outflow Valve
Safety Valve
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12
Q

The pressure controller uses __________ to open the outflow valve for scheduled pressurization.

a. Pressurization air.
b. Waveguide air.
c. Vacuum
d. Electricity.

A

c. Vacuum

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13
Q

What are two major functions of the outflow valve?

A

Two major functions –

Modulates pressurization
Negative Pressure Relief
Maximum Pressure Relief is capped

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14
Q

From the list below, which is NOT a function of the outflow valve?

Positive Relief.
Negative Relief.
Dump Operations.
Pressure Modulation.

A

Dump Operations.

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15
Q

During the pressurization test what valve closes when we place the switch to test?

a. Safety valve.
b. Outflow valve.
c. Motive flow valve.
d. One way check valve.

A

a. Safety valve.

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16
Q

What prevents “pressure bumps” from occurring after takeoff?

a. The Left and Right Air-to-Air Heat Exchangers.
b. The Normally Closed Solenoid and Safety valve.
c. The Normally Open Solenoid and Outflow valve.
d. The left landing gear safety switch and 6 – 8 second delay that opens up the right FCU ambient air valve.

A

d. The left landing gear safety switch and 6 – 8 second delay that opens up the right FCU ambient air valve.

17
Q

Which valve modulates to maintain scheduled pressurization in flight?

a. Outflow valve.
b. Safety valve.
c. Motive flow valve.
d. One way check valve.

A

a. Outflow valve.

18
Q

What cabin altitude does the Cabin Altitude white annunciator come on?

A

When the cabin altitude exceeds 10,000 feet MSL.

19
Q

What cabin altitude does the Can ALT HIGH RED Warning come on?

A

When the cabin altitude exceeds 12,000 feet MSL.

20
Q

What cabin altitude drops the passenger oxygen masks?

A

Cabin Altitude greater than 12,500 ft the passenger oxygen masks will drop down.

21
Q

Explain the Cabin Diff HI Warning.

A

Cabin Pressure is greater than 6.9 PSI.

22
Q

Analyze the following scenario and select the best answer:

You are flying along and you experience a complete electrical failure. What will happen with regards to pressurization?

The aircraft will attempt to over pressurize.

The aircraft will immediately dump the cabin.

The aircraft will maintain scheduled pressurization.

The aircraft will depressurize at the cabin leak rate.

A

The aircraft will depressurize at the cabin leak rate.

23
Q

What are the Unregulated 120 PSI Users?

A
Brake Deice (if installed)
18 psi Regulator
24
Q

What are the Regulated 18 psi users?

A
Regulated 18 psi users
Flight hour meter
Bleed Air Warning
Hydraulic fill can
Ejector (creates vacuum)
Pressurization control
Deice boots
25
Q

Where is vacuum obtained?

A

Vacuum is obtained from pneumatic air passing through the vacuum ejector.

26
Q

How many users of vacuum are there? What are they?

A

Vacuum is provided for the deice boots and the pressurization control system.

27
Q

Question: After selecting the bleed air valve to pneumatic and environmental off after illumination of a single [L or R BLEED FAIL] red master warning annunciator, the annunciator will?

A

Answer: Remain illuminated.

28
Q

Question: Regulated pneumatic air is ____ psi with overpressure relief at ____ psi?

A

Answer: 18, 21.

29
Q

Question: What is regulated pneumatic air pressure used for?

A

Answer: Vacuum, hydraulic head pressure, door seal, bleed air warning, flight hour meter.

30
Q

Question: Is Brake Deice available during single engine operations?

A

Answer: No.

This is because the check valves do not allow unregulated P3 air to the opposite brake manifold.

31
Q

What is a more efficient means of cooling the aircraft while on the ground?

A

Leave the Bleed Air Valves switches in the ENVIRO OFF position.

32
Q

True or False –

The Air-to-Air Heat Exchangers have a bypass capability?

A

True

33
Q

True or False –

The temperature of the air coming into the cabin when in the MAN mode is controlled by the floor sensors.

A

False

34
Q

What is the CAUTION associated with using the INCR / DECR in the MAN mode?

A

INCR / DECR switch activation longer than 2-3 second intervals or longer than 60 seconds can result in duct overheating and the illumination of the amber DUCT OVERTEMP annunciator.