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B777 Air Conditioning

Total questions: 10

Worksheet time: 11mins

Name
Class
Date
1.

What does ATA 21 refer to ?

a)

Avionics Systems

b)

Airframe Structure

c)

Air Conditioning and Pressurization

d)

Landing Gear

2.

Which component is responsible for cooling the bleed air in the air conditioning system ?

a)

Heat Exchanger

b)

Air Cycle Machine (ACM)

c)

Compressor

d)

Bleed Air Valve

3.

Which one of the following is not the source of bleed air for the air conditioning system?

a)

APU (Auxiliary Power Unit)

b)

Engine

c)

Ram Air Turbine (RAT)

d)

Ground Power Unit (GPU electrical)

4.

What role does the pressurization system play ?

a)

Cooling the cabin air

b)

Regulating cabin pressure

c)

Controlling aircraft altitude

d)

Providing fresh air to the cabin

5.

In the Air Conditioning and Pressurization system, what does the term "bleed air" refer to?

a)

Air used for pressurizing the cabin

b)

Air taken from the cabin for cooling

c)

High-pressure air from the engines or apu

d)

Air released during emergency descent

6.

What is the purpose of the air cycle machine (ACM) in the Air Conditioning system of the Boeing 777-200?

a)

Generates electrical power

b)

Cools the cabin air

c)

Pressurizes the cabin

d)

Controls aircraft altitude

7.

Which part of the aircraft is responsible for releasing excess cabin pressure in emergency situations?

a)

out flow valve

b)

cabin temp controller

c)

Emergency Oxygen Masks

d)

Bleed Air Valve

8.

What role does the Recirculation Fan play in the air conditioning system ?

a)

Filters bleed air

b)

Distributes used and filtered air to the cabin

c)

Regulates cabin pressure

d)

Controls engine bleed air

9.

What safety precautions should be observed when accessing the air conditioning compartment for maintenance purposes?

a)

Use of personal protective equipment

b)

Manual pressurization of the compartment

c)

Activation of emergency oxygen masks

d)

Disconnecting the aircraft's power supply

10.

In the event of a trim air valve malfunction, how might it impact the pressurization system?

a)

Loss of bleed air

b)

Inability to control cabin temperature

c)

Limited impact on pressurization

d)

Rapid loss of cabin pressure