Air Management System Flashcards

(29 cards)

1
Q

What are the two components of the AMS?

A

The pneumatic system
Environmental control system (ECS)

Cabin pressure control system is included but has a separate controller

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

The AMS controller provides primary control for what systems? (5)

A
Bleed control
Environmental control
Hot air leak detection
Crew O2 Monitoring
Wing and engine ice protection
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

(T/F) The two channels are independent of one another and should one fail the entire channel is lost

A

False. Both channels can fully cover the other, should one fail

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

What are all the sources for pneumatic air?

A

Engine bleed air
APU bleed air
External pneumatic source

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

The pneumatic air is used for what 4 jobs?

A

Engine starting
Anti Ice system
Environmental control system
Water pressurization system

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

Low pressure bleed air comes from what stage of the engine?

A

Stage 6

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

High pressure bleed air comes from what stage of the engine?

A

Stage 10

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

What is the purpose of the low stage bleed check valve

A

Prevents reverse flow of high pressure bleed air back into the engine at the low pressure supply port

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

The engine bleed valve regulates pressure at __ power settings

A

High

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

What does a white bar on either engine bleed buttons, or the APU bleed button mean?

A

The check valves are closed and the system is not supplying pneumatic air

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

If more than one bleed air source is available the AMS logic uses what priority?

A

Onside engine
Opposite engine
APU, if available

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

(T/F) The APU bleed air can be used for the anti ice system in flight

A

False

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

The ECS packs 1 and 2 shall be closed if any of what conditions exist? (7)

A
  • A bled air source is not available for the pack
  • The respective pack button is off
  • Any engine is starting and weight-on-wheels is true
  • The respective engine is starting, wight-on-wheels is false and the opposite engine is not starting
  • Any engine is starting AND APU is the bleed source
  • Respective bleed system duct leak
  • Respective packs BIT shutdown failures are present (PACK 1(2) FAIL EICAS message displayed)
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

The two ECS packs are installed where?

A

In the two wing to fuselage fairing

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

The air reaching the cockpit and cabin is approximately __% fresh air and __% recirculated air

A

52% fresh

48% Recirculated air

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

The recirculation fans will automatically turn off if ___ or ___

A

The pressurization dump button is pressed

or, smoke is detected in the recirculation bay

17
Q

The gasper shutoff valve will automatically open whenever the gasper air supply exceeds __C (__F)

18
Q

(T/F) Live animals can be placed into both cargo bays

A

False. They must be in the FWD cargo bay because it is the only one with a recirculation fan

19
Q

The pack 1 ram air valve will automatically open when: (3)

A

The airplane is in flight
Pack 1 and 2 are commanded OFF or failed
The airplanes flight altitude is less than 25,000 feet

20
Q

(T/F) Passenger cabin temperature must be controlled by the pilots

A

False. The pilots can select manual FA control on the ECS panel

21
Q

The Cabin Pressure Control System (CPCS) 5 main components are:

A
Cabin Pressure Controller (CTR)
Cabin outflow valve
Negative pressure relief valve
Positive pressure relief valve
Static port
22
Q

The positive pressure relief valve opens independently whenever differential pressure exceeds ___ PSID

23
Q

The negative pressure relief valve limits the negative differential pressure to ___ PSID

24
Q

A CABIN ALTITUDE HI message illuminates whenever the cabin altitude is above ____ ft

25
The dump button will depressurize the cabin at a rate of ____ FPM up to ____ ft
2000 FPM up to 12,400 ft
26
(T/F) If pressurization dump button is pressed a second time, the system will return to normal operation
True
27
(T/F) In manual mode there is still automatic cabin depressurization on the ground (after landing)
False
28
PRESN AUTO FAULT means what?
One of the two controllers on the cabin pressure controller (CTR) has failed, but the other is still fuctioning
29
PRESN AUTO FAIL
Both controllers on the cabin pressure controller (CTR) have failed