Systems AIR Flashcards

Air Conditioning, Bleed Air & Pressurisation

1
Q

How many IASC Integrated Air System Controllers

A

2
FCOM 1 02-02-12

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

Each IASC is composed of

A

3 Channels
A B and Safety Channel C
FCOM 1 02-02-12

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

IASC 1 controls

A

Left Engine Bleed Air Valve
L ENG High Pressure Valve
L ENG Fan Air Valve
APU Bleed Valve
Cross Bleed Valve
Left Wing Anti-Ice Valve
FCOM 1 02-02-12

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

IASC 2 controls

A

Right Engine Bleed Air Valve
R ENG Hi Pressure Valve
R ENG Fan Air Valve
R Wing Anti-Ice Valve
FCOM 1 02-02-12

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

List uses of Bleed Air

A

AIR CON & Pressurisation
Cowl and Wing Anti-Ice
Main Eng Start
Fuel Inerting
FCOM 1 02-02-1

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

Integrated Air Management System IAMS includes which systems

A

Bleed Air System
Bleed Air Leak and Overheat Detection System BALODS
Air Con system
Avionics cooling and Heat extraction system
Pressurisation system
FCOM 1 02-01-1

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

In what situation on the ground can the AIR synoptic page indicate L and R bleed pressure varying between 9-16 PSI instead of 0 PSI

A

Without Bleed Air connected and while on BATT Power only.
FCOM 1 02-02-3

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

When will the IASC use Engine Bleed Air priority over APU bleed Air, if both are available.

A

When Wing Anti-Ice active or On, Aircraft Inflight and Clean and above 16,500 ft. Otherwise APU Bleed is used.
FCOM 1 02-02-15

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

What does CYAN EICAS message LEAK DET FAULT indicate

A

Single Loop Leak Detection Failure
FCOM 1 02-02-22

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

How many AIR CON flow modes are there

A
  1. Automatic and HIGH Flow
    AUTO based on number of Pax entered in FMS
    HIGH Flow automatically selected when necessary (APU operation on ground, high or low mix duct temp) can be manually selected with PACK FLOW switch on AIR panel
    FCOM 1 02-03-7
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

What is the function of the Trim Air System

A

Supplies additional hot bleed air through 4 Trim Air Valves. One for each air-conditioned zone
FCOM 1 02-03-11

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

Which temperature is controlled by the IASC when MAN TEMP is selected

A

Duct temperature instead of zone
FCOM 1 02-03-18

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

Approximately what percentage of Cabin Air is recirculated

A

35-40%
FCOM 1 02-03-22

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

What does Cyan message EQUIP BAY COOL FAULT indicate

A

Loss of redundant or non critical function for the Air Con system
FCOM 1 02-03-48

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

Explain pressurisation system Return to Base Mode

A

Begins if A/C descends at a rate >500ft/min for more than 10secs within 10 minutes of TO or before reaching 5000ft above Field Elevation. IASC depressurises to Field Elevation
FCOM 02-04-7

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

What altitude does the AC descend to if the guarded EMER DEPRESS switch is pushed

A

15,000 ft or the AC altitude, whichever is lower
FCOM 02-04-10

17
Q

Which valves are closed by the Guarded DITCHING switch

A

Avionics Exhaust Valve AEV
Flow Control Valve FCV
Trim Air Pressure Regulating Valve TAPRV
Bulkhead Check Valve
Outflow Valve OFV which is closed last
FCOM 1 02-04-11

18
Q

Which Valve needs to be manually closed when the DITCHING switch is pushed

A

RAM AIR valve
FCOM 1 02-04-11

19
Q

Bleed Air Leak and Overheat Detection System BALODS detects leaks in

A

Bleed Air manifold L/R
Wing Anti-Ice manifold L/R
Air Con packs and manifolds
Trim Air manifolds
APU bleed air manifold

Both Dual Loops must detect leak to trigger alert
FCOM 1 02-02-15

20
Q

Main components of Pressurisation System are

A

Outflow Valve OFV (mid aircraft behind Fwd Cargo)
2x Safety Over/Under Pressure Relief Valves (Rear Bulkhead)
Negative Pressure Relief Valve NPRV (Rear Bulkhead)
Pressure Equalisation Valves (Each Cargo CMPT has a Large and Small PEV)
FCOM 1 02-04-1

21
Q

MANUAL Pressurisation activated when AUTO PRESS switch is pushed. The rates are

A

12 o’clock 0 ft/min
9 o’clock and 3 o’clock -1,000 and +1,000 ft/min
9 o’clock and Dn and 3 o’clock and UP between -/+1,000 to -/+2,500 ft/min
FCOM 1 02-04-8

22
Q

The FWD CARGO switch on the AIR panel has 4 settings

A

OFF Not vented not heated
LO HEAT 15-20 deg
HI HEAT 20-25 deg
VENT Ventilation only 4-25 deg
FCOM 1 02-03-19/35

23
Q

Flight Crew can select what range of temperatures in Manual mode

A

COCKPIT, FWD CABIN & AFT CABIN
Cold 18 deg
Hot 30 deg
Centre position 24 deg
FCOM 1 02-03-33

24
Q

The engine bleed air system has which components

A

Intermediate Pressure Check Valve IPCV
High Pressure Valve HPV
Pressure Regulating Shut Off Valve PRSOV
Fan Air Valve FAV
Bleed Temperature Sensor BTS
Precooler
FCOM 1 02-02-6

25
What are the primary sources of pneumatic power for the aircraft
4th or 8th stage engine compressor FCOM 1 02-02-6
26
The Intermediate Pressure Check Valve prevents
Backflow to the engine when the HPV is open FCOM 1 02-02-7
27
The High Pressure Valve HPV lets 8th stage bleed air flow when
Thrust settings are low or when demand is too high for the 4th stage FCOM 1 02-02-7
28
The Pressure Regulating Shut Off Valve PRSOV maintains a constant pressure to the bleed manifold of approximately
45 psi FCOM 1 02-02-7
29
The Fan Air Valve FAV directs cooling fan section air to the
Bleed Air Precooler FCOM 1 02-02-7
30
The Bleed Temperature Sensor downstream of the precooler sends temperature information to the IASC to adjust the
Fan Air Valve FAV FCOM 1 02-02-8