CQ2 Flashcards

1
Q

Up to what alt can the APU provide bleed air

A

20,000ft

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2
Q

High Pressure HP bleed air is used for

A

Wing and engine anti ice

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3
Q

Intermediate air IP bleed air is used for

A

Environmental air

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4
Q

What controls the pneumatics

A

Integrated air system controller IASC

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5
Q

What is IP psi limit

A

50 +-3 psi

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6
Q

What is the HP psi limit

A

36+-3 PSI

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7
Q

What side does APU bleed air flow to

A

Right side only

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8
Q

How many IASC does the system have

A

2

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9
Q

What does the IASC control

A

IASC 1 left HP and IP valves
IASC 2 right Hp and IP valves

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10
Q

What does bleed loop fault mean

A

One loop of a dual loop system has failed

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11
Q

What does bleed loop fail mean

A

One loop of a single loop system or both loops of dual loop system has failed

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12
Q

How is the flow control valves controlled

A

Electrically controlled
Pneumatically operated

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13
Q

What is responsible for the opening and closing of the flow control valves

A

Air source switch

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14
Q

What happens to the flow control valves when the engine start switch if selected

A

They close

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15
Q

What is the max cabin change rate when in manual mode

A

2500fpm

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16
Q

What happens when EMER depress is selected in auto mode

A

Cabin is depressurized at 2500fpm up to 14,000ft +- 100 ft or the aircraft altitude whichever is lower

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17
Q

What happens when EMER depress is selected in manual mode

A

The cabin depressurizes at 3000fpm up 14,500ft +-500ft or the aircraft’s altitude whichever is lower

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18
Q

What does the ditching switch do

A

Depressurizes the cabin
Shuts off AC
Keeps OFV closed in the event of a water landing

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19
Q

When is the ditching switch available

A

Below 15000 ft in auto mode

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20
Q

When is the ditching switch not available

A

Above 15000ft or in manual mode

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21
Q

How can you close the out flow valve in manual mode

A

Turn Man rate knob to max down

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22
Q

How long is the cabin pressurized to 300ft below TO alt

A

6000ft or 10min

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23
Q

When the roll disconnect is pulled who controls what

A

Left seat controls roll spoilers
Right seat controls ailerons

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24
Q

What is attached to the gust lock

A

The ailerons and throttles

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25
Q

How are the elevators and rudder gust locked

A

Trapped hydraulic fluid

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26
Q

What happens to the rudder if the right hydraulic system fails

A

The aux hydraulic system powers the lower rudder PCU

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27
Q

When is the yaw damp inhibited

A

Above 60knts until weight off wheels

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28
Q

How does the rudder trim work

A

Actuates the rudder because there is no trim tab

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29
Q

What is config trim

A

Auto trim movement when flaps or spoilers are extended or retracted

30
Q

In normal ops how long does the flaps take 0-20

A

Does not exceed 20 sec

31
Q

What is required for ground spoilers to be armed

A

Both throttles in TO or above
Main wheel speed of 60knts or greater
Wow and RA > 7ft

32
Q

What items are part of the TO config warning system

A

Flaps
Spoilers
Parking break
AP
All trims
Roll/pitch disconnect

33
Q

What are the functions of primary stab trim

A

Config trim
Mach trim
Variable rate pitch trim

34
Q

What do we loose in sec stab trim

35
Q

Will the cabin remain pressurized on trim air only

36
Q

What is the max alt for trim air

37
Q

How many safety valves does the aircraft have

A

2 over pressure and under pressure

38
Q

What is the power source of the safety valves

A

A spring, has no power

39
Q

What needs to be done if a fire extinguisher is used in the cabin

A

Pilots need to wear oxygen mask, goggles emer oxygen

40
Q

Does the oxygen mask have an auto mode

A

Yes, when cabin alt above 35,000 mask automatically does EMER oxygen

41
Q

What is a warning for a stab trim runaway

A

The clacker

42
Q

When the engine anti ice is on what is heated

A

Engine cowling leading edge
T2 probe

43
Q

How is the T2 probe heated

A

Electrically

44
Q

How do you know the T2 probe heat failed

45
Q

What is the difference between CAS and EICAS

A

CAS - crew alerting system
EICAS- Engine Instruments crew alerting system

46
Q

What is the normal power source for the standby instrument lighting

A

L main bus

47
Q

When can you use ram air

A

Below 10,000
Flying unpressurized
When the QRH tells you to

48
Q

Pack air is

49
Q

Trim air is

50
Q

When do you need engine anti ice

A

10*C or below
Ground contamination

51
Q

When do you need wing anti ice

A

5* C on the ground
10* C in flight
Below 210 knots in icing conditions

52
Q

Where are the oxygen tanks

A

In the lav

53
Q

What is the oxygen blow out disk for

A

Over pressure in the system

54
Q

What are the oxygen mask limitations

A

-5* C
40,000-41,000

55
Q

What is the concern with manually deploying oxygen masks

A

The oxygen is unregulated, continuous flow of oxygen

56
Q

What is the max Delta P

57
Q

Where are the PBE

A

1 behind the left pilot seat
1 in the lav

58
Q

What needs to happen if the med kit is opened

A

MELed
Inventoried

59
Q

When are the Emergency lights activated when armed

A

Loss of power to the R main Bus

60
Q

What is the normal source of power for the emergency lights

A

R main bus

61
Q

How long do the emergency lights last

62
Q

When does the FDR start recording

A

Beacon or Weight off wheels

63
Q

What’s should you do if you loose WAAS

A

Change WAAS to Baro in arrival data index page 2

64
Q

When does the stick shaker activate

A

.88 AOA/bottom of the red on AOA tape

65
Q

When does the pusher activate

A

1.0 AOA /top of the red on AOA tape

66
Q

Is the AOA the primary source for stall indication

A

No, shaker and airspeed are

67
Q

What constitutes an Emergency safe altitude

A

MAA
MSA
MVA
TPA

68
Q

What powers the main entry and exit lights

A

Left battery bus

69
Q

Where is the switch for the secondary nav lights

A

The right avionics rack CB panel

70
Q

Do we need 1 or both ice detectors to generate an EICAS?