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Normal Checklist for Flight > Cockpit Prep Flow/Checklist > Flashcards

Cockpit Prep Flow/Checklist Flashcards

To better understand some of the items on the Cockpit Flow

1
Q

Circuit Breaker: Pretty self explanatory.

A

Check

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2
Q

What CBP is behind the pilot seat

A

CBP-1

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3
Q

What CBP is behind the Co-Pilot seat

A

CBP-2

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4
Q

What CBP is at the pilots left leg

A

CBP-3

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5
Q

What CBP is at the co-pilots right leg

A

CBP-4

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6
Q

What CBP is in the aft equipment bay

A

CBP-5

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7
Q

What CBP is in the nose

A

CBP-6

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8
Q

Gen 1/2

A

Off/Reset

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9
Q

What are the main generators rating up to 35,000 feet

A

30kVA

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10
Q

What are the main generators rating up to 41,000 feet

A

25kVA

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11
Q

AUTOXTFER Switch/lights

A

Both extinguished

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12
Q

In general terms what is the function of the AUTOXTFER

A

To ensure AC bus’s 1/2 remain powered at all times

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13
Q

Bus priority logic

A

Onside Gen APU Gen Cross-side Gen External AC

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14
Q

Why would you want to inhibit (selecting off (off white light) auto transfer

A

to isolate a main AC bus in the event of an electrical emergency

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15
Q

On the AUTOXFER switch/lights what does the “OFF” light indicate

A

that the crew pressed the switch/light to prevent auto transfer. Look at AC synoptic page

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16
Q

On the AUTOXFER switch/lights what does the ‘FAIL” light indicate

A

That auto transfer fail. Look at AC synoptic page

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17
Q

Will AUTOXFER automatically happen

A

Yes

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18
Q

ESS POWER (AC ESS XFER) Switch/Light

A

Extinguished

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19
Q

What does it mean when the ESS POWER switch/light is illuminated

A

The ESS Bus is normally powered by AC bus 1, which is essential to flight, if this is illuminated AC bus 1 is not powering the ESS Bus.

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20
Q

What else will power the AC ESS Bus

A

AC Bus 2 or the ADG Bus

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21
Q

AC/DC UTILITY Switch/light

A

Extinguished

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22
Q

What do it mean if the AC/DC UTILITY Switch/light is illuminated

A

That all utility busses have been shed

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23
Q

Will the AC/DC UTILITY Switch/light illuminate if one bus is shed

A

No

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24
Q

What happens when this switch/light is illuminated or pushed

A

Ties DC Bus 1 and 2 together to the working TRU. The DC Utility Bus’s 1 and 2 will be shed

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25
Q

LANDING LTS

A

Off

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26
Q

What are the limitations on the Landing/Taxi Lights

A

Do not illuminate on the ground except for takeoff and landing

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27
Q

IGNITION

A

OFF

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28
Q

When does ignition com on automatically

A

During a stall or when the stall system is being tested.

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29
Q

What are the 5 conditions that require continuous ignition

A
  1. vicinity of thunderstorms 2. contaminated runways 3. high crosswinds 4. moderate of heavier rain 5. moderate or heavier turbulence
30
Q

DUMP Switch/Light

A

Extinguished and covered

31
Q

What are fuel dumping limitation

A

Flaps 0 and not in the vicinity of thunderstorms

32
Q

L & R PACK Switch/Lights

A

EXTINGUISHED

33
Q

On the Air Condition panel you have the temperature control knobs (NORM, STBY, MAN). In the NORM mode what controls the temp

A

The fan and duct sensor

34
Q

On the Air Condition panel you have the temperature control knobs (NORM, STBY, MAN). In the STBY mode what controls the temp

A

Only the duct sensor

35
Q

On the Air Condition panel you have the temperature control knobs (NORM, STBY, MAN). In the MAN mode what controls the temp

A

Fan and duct sensors are removed. Requires constant monitoring

36
Q

What would cause a PACK FAIL light to illuminate

A

Over temp/pressure or if the pressure regulating valve fails

37
Q

If in flight and using one PACK what happens to the remaining PACK

A

It goes into HIGH Mode

38
Q

What other time will the PACK’s go into High Mode

A

When on the ground with the APU on

39
Q

If a PACK fails due to over press/temp does the other PACK automatically go to High Mode

A

No, the failed pack must be deselected

40
Q

RAM-AIR Switch Light

A

Extinguished

41
Q

What is the function of the RAM-AIR switch/light

A

To allow air to ventilate the cockpit and cabin during un-pressurized flight

42
Q

What is the recommended airspeed to provide sufficient airflow to the cabin

A

250 knots

43
Q

CABIN PRESSURIZATION SELECTOR

A

Set

44
Q

The knob with the “R” (rate knob) on it should be set where and why

A

The white “dot” on the rate knob should be set to the white “triangle” (pip mark). This set the climb rates to 500 up and 300 down.

45
Q

The Cabin Pressure Controler (CPC) has a Flight Abort Mode, what is this

A

CPC will drive the cabin altitude back to the takeoff field elevations should it detect a flight abort.

46
Q

For the Flight Abort Mode to work what three things must be met

A
  1. Less than 10 have elapsed since takeoff 2. Aircraft has climbed less than 6,000 feet 3. Descent has been detected (greater than 1000 feet from max altitude)
47
Q

DUCT MON

A

Should be in NORM mode

48
Q

What is tested when the DUCT MON selector is selected to TEST

A

Verify all sensing element loops continuity by simulating an over heat conditions

49
Q

During the DUCT MON TEST will there be an EICAS message if all checks normal

A

Yes, you will see a DUCT TEST OK in green

50
Q

When the DUCT MON selector switch is turned to Loop A or B what are we testing

A

Individually testing each left and right 10th-stage loop for shorts

51
Q

If the loop test is normal will there be an EICAS message

A

Yes, LOOP A/B TEST OK

52
Q

What is 10th-stage air used for

A

Engine start, air conditioning and pressurization

53
Q

What is 14th-stage air used for

A

Wing/Cowl anti-ice and trust reverse

54
Q

L&R WSHLD/WIND

A

TEST

55
Q

How is the WSHLD/WIND tested

A

The WSHLD/WIND switches are placed in HI mode and depressing the TEST switch

56
Q

What 4 EICAS messages should you see when testing the WSHLD/WIND

A

L/R WINDOW HEAT OK L/R WSHLD HEAT OK

57
Q

Can the WSHLD/WIND system be tested in the LOW position

A

Yes, but only the window heat will be tested

58
Q

STALL PROT PUSHER

A

ON

59
Q

Will the Stick Shaker work if one of the STALL PROT PUSHER’s is switches is off

A

Yes, the stick shaker will shake but the PUSHER will be disabled

60
Q

While performing the Stall Protection System (SPS) test what is being demonstrated when the AP/SP DISC is pressed

A

To ensure that the PUSHER can be disconnected

61
Q

What is the CAUTION associated with performing the SPS TEST

A

Do not conduct test while refueling

62
Q

L&R THRUST REVERSER

A

ARMED

63
Q

Which bleed air system powers the THRUST REVERS

A

14th-stage

64
Q

Is there an EICAS message associated with arming the THRUST REVERS

A

Yes, green L/R REV ARMED

65
Q

What are the memory items associated with REV UNLOCKD

A
  1. Thrust lever- Idle [PF] 2. Auto-throttle- Disconnect [PF] 3. EMER STOW- Press [PM]
66
Q

PITCH DISC

A

STOWED

67
Q

What happens when the PITCH DISC is pulled

A

In the case of an elevator jam the Left and Right Elevator circuits can be isolated to determine which elevator is working (at a reduced pitch authority)

68
Q

MLG BAY OVHT TEST

A

CHECK

69
Q

What occurs during the MLG BAY OVHT TEST

A

To verify the continuity of the system by simulating an over heat condition

70
Q

On the MLG BAY OVHT TEST Panel what does the FAIL TEST switch determine

A

This test the ability of the system to detect an actual overheat condition or a short

Normal Checklist for Flight (3 decks)

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