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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
LANDING LTS
Off
26
What are the limitations on the Landing/Taxi Lights
Do not illuminate on the ground except for takeoff and landing
27
IGNITION
OFF
28
When does ignition com on automatically
During a stall or when the stall system is being tested.
29
What are the 5 conditions that require continuous ignition
1. vicinity of thunderstorms 2. contaminated runways 3. high crosswinds 4. moderate of heavier rain 5. moderate or heavier turbulence
30
DUMP Switch/Light
Extinguished and covered
31
What are fuel dumping limitation
Flaps 0 and not in the vicinity of thunderstorms
32
L & R PACK Switch/Lights
EXTINGUISHED
33
On the Air Condition panel you have the temperature control knobs (NORM, STBY, MAN). In the NORM mode what controls the temp
The fan and duct sensor
34
On the Air Condition panel you have the temperature control knobs (NORM, STBY, MAN). In the STBY mode what controls the temp
Only the duct sensor
35
On the Air Condition panel you have the temperature control knobs (NORM, STBY, MAN). In the MAN mode what controls the temp
Fan and duct sensors are removed. Requires constant monitoring
36
What would cause a PACK FAIL light to illuminate
Over temp/pressure or if the pressure regulating valve fails
37
If in flight and using one PACK what happens to the remaining PACK
It goes into HIGH Mode
38
What other time will the PACK's go into High Mode
When on the ground with the APU on
39
If a PACK fails due to over press/temp does the other PACK automatically go to High Mode
No, the failed pack must be deselected
40
RAM-AIR Switch Light
Extinguished
41
What is the function of the RAM-AIR switch/light
To allow air to ventilate the cockpit and cabin during un-pressurized flight
42
What is the recommended airspeed to provide sufficient airflow to the cabin
250 knots
43
CABIN PRESSURIZATION SELECTOR
Set
44
The knob with the "R" (rate knob) on it should be set where and why
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
The Cabin Pressure Controler (CPC) has a Flight Abort Mode, what is this
CPC will drive the cabin altitude back to the takeoff field elevations should it detect a flight abort.
46
For the Flight Abort Mode to work what three things must be met
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
DUCT MON
Should be in NORM mode
48
What is tested when the DUCT MON selector is selected to TEST
Verify all sensing element loops continuity by simulating an over heat conditions
49
During the DUCT MON TEST will there be an EICAS message if all checks normal
Yes, you will see a DUCT TEST OK in green
50
When the DUCT MON selector switch is turned to Loop A or B what are we testing
Individually testing each left and right 10th-stage loop for shorts
51
If the loop test is normal will there be an EICAS message
Yes, LOOP A/B TEST OK
52
What is 10th-stage air used for
Engine start, air conditioning and pressurization
53
What is 14th-stage air used for
Wing/Cowl anti-ice and trust reverse
54
L&R WSHLD/WIND
TEST
55
How is the WSHLD/WIND tested
The WSHLD/WIND switches are placed in HI mode and depressing the TEST switch
56
What 4 EICAS messages should you see when testing the WSHLD/WIND
L/R WINDOW HEAT OK L/R WSHLD HEAT OK
57
Can the WSHLD/WIND system be tested in the LOW position
Yes, but only the window heat will be tested
58
STALL PROT PUSHER
ON
59
Will the Stick Shaker work if one of the STALL PROT PUSHER's is switches is off
Yes, the stick shaker will shake but the PUSHER will be disabled
60
While performing the Stall Protection System (SPS) test what is being demonstrated when the AP/SP DISC is pressed
To ensure that the PUSHER can be disconnected
61
What is the CAUTION associated with performing the SPS TEST
Do not conduct test while refueling
62
L&R THRUST REVERSER
ARMED
63
Which bleed air system powers the THRUST REVERS
14th-stage
64
Is there an EICAS message associated with arming the THRUST REVERS
Yes, green L/R REV ARMED
65
What are the memory items associated with REV UNLOCKD
1. Thrust lever- Idle [PF] 2. Auto-throttle- Disconnect [PF] 3. EMER STOW- Press [PM]
66
PITCH DISC
STOWED
67
What happens when the PITCH DISC is pulled
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
MLG BAY OVHT TEST
CHECK
69
What occurs during the MLG BAY OVHT TEST
To verify the continuity of the system by simulating an over heat condition
70
On the MLG BAY OVHT TEST Panel what does the FAIL TEST switch determine
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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