Training Interview Study Flashcards

(61 cards)

1
Q

The main door is sealed by?

A

An inflatable seal supplied by 18psi de-ice air via storage accumulator

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2
Q

Vmo?

A

243kt - 0-17,000ft
214kt - 20,000ft - 25,000

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3
Q

MLW?

A

19,051kg

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4
Q

When Battery Master is selected on which busses will receive power?

A

Essential Busses

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5
Q

How many inverters are required to power the entire 115VAC fixed system?

A

One

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6
Q

What is the minimum battery voltage required for a batter power engine start?

A

22 Volts

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7
Q

What type of and how many batteries does the aircraft have?

A

2 Batteries, one main, one AUX.
40amp/h NICAD Battery

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8
Q

Max DC Gen Load Ground

A

0.7

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9
Q

What is the purpose of the BBPU?

A

To detect amperage over 400 on a generator and inhibit the bus tiesW

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10
Q

What busses are powered by the TRUs?

A

SecondaryI

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11
Q

If both TRUs fail will the secondary busses be powered and how?

A

Vertical bus ties close to power the busses

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12
Q

What will happen if the APU fire test is carried out with the APU running?

A

The APU will shut down and if the test is prolonged the fire suppression system may activate.

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13
Q

Fire detection in the cargo hold is provided by?

A

Two smoke detectors

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14
Q

What happens when you pull the T Handles?

A

1- Arms Fire Bottles
2 - Close Fire Wall SOV
3 - Close hydraulic SOV

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15
Q

When the emergency lights are activated where does the PA system power come from?

A

Battery Bus

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16
Q

How are the outflow valves controlled?

A

Forward outflow valve manually and the two rear valves are controlled by the CPC

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17
Q

What is the purpose of the ISO switch for the Ice System?

A

To seperate the two systems so that the tail, inboard wing and intake boots can be inflated

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18
Q

Max fuel imbalance?

A

272kg

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19
Q

How many KG are left when the low fuel caution light comes on?

A

59kg

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20
Q

What position must the dump valve be for fueling

A

Open

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21
Q

What implications does a fueling on caution light have in flight?

A

Fuel transfer unavailable

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22
Q

ITT For Starting?

A

800-840 - 20 Sec
840-900 - 12 Sec
900-950 - 5 Sec

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23
Q

What is the maximum SHP

A

2380

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24
Q

Max Torque Cont Operations 1200RPM

A

90% @ 1200RPM

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25
Transient Engine Settings Are Allowed For How Long?
20 Seconds
26
What temp does the temp overtemp light come on at?
800 deg
27
What is the prohibited range for the props?
500-780RPM
28
What keeps the propellers out of the prohibited range?
The ECU monitoring fuel
29
How are the AC gens and Hydraulic Pumps Powered
Reduction Gearbox
30
With the ignition to AUTO when will the ignitors activate?
1 - NH goes below 60% in flight 2 - During Start 3 - ESS Busses Powered and condition lever selected above fuel off
31
Propeller overspeed protection is provided by?
Pneumatic action of the Prop Overspeed Governor at 1308RPM
32
What will cause auto feather to activate on takeoff?
Failed torque below 28% and good torque above 38%
33
When will the SPU's operate?
When the flap is selected to greater than zero or the SPUs are selected on
34
While taxiing with engine 1 shut down what provides hydraulics to the #1 system?
The #1 SPU
35
Normal pressure of the hydraulic engine driven pumps?
3,000psi
36
What are the flow rates of EDP/SPU/PTU
EDP - 9.5gpm SPU - 1.5gpm PTU - 4.5gpm
37
The PTU will automatically activate on take off if what engine fails?
#2
38
What does a LANDING GEAR INOP caution light indicate
An alternate landing gear extension will need to be carried out
39
Will nose wheel steering be available after an alternate extension?
Nope
40
Under which circumstances can a landing gear warning horn be muted?
One power lever at or near flight idle below 130kias
41
What two things are inhibited when the inhibit switch is used?
Normal landing gear extension and nose wheel steering.
42
Maximum speed for alternate extension?
140kias
43
What activates Antiskid after landing?
Either; 1 - Wheel speed above 35kt 2 - 3sec after WOW sensor
44
How many degrees does the rudder control the steering by?
7 degrees
45
Which component ensures the gear cannot fully extend or retract unless the doors are open?
The mechanical sequenceing valve
46
What can a NOSE STEERING caution indicate
Either; 1 - Loss of power to NWS 2 - Nose Wheel is exceeding the 60degree limiit
47
In normal flight each rudder receives how much pressure?
1500psi below 150kt 900psi above 150kt
48
What is the purpose of ARPS
Ensures hydraulic pressure is available to the upper rudder actuator if hydraulic fluid is lost from the #2 system
49
How is roll control achieved?
Cables to ailerons, hydraulics to spoilers
50
What does FLAP POWER caution indicate?
Pressure less than 1500psi during flap operation
51
What does a BASIC light mean?
ADC input has failed to the APIRS
52
How are the airspeed indicators driven?
Directly from Pitot
53
Minimum O2 dispatch 2/3 crew?
1,300psi/1,800psi
54
How many portable O2 bottles are there and where are they stowed?
3 in the forward emergency equipment cupboard and 2 in a draw behind row 12 C/D
55
Maximum Baggage Load
1,134kg
56
How many fire extinguishers are there?
Five - 1 In Cockpit - 1 in GEEC - 2 in REEC - 1 in Overhead 11/12CD locker
57
What emergency exit cannot be opened from the outside?
The wing exits
58
What does NOSIG on a METAR mean?
No significant changes expected in the next two hours
59
When are you required to nominate a weather alternate?
Cloud - 1,000ft above minima. Vis - 5km or 2km above landing vis.
60
Severe Ice Procedure
AP - DISC Condition Levers - Max Power Levers - As Req Min Airspeed - 160kias Exit Ice
61