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T-1 > Systems 1 > Flashcards

Systems 1 Flashcards

1
Q

The annunciators on the shroud panel are designed to _______

A

Get the attention of the crew

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2
Q

The MASTER TEST switch and GO/NOGO annunciators ________

A

Check the status of eight different systems

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3
Q

Aural Warnings consist of _______

A

Tones, horns and voice messages

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4
Q

What can you reference in T.O. T1-1A to determine the meaning of an annunciator on the main annunciator panel?

A

Section III, Figures 3-12 and 3-13

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5
Q

Who is responsible for handling emergencies on the T-1?

A

The entire crew

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6
Q

What does it mean when the L F/V CLOSE switchlight on the shroud panel is illuminated amber?

A

The left fuel valve is closed and no fuel is flowing to the left engine.

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7
Q

If the amber L GEN OFF annunciator on the main annunciator panel illuminates, what flashes?

A

The two MASTER CAUTION RESET switchlights

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8
Q

Bypass Air _______

A

Helps cool the core of the engine

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9
Q

The low compressor _______

A

Is driven by a two-stage turbine

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10
Q

ITT probes are located _______

A

Between the core and fan turbine

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11
Q

The fan is connected to the low compressor turbine by a

A

Shaft running through the center of the hollow impeller shaft

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12
Q

The performance of the core engine is measure by _____

A

The N2 gauge

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13
Q

During engine start, ITT should not exceed ______ °C

A

550

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14
Q

If the ITT is between 550°C and ______°C for less than 4 seconds, you can try to start again.

A

600

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15
Q

Where are the navigation lights installed on the T-1A?

A

In each wingtip, as well as the top of the vertical stabilizer trailing edge.

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16
Q

What would you do to extend and illuminate the landing lights following an automatic retraction?

A

Recycle the landing light switches from the EXT/ON to RET/OFF and back to EXT/ON

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17
Q

Upon initially arriving at the aircraft, you want to turn on some interior lights. What lights illuminate if you push the ROOM LIGHT switch?

A

Two general area flood lights in the cabin area

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18
Q

How do you illuminate circuit breaker panels?

A

Push the C/B LT pushbutton switch on the aft circuit breaker panel.

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19
Q

The anti-collision strobe lights are

A

White and located in each wingtip and and the aft most point of the fuselage

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20
Q

The wing inspection lights

A

Are an aid for checking ice formation

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21
Q

If the landing light switches are set to the EXT/ON position, what will happen when you retract the landing gear?

A

The landing lights will automatically retract and extinguish.

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22
Q

During night ops, how should you set the cabin lights?

A

At a level to reduce glare on the flight deck.

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23
Q

The emergency lighting system is controlled by ________

A

A guarded switch on the overhead control panel

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24
Q

If the INTEG switch is on, what will happen if the L LOAD BUS fails?

A

The panel flood lights will illuminate

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25
Q

With primary power available to all busses, what normally powers the standby bus?

A

Left Load Bus

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26
Q

Where is the standby battery located?

A

Nose compartment

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27
Q

With the battery bus in EMER position, the main aircraft battery powers the __________

A

Emergency Bus

28
Q

The STBY PWR switchlight ON indication illuminates amber when _________

A

The standby bus is being powered by the standby battery

29
Q 
Which of the following is powered by the standby bus?
EADI #1
Left and Right fuel flow gauges
RTU #1
Left N1 guage
A

RTU #1

30
Q

When operating with only emergency and standby buses, what will not be available?

A

Normal pitch trim

31
Q

The standby batter provides

A

24-volt DC power

32
Q

Under normal operating conditions (both generators online and the battery switch set to ON), what is the source of power for the emergency bus?

A

Generator power through the emergency bus power feed line.

33
Q

To arm the standby battery,

A

Press the standby power switch light

34
Q

When operating with only emergency and standby electrical power, the crew can lower the landing gear using normal procedures.

A

False

35
Q

The two inverters produce what kind of power?

A

26 and 115-volt AC power

36
Q

From which source does the NO. 2 inverter normally receive power?

A

Right load bus

37
Q

Each inverter regulates its own voltage and frequency output.

A

True

38
Q

An illuminated AC BUS SHED annunciator on the pilot’s shroud panel indicates ________

A

The AC shed buses are de-energized

39
Q

The AC voltmeter ______

A

Displays the voltage of one of four sources of AC power as selected by the AC voltmeter selector switch

40
Q

The NO. 1 inverter usually receives power from what source?

A

LH Load Bus

41
Q

With both load buses powered and the inverter selector switch set to to AUTO, a failure of the NO. 1 inverter causes _________

A

the NO. 2 inverter to power the primary AC buses and the AC shed buses.

42
Q

If the RH LOAD BUS loses power, the NO. 2 inverter can be powered by the ________

A

Emergency bus

43
Q

What are the power sources of the T-1A DC electrical system?

A

Battery, generators and external power unit

44
Q

What kind of power/battery does the T-1A have?

A

24-volt DC lead-acid, located in the aft fuselage compartment.

45
Q

What kind of power is produced by the T-1A starter generators?

A

28-volt DC power

46
Q

T or F: The main aircraft battery is capable of providing power to all DC buses

A

True

47
Q

Illumination of the L BUS FDR FAIL annunciator indicates that the _______

A

Standby feeder on the left side is active

48
Q

What happens if both master generator switches are moved to EMER?

A

Both generators are isolated from their main buses.

49
Q

While performing a GPU assisted start, the generator RESET switches should be in the ________ position

A

OFF

50
Q

While performing a battery start, the generator RESET switches should be in the ________ position

A

AUTO

51
Q

Do not perform a battery start if the battery voltage is below ________

A

22 volts DC

52
Q

What is max generator load if one generator is operating at FL270?

A

400 amps

53
Q

What is the max generator load if one generator is operating above FL325 or on the ground?

A

280 amps

54
Q

What is the primary source of DC power while in flight?

A

28-volt generators

55
Q

Under normal operating conditions, how many feeders carry power from each main bus to its corresponding load bus?

A

Two feeders

56
Q

During engine start, the GCU removes power from the starter when the engine reaches approx ______ %N2

A

35-40

57
Q

If the right generator fails in flight, what is the impact on the electrical system?

A

No buses loses power.

58
Q

The fuselage fuel indicator measures

A

The total fuel remaining in the fuselage tanks

59
Q

Fuel is fed directly to the engines from the

A

Fuel feed chambers

60
Q

During fuel crossfeed, fuel flow from the engines is supplemented by _______

A

A boost pump

61
Q

The primary jet pumps are driven by

A

Motive flow

62
Q

Where are the remote control circuit breakers located? (RCCB)

A

Aft fuselage compartment

63
Q

What is the normal position for the inverter selector switch?

A

AUTO

64
Q

The No. 1 inverter is supplied 28-volt DC electrical power from the LEFT LOAD BUS.

A

True

65
Q

The AC voltmeter is located where?

A

The aft circuit breaker panel

T-1 (6 decks)

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