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T-1 18-12 > SYS2 Test Review (Electronics) > Flashcards

SYS2 Test Review (Electronics) Flashcards

1
Q

What are the DC sources for the T-1

A

Battery, Starter/Generator, GPU

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2
Q

Describe T-1 Main Battery

A

24 volt, 40 ampere-hr, lead-acid

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3
Q

min battery voltage

A

22v

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4
Q

Where is the main battery located?

A

Aft Fuselage

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5
Q

Can the main battery power all the electronics?

A

Yes

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6
Q

Where is the external power receptacle?

A

Left fuselage

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7
Q

Describe the generator properties

A

28 volt, up to 400 amps

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8
Q

N2 required for single generator operations?

A

58%

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9
Q

Max Load for single generator operations on the ground?

A

280 amps

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10
Q

In-flight limitations for single generator operations

A

Below 32,500 ft: 400 amps

Above 32,500 ft: 280 amps

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11
Q

In-flight limitations for dual generator operations

A

280 amps

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12
Q

What component helps equalize the generator load?

A

GCU Generator Control Unit

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13
Q

Switch positions of the Master Generator Switch?

A

EMER and NORM

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14
Q

How many bus feeder lines are normally powered?

A

2

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15
Q

Where is the STBY BATT switch?

A

Co-pilot instr. panel

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16
Q

How do you arm the STBY BATT?

A

Push the button, it will say ARM

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17
Q

STBY Battery: Volts, Location, Type?

A

24v, Nose compartment, Lead-acid

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18
Q

What buses can the STBY BATT power?

A

only the STBY BUS

19
Q

What does placing the BATT switch into the EMER position do?

A

Sends main battery power directly to the EMER BUS

20
Q

What does placing the BATT switch into the EMER position do?

A

Sends main battery power directly to the EMER BUS

21
Q

What are the AC power sources?

A

Inverters

22
Q

Inverter voltage/frequency?

A

26v, 115v, 400Hz

23
Q

1 inverter normally powered from which bus?

A

LH Load Bus

24
Q

2 inverter normally powered from which bus?

A

RH Load Bus

25
Q

Inverter Selector switch positions?

A

1, #2, AUTO

26
Q

If Inverter Selector switch positioned to #2, what happens?

A

2 inverter powers the primary AC buses

27
Q

What conditions will trigger the AC BUS SHED annunciator?

A

2 inverter powering the primary AC buses AND the #2 inverter is being powered by the EMER BUS

28
Q

Limitations of the LDG lights?

A

200 KIAS

Only below 20,000 MSL

29
Q

Describe the NAV lights

A

Red (left wingtip)
Green (right wingtip)
White (vertical stab. trailing edge)

30
Q

Describe the Anti-collision lights

A

3 white strobe lights, one on each wingtip, one on aft-most point of tail

50-60 cycles/min

31
Q

Describe the rotating beacon

A

Red, top of the vertical stab.

45-55 cycles/min

32
Q

Describe the wing inspection lights

A

White lights, shine on the leading edge of each wing to inspect for ice

33
Q

Describe the LDG lights

A

2 white lights that extend from the nose of the aircraft

34
Q

If the LDG gear is retracted, the LDG lights will …

A

Automatically retract and shutoff

35
Q

Flood Lights

A

Shine from beneath the shroud panel

36
Q

The flood lights will automatically turn on when …

A

INTEG ON

LH Load Bus loses power

37
Q

Emergency Lighting System control located …

A

Top right of overhead panel

38
Q

Emergency Lighting System control located …

A

Top right of overhead panel

39
Q

What gets checked when Emer Lighting is placed in TEST position?

A

Exit lights and 2 cabin overhead general lights

40
Q

Indications of a single generator failure?

A

MASTER WARNING
red GEN OFF
no volts or amps for that side

41
Q

required N2 for single generator operations

A

58%

42
Q

What is a remote control circuit breaker?

A

Circuit breaker for those that are inaccessible to the pilot (aft-fuselage)

43
Q

What kind of circuit breaker do the Radio Masters and Non-essential Bus use?

A

Switch circuit breakers

T-1 18-12 (23 decks)

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