Electrical Flashcards

1
Q

What are the Main AC electrical power sources on the LCF aircraft?

A

Four IDGs
Two external power sources

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2
Q

What is the function of the Standby Power Switch in the Auto position?

A

Allows the main and APU standby busses to be powered from available sources.

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3
Q

What does the “AVAIL” light indicated on the external and APU power switches?

A

The related power source is plugged in and available, and the power quality is acceptable.

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4
Q

When is the main cargo deck handling bus powered?

A

When the “AVAIL” light is displayed on the APU 2 or EXT 2 switches.

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5
Q

What electrical power source provides power for the lower lobe cargo handling, fueling panel, and AUX 4 hydraulic pump.

A

EXT PWR 1 or APU GEN 1 is AVAIL or selected ON (powering the ground handling bus)

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6
Q

What are some of the items powered by the utility busses?

A

5 fuel pumps
Galley equipment

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7
Q

What happens when you pus a Generator Drive Disconnect (DRIVE DISC) switch?

A
  • disconnects IDG from engine when above idle speed
  • opens the related Generator Control Breaker (GCB)
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8
Q

What condition would automatically disconnect the IDG if not manually disconnected y the flight crew?

A

Excessively high drive oil temperature

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9
Q

What does a Bus Isolation (ISLN) light illuminated indicate?

A
  • Bus Tie Breaker (BTB) OPEN
  • AC bus isolated from the syncrhonous bus
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10
Q

How do you reconnect an IDG that has been disconnected?

A

IDG cannot be restored by flight crew action
- maintenance action is required

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11
Q

How is the electrical system configured during an automatic ILS approach (autoland)?

A
  • AC and DC busses 1,2, and 3, are isolated form the synchronous bus

-AC bus 4 continues to power the synchronous bus

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12
Q

What are the main AC electrical power sources?

A

4 IDGs
2 APU sources
2 EXT PWR sources

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