A330 Electrical Flashcards

1
Q

If APU and EXT A and B are connected which system has priority over which?

A
  • APU GEN will have priority over EXT B to power AC1

- EXT A will power AC2

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2
Q

How much power can each EXT PWR supply?

A

90kVA max

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3
Q

How long does NBPT take?

A
  • Milliseconds

- APU can take up to 15sec

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4
Q

Once the IDG’s are disconnected, can they be re-connected?

A

Only on ground by maintenance

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5
Q

If the EMER GEN is powered by the RAT only, what can occur?

A
  • If slats are extended, EMER GEN deactivates

- Can be re-activated when slats are retracted and MAN ON pb is pressed.

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6
Q

Which has a higher priority? GEN 1/2, APU GEN, EXT A/B

A
  1. GEN 1/2
  2. APU GEN
  3. EXT A/B
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7
Q

How many generators are there?

A
  • 2 engine generators
  • 1 APU generator
  • 1 emergency generator
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8
Q

Where are the circuit breakers located?

A

Electronic Equipment Bay (Avionics Bay)

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9
Q

How much power can each GEN supply?

A

115kVA of three phase 115/200V 400Hz

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10
Q

What does NBPT stand for?
What does this system do?
When is it active?

A
  • No Break Power Transfer
  • Prevents busbar power interruption during supply source transfer
  • On ground only
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11
Q

How is the emergency generator driven?

A
  • By the green hydraulic circuit via
  • Engine 1 and or 2
  • RAT
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12
Q

How are GEN1 and GEN2 driven?

A

By engine 1 and 2 via an integrated drive

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13
Q

What happens when both GEN1 and GEN2 are lost?

A
  • The emergency gen kicks in
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14
Q

What system controls the contactors?

A

Electrical Contactor Management Unit (ECMU)

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15
Q

What happens if one generator is shut down due to over-current detection?

A
  • The related AC BUS is lost

- No re-configuration

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16
Q

If one generator is lost what happens?

A
  • Re-configuration

- GEN1/2 powers complete system

17
Q

How does the ECMU control the NBPT?

A

It takes control of both busbars for a short period of time and synchronizes the frequencies.

18
Q

If AC1 fails, what happens?

A
  • Re-configuration
  • AC1 is lost completely
  • AC2 powers AC ESS and ESS TR
19
Q

How much power can the APU GEN supply?

A

115kVA of three phase 115/200V 400Hz

20
Q

What happens when the ESS TR and TR 1 or 2 has failed?

A
  • The DC ESS bus is lost
21
Q

What happens when one of the TR’s fail?

A
  • Re-configuration

- The other TR replaces the faulty one

22
Q

Where can electrical power be supplied from?

A
  • 2 Generators
  • 1 Emergency Generator
  • APU Generator
  • 3 Batteries (1 for APU start only)
  • 2 External Power Plugs
23
Q

How is the APU generator driven?

A

Directly by APU

24
Q

What system controls the NBPT?

25
How are the main generators controlled? What does it control?
- Generator Control Unit | - Frequency and Voltage
26
What two types of electrical supply does the A330 have?
- 115/200V 400Hz AC | - 28V DC
27
Your APU is inop and you’ve started one engine on the bay and you decide to start the second engine during pushback, what do you need to be aware of?
- There is no NBPT active between GEN1 and GEN2 | - Power interruptions may occur in system (cabin systems)
28
How much power can the emergency generator supply?
- 8kVA three-phase 115/200V 400 Hz | - when RAT supplies power and speed below 260kts then 3.5kVA