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Questions for Electricals A320

Answer the following questions

1. Which of the following AC busses can be powered by the emergency generator?
2. When will the RAT & EMER GEN red FAULT light illuminate?
3. During the five seconds it takes for the RAT to extend:
4. While operating on Emergency Electrical Power with the landing gear lowered which of the following control laws is in effect?
5. The APU is supplying the electrical system. What is the order of priority for the different generators?
6. What is the function of APU GEN push button located on the overhead electrical panel?
7. If normal electrical power is lost; essential cockpit lighting is maintained for the:
8. The emergency generator supplies power as long as:
9. The IDG Fault light indicates:
10. An AC ESS FEED switch located on the overhead panel shifts the power source for the AC ESS bus from:
11. What cockpit lighting is available during an emergency electrical situation?
12. Are there any limitations associated with disconnecting an IDG?
13. You enter a dark cockpit, what action is necessary before checking the battery voltages?
14. Do not depress the IDG DISCONNECT switch for more than _______ to prevent damage to the disconnect mechanism.
15. What is the function of the GEN 1 LINE push button?
16. The A-320 has _______ batteries in its main electrical system.
17. The purpose of the AUTO BUS TIE is to allow either engine-driven IDG to automatically power both main AC buses in the event of a generator loss until either ground power or the APU generator is activated.
18. Is it possible to parallel generators?
19. The BAT FAULT light will illuminate when:
20. What is the minimum voltage when conducting a BATTERY CHECK?
21. During a routine flight, which of the following would result after the loss of Gen #2 and the subsequent start of the APU?
22. Having started the APU, how can you get the APU generator to power the electrical system?
23. What is the significance of the green collared circuit breakers?
24. The number 1 AC bus channel normally supplies power to _____ and to the _____ bus which supplies power to the ______ bus.
25. The RAT is connected directly (mechanically) to the Emergency Generator
26. The normal priority for supplying electrical power to the AC busses is:
27. A battery fault light will illuminate when:
28. What is the significance of the circuit breakers on the overhead panel?
29. Which flight control computer will be inoperative with gear extension while in the Emergency Electrical Configuration?
30. Which voltage requires recharging or replacing the batteries?
31. If both engine generators are powering the system, and one subsequently fails, are any busses unpowered?
32. On the cockpit overhead panel, there is a three position EMERGENCY EXIT Light switch. What lights are associated with this switch?
33. When does the RAT automatically deploy?
34. How many times can you reset a circuit breaker?
35. If the battery voltages are below the minimum, how do you charge them?
36. After landing, in the emergency electrical configuration: the batteries automatically connect to the DC BAT bus when speed decreases below _______ knots.
37. The engine generators and APU generator are rated at _____ KVA.
38. When no other power is available in flight, the static inverter converts _____ power to AC power for the ______ bus; and ______ powers the _______ bus.
39. With the EMER EXIT LT selector in the ARM position, which situation will activate the emergency lights and exit signs?
40. The BATTERY BUS is normally powered by:
41. If batteries are the only source of power in flight, how long will battery power be available?