1. What is the primary electrical power, volts, phase, hertz and current
2. What converts variable input speed from the engine accessory pad to a constant RPM output to the generator.
3. AC power to the airplane may be supplied by the engine driven generators and what other sources.
4. CSD oil cooler efficiency is determined by observing what.
5.  To prevent the disconnected generator from being motorized by paralleled generators the disconnect switch also trips what.
6. The voltage regulator adjusts what to control the voltage output of an isolated generator
7. To reduce the output of a generator to a minimum. What would you trip.
8. What connects a generator to it's load bus
9. To equalize the loads on the generators. The load busses are connected together by what
10.  Damage to the generators might occur if they are not what
11. In order for a generator to be able to supply essential power. its what must be closed
12. The standby bus can be powered from the essential bus or by what other means.
13. The AC transfer bus can be powered from what two sources
14. If residual voltage is 10 to 17 volts, you know the generator is doing what.
15.  If the synch lights are out. The generator selected is in what with the synch bus.
16. Normal DC power is supplied by what
17. The battery charger receives power from the bus
18. If  TR 1 fails.  DC bus number 1 will be powered by
19. Failure of a TR is indicated by what, indicating zero
20.  The battery bus is normally powered by What
21. With the airplane not powered, What will be powered from the Battery
22. In flight normally the hot battery bus is powered by what
23. What two sources can power the battery transfer bus
24. What illuminates with the loss of essential power
25.  When paralleling manually, the bus tie breaker should be closed when the synch lights are
26. If all generators are lost while on the ground, the battery switch should be checked on and what  should be turned on/opened 
    Answer the following as True or False
27. In order to check the battery, power to the battery charger should be interrupted.
28. When the APU generator breaker is closed, the bus tie breakers should remain open
29.  The CSD disconnect switches should be selected to DISCONNECT to check their operation during flight.
30. Prior to engine start the electrical load should be reduced
31. Immediately after engine start. When the first engine driven generator is connected and the APU generator drops off line, essential power will be lost
    Abnormal & Emergency  Procedures
32. If all generators are lost in flight. The first action to be taken is to
33. When can the generator drive be reconnected
34. For landing with only two generators operating how many packs on
35. One generator inoperative when should you turn on the 2nd pack
36. With only one generator operating before flap extension do what.

ANSWERS

1. 115 Volts, 3 Phase, 400 Hz, AC
2. CSD (Constant Speed Drive)
3. APU and External Power
4. "IN" Temperature
5. Trips the Generator Breaker
6. Excitation Current
7. Field Relay
8. Generator Breaker
9. Sync Bus (tie bus)
10. In Phase
11. Field Relay
12. Inverter, Battery Bus
13. No3 Ac Load Bus or External Power
14. Rotating
15. In Phase
16. Transformer - Rectifier (TR's)
17. AC Transfer Bus
18. No2 TR
19. DC Amps Indicator
20. Essential DC Bus
21. Hot Battery Bus, Hot Battery Transfer Bus
22. Battery, Battery Charger
23. Battery Bus, External DC Bus (External power)
24. Red Steady Light At FE Panel, Flashing Red at Fwd Instrument Panel
25. Out
26. Brake Interconnect
27. True, Yes you need to
28. False
29. False, If you did your a dickhead can only be reset on the ground
30. True, Loads Reduced To Minimum
31. False, Will Only be affected If you Trip The APU Field Relay
32. Essential Power Selector, Standby
33. On The Ground
34. One
35. After Flap Retraction and the Pack Fans Are Off
36. Turn Off Both Packs, Depressurize