Systems 2 Review

Question 1

A remote control circuit breaker (RCCB) is a specific kind of circuit breaker

Answer 1

not readily accessible to Pilot or Co-Pilot

Question 2

The LH and RH radio busses are

Answer 2

switch type circuit breaker

Question 3

An electrical bus is a line in either the AC or DC power that

Answer 3

connects electrical components

Question 4

The. power sources for the DC electrical system are

Answer 4

Generators
External Power

Question 5

The main aircraft battery powers

Answer 5

AC and DC busses

Question 6

When the BATTERY switch. is ON and there is no other power on the aircraft, battery power is supplied to

Answer 6

the entire DC electrical system and both inverters

Question 7

The main aircraft battery is locate in the

Answer 7

aft fuselage compartment

Question 8

The output of a fully charged main aircraft battery is

Answer 8

24 Volts DC

Question 9

The T-1A main aircraft batter is a

Answer 9

24 Volt DC Lead Acid Battery

Question 10

Do not attempt a battery start if the main aircraft battery voltage is

Answer 10

below 22 volts DC

Question 11

The external power receptacle is located on the

Answer 11

lower left side of the fuselage and routes 28 volt DC power to the aircraft

Question 12

Generator "In flight" limitations when only one generator is operating are:
up to \_\_\_ feet
\_\_\_ amps
\_\_\_ to \_\_\_ feet
\_\_\_ amps

Answer 12

up to 32,500 feet
400 amps

32,500 to 41,000 feet
280 amps

Question 13

With both engines operating on the ground, what is the maximum allowable load for each generator

Answer 13

280 amps

Question 14

T-1A generators output is

Answer 14

28 volts DC

Question 15

Under normal operations there are how many bus feeders?

Answer 15

2 Bus feeders

powered between Main bus and its associated Load bus

Question 16

The standby power switch light is located

Answer 16

on the Co-Pilots panel

Question 17

That is the location and load for the standby battery is

Answer 17

Nose compartment

24 volt

Question 18

The only communication/navigation system available, when the standby bus is the only bus powered on the aircraft is the

Answer 18

UHF communication radio

Question 19

The standby battery can power the

Answer 19

Standby bus only

Question 20

How do you arm the standby power system

Answer 20

Press the STBY PWR switch light and insure the ARM indicator illuminates

Question 21

Placing the battery switch to the EMER position causes the main aircraft battery to power

Answer 21

the Emergency bus

Question 22

When operating on the standby and emergency buses only, you lose

Answer 22

Normal Landing Gear Extension
Flaps
Speed Brakes

Question 23

With the STBY POWER in ARM on the Standby bus will be powered bu the Master Generator Switches are placed in the

Answer 23

EMER position and the Battery Switch is placed to OFF

Question 24

Location and Positions of the MASTER L GEN and R GEN switches

Answer 24

Overhead board

NORM and EMER

Question 25

Location and Positions of the MASTER L GEN and R GEN switches

Answer 25

Overhead board | NORM and EMER

Question 26

The inverter select switch, located on the main circuit breaker panel has which positions

Answer 26

No. 1 OFF No. 2

Question 27

According to TO 1T-1A-1, the pilot should normally leave the AC voltmeter selector switch in

Answer 27

No. 1 INV | 115 V

Question 28

The No. 2 INVERTER powers the primary AC buses when

Answer 28

the inverter selector is in the No. 2 Position

Question 29

The NO. 1 INVERTER receives power from

Answer 29

the LH Load Bus

Question 30

The RH LOAD BUS normally powers

Answer 30

the No. 2 Inverter

Question 31

If the AC BUS SHED annunciator on the copilot's shroud panel is illuminated

Answer 31

the AC shed buses are depowered

Question 32

Each inverter converts DC power into

Answer 32

25 and 115 volts AC

Question 33

Each inverter converts DC power into

Answer 33

25 and 115 volts AC

Question 34

Indications of left generator failure: MASTER CAUTION RESET switch lights flash and

Answer 34

``` L GEN OFF annunciator illuminates LH AMPS read zero RH AMPS read higher LH VOLTS read zero RH COLTS read normal No Loss of electrical equipment ```

Question 35

If the. NO. 1 INVERTER fails and the distribution circuits are functioning properly

Answer 35

the No. 2 INVERTER powers the Primary AC Buses and Secondary AC Buses depower

Question 36

If you've experienced a single inverter failure, set the inverter voltage select knob to

Answer 36

115 Volt position for the inverter that is powering the Primary bus

Question 37

If the MASTER CAUTION RESET switch lights flash and the INV 2 FAIL annunciator illuminates, check the

Answer 37

Inverter and Inverter control circuit breakers for the No. 2 INVERTER

Question 38

The NO 1 INVERTER has failed. The AC BUS SHED annunciator (on copilot's shroud panel) illuminates when the

Answer 38

NO 2 INVERTER is powered by the EMER bus and is providing power to the Primary buses

Question 39

BAT CUT OFF annunciator indicates the

Answer 39

Battery relay is open and battery charging will not occur

Question 40

You notice an illuminated BATTERY FDR FAIL light on the overhead panel and there are no other indications. Per Section III, you turn the

Answer 40

Battery OFF. | Battery charging will not occur.

Question 41

The EMER BUS FDR FAIL annunciator light illuminates and the EMER BUS FDR circuit breaker open, the

Answer 41

The Emergency bus is powered by the left load bus

Question 42

A secondary indication of failure of the emergency bus feeder circuit is

Answer 42

an open EMER BUS FDR