SYS108

Question 1

During normal operation, while the bus tie is closed, which electrical buses does the generator supply?

Answer 1

Both the generator bus and battery bus

Question 2

The GCU is located under a side panel in which cockpit?

Answer 2

The rear cockpit under a panel on the right side of the cockpit

Question 3

Generator and battery buses are tied together through which switch?

Answer 3

The bus tie switch

Question 4

Power for aircraft avionics is supplied by which bus?

Answer 4

Both the generator and battery bus

Question 5

Battery bus circuit breakers are located on which side of the cockpit?

Answer 5

The left side of the aircraft

Question 6

Control of battery power is transferable between cockpits using what?

Answer 6

The battery switch

Question 7

True or false? The auxiliary battery will activate automatically upon failure of the primary battery.

Answer 7

False, it is manually activated.

Question 8

The landing and taxi lights are activated by the LDG and TAXI switches when the gear is __________.

Answer 8

down and locked

Question 9

The navigation lights at the leading edge wingtips are what colors?

Answer 9

Left-Red, Right-Green

Question 10

Using single point refueling, the T-6A’s maximum usable fuel is how many pounds?

Answer 10

1100 lb

Question 11

Which refueling method allows more fuel to be pumped into the wing tanks?

Answer 11

over the wing gravity refueling

Question 12

The primary jet pump and transfer jet pumps are operated by what means?

Answer 12

Venturi flow

Question 13

Data from the fuel flow transmitter is displayed on what instrument?

Answer 13

AEDD

Question 14

AEDD fuel quantity indications are derived from how many sensors in the fuel tanks?

Answer 14

7- 3 per wing, 1 in collector tank

Question 15

What is indicated if the M FUEL BAL annunciator is lighted?

Answer 15

That the fuel balance switch is in MAN/RESET

Question 16

True or false? The weight of fuel in the collector tank is included in the total fuel weight on the AEDD.

Answer 16

True

Question 17

Which component prevents fuel from draining from the wing tank?

Answer 17

Float valves at the tip of each tank

Question 18

If tank loads are out of balance, the auto balance system stops motive flow to which tank?

Answer 18

The lighter tank.

Question 19

The FUEL BAL annunciator will illuminate if the fuel weight difference between the left and right tanks exceeds what figure for more than 2 minutes?

Answer 19

30 lb

Question 20

The BOOST PUMP annunciator is cycling on and off. This could be an indication of what?

Answer 20

Low fuel pressure (<10 psi)

Question 21

The generator supplies what voltage to the generator and battery buses?

Answer 21

28 VDC

Question 22

The anti-collision strobe lights are located where?

Answer 22

On the leading edge,on the wingtips

Question 23

External power is distributed on which bus?

Answer 23

The battery bus

Question 24

Gravity refueling adds how many total pounds to the T-6A normal capacity?

Answer 24

100 lb

Question 25

Generator bus circuit breakers are located on which side of the aircraft?

Answer 25

The right side

Question 26

True or False? Single-point refueling fills all three tanks sequentially beginning with the collector tank.

Answer 26

False- they are filled simultaneously

Question 27

The control for which shutoff valve is located in the cockpit?

Answer 27

The firewall shutoff handle

Question 28

Which electrical component provides power for engine starts?

Answer 28

The primary battery.