Systems 1

Question 1

The annunciators on the shroud panel are designed to _______

Answer 1

Get the attention of the crew

Question 2

The MASTER TEST switch and GO/NOGO annunciators ________

Answer 2

Check the status of eight different systems

Question 3

Aural Warnings consist of _______

Answer 3

Tones, horns and voice messages

Question 4

What can you reference in T.O. T1-1A to determine the meaning of an annunciator on the main annunciator panel?

Answer 4

Section III, Figures 3-12 and 3-13

Question 5

Who is responsible for handling emergencies on the T-1?

Answer 5

The entire crew

Question 6

What does it mean when the L F/V CLOSE switchlight on the shroud panel is illuminated amber?

Answer 6

The left fuel valve is closed and no fuel is flowing to the left engine.

Question 7

If the amber L GEN OFF annunciator on the main annunciator panel illuminates, what flashes?

Answer 7

The two MASTER CAUTION RESET switchlights

Question 8

Bypass Air _______

Answer 8

Helps cool the core of the engine

Question 9

The low compressor _______

Answer 9

Is driven by a two-stage turbine

Question 10

ITT probes are located _______

Answer 10

Between the core and fan turbine

Question 11

The fan is connected to the low compressor turbine by a

Answer 11

Shaft running through the center of the hollow impeller shaft

Question 12

The performance of the core engine is measure by _____

Answer 12

The N2 gauge

Question 13

During engine start, ITT should not exceed ______ °C

Answer 13

550

Question 14

If the ITT is between 550°C and ______°C for less than 4 seconds, you can try to start again.

Answer 14

600

Question 15

Where are the navigation lights installed on the T-1A?

Answer 15

In each wingtip, as well as the top of the vertical stabilizer trailing edge.

Question 16

What would you do to extend and illuminate the landing lights following an automatic retraction?

Answer 16

Recycle the landing light switches from the EXT/ON to RET/OFF and back to EXT/ON

Question 17

Upon initially arriving at the aircraft, you want to turn on some interior lights. What lights illuminate if you push the ROOM LIGHT switch?

Answer 17

Two general area flood lights in the cabin area

Question 18

How do you illuminate circuit breaker panels?

Answer 18

Push the C/B LT pushbutton switch on the aft circuit breaker panel.

Question 19

The anti-collision strobe lights are

Answer 19

White and located in each wingtip and and the aft most point of the fuselage

Question 20

The wing inspection lights

Answer 20

Are an aid for checking ice formation

Question 21

If the landing light switches are set to the EXT/ON position, what will happen when you retract the landing gear?

Answer 21

The landing lights will automatically retract and extinguish.

Question 22

During night ops, how should you set the cabin lights?

Answer 22

At a level to reduce glare on the flight deck.

Question 23

The emergency lighting system is controlled by ________

Answer 23

A guarded switch on the overhead control panel

Question 24

If the INTEG switch is on, what will happen if the L LOAD BUS fails?

Answer 24

The panel flood lights will illuminate

Question 25

With primary power available to all busses, what normally powers the standby bus?

Answer 25

Left Load Bus

Question 26

Where is the standby battery located?

Answer 26

Nose compartment

Question 27

With the battery bus in EMER position, the main aircraft battery powers the __________

Answer 27

Emergency Bus

Question 28

The STBY PWR switchlight ON indication illuminates amber when _________

Answer 28

The standby bus is being powered by the standby battery

Question 29

``` Which of the following is powered by the standby bus? EADI #1 Left and Right fuel flow gauges RTU #1 Left N1 guage ```

Answer 29

RTU #1

Question 30

When operating with only emergency and standby buses, what will not be available?

Answer 30

Normal pitch trim

Question 31

The standby batter provides

Answer 31

24-volt DC power

Question 32

Under normal operating conditions (both generators online and the battery switch set to ON), what is the source of power for the emergency bus?

Answer 32

Generator power through the emergency bus power feed line.

Question 33

To arm the standby battery,

Answer 33

Press the standby power switch light

Question 34

When operating with only emergency and standby electrical power, the crew can lower the landing gear using normal procedures.

Answer 34

False

Question 35

The two inverters produce what kind of power?

Answer 35

26 and 115-volt AC power

Question 36

From which source does the NO. 2 inverter normally receive power?

Answer 36

Right load bus

Question 37

Each inverter regulates its own voltage and frequency output.

Answer 37

True

Question 38

An illuminated AC BUS SHED annunciator on the pilot's shroud panel indicates ________

Answer 38

The AC shed buses are de-energized

Question 39

The AC voltmeter ______

Answer 39

Displays the voltage of one of four sources of AC power as selected by the AC voltmeter selector switch

Question 40

The NO. 1 inverter usually receives power from what source?

Answer 40

LH Load Bus

Question 41

With both load buses powered and the inverter selector switch set to to AUTO, a failure of the NO. 1 inverter causes _________

Answer 41

the NO. 2 inverter to power the primary AC buses and the AC shed buses.

Question 42

If the RH LOAD BUS loses power, the NO. 2 inverter can be powered by the ________

Answer 42

Emergency bus

Question 43

What are the power sources of the T-1A DC electrical system?

Answer 43

Battery, generators and external power unit

Question 44

What kind of power/battery does the T-1A have?

Answer 44

24-volt DC lead-acid, located in the aft fuselage compartment.

Question 45

What kind of power is produced by the T-1A starter generators?

Answer 45

28-volt DC power

Question 46

T or F: The main aircraft battery is capable of providing power to all DC buses

Answer 46

True

Question 47

Illumination of the L BUS FDR FAIL annunciator indicates that the _______

Answer 47

Standby feeder on the left side is active

Question 48

What happens if both master generator switches are moved to EMER?

Answer 48

Both generators are isolated from their main buses.

Question 49

While performing a GPU assisted start, the generator RESET switches should be in the ________ position

Answer 49

OFF

Question 50

While performing a battery start, the generator RESET switches should be in the ________ position

Answer 50

AUTO

Question 51

Do not perform a battery start if the battery voltage is below ________

Answer 51

22 volts DC

Question 52

What is max generator load if one generator is operating at FL270?

Answer 52

400 amps

Question 53

What is the max generator load if one generator is operating above FL325 or on the ground?

Answer 53

280 amps

Question 54

What is the primary source of DC power while in flight?

Answer 54

28-volt generators

Question 55

Under normal operating conditions, how many feeders carry power from each main bus to its corresponding load bus?

Answer 55

Two feeders

Question 56

During engine start, the GCU removes power from the starter when the engine reaches approx ______ %N2

Answer 56

35-40

Question 57

If the right generator fails in flight, what is the impact on the electrical system?

Answer 57

No buses loses power.

Question 58

The fuselage fuel indicator measures

Answer 58

The total fuel remaining in the fuselage tanks

Question 59

Fuel is fed directly to the engines from the

Answer 59

Fuel feed chambers

Question 60

During fuel crossfeed, fuel flow from the engines is supplemented by _______

Answer 60

A boost pump

Question 61

The primary jet pumps are driven by

Answer 61

Motive flow

Question 62

Where are the remote control circuit breakers located? (RCCB)

Answer 62

Aft fuselage compartment

Question 63

What is the normal position for the inverter selector switch?

Answer 63

AUTO

Question 64

The No. 1 inverter is supplied 28-volt DC electrical power from the LEFT LOAD BUS.

Answer 64

True

Question 65

The AC voltmeter is located where?

Answer 65

The aft circuit breaker panel