Day 14 - All Previous Topics

Question 1

State the four purposes of the boost pumps

Answer 1

Engine start, backup for primary jet pumps, source of pressure for transfer pumps, crossfeed

Question 2

In the automatic mode, the boost pump will operate when

Answer 2

Fuel feed line pressure drops below 5 psi, fuel feed chamber falls below 11 gallons, engine starting is selected, crossfeed is selected

Question 3

Where are the electric transfer pumps located and what do they do

Answer 3

In each mid tank, transfer fuel to wing tanks

Question 4

How is fuel transferred through the jet pumps

Answer 4

Motive flow

Question 5

If the fuel indicators fail, they will display

Answer 5

Below zero

Question 6

What are the three electrical power systems of the T-1

Answer 6

Primary direct current (DC), alternating current (AC), and DC standby current

Question 7

What are the three primary DC power components

Answer 7

Starter generators, battery, and external power

Question 8

The generators power their respective load buses though __

Answer 8

The main buses

Question 9

What type of battery is in the T-1

Answer 9

24 volt, 40 ampere-hour lead acid

Question 10

What does the BATT FDR FAIL light indicate

Answer 10

Battery feeder protection is lost

Question 11

What does the BATT FDR FAIL light accompanied by EMER BUS FDR FAIL annunciator indicate

Answer 11

Emergency bus is being powered by the LH load bus

Question 12

What does the BATT FDR FAIL light accompanied by EMER BUS FDR FAIL and BATT CUTOFF annunciators indicate

Answer 12

Ground fault has occurred and battery feeder protection unit has disconnected the battery

Question 13

T/F - Ground fault protection is provided by the battery protection circuits

Answer 13

TRUE

Question 14

The standby battery provides power to

Answer 14

Standby attitude indicator, UHF radio, RTU#1, No.1 ITT indicator, electronic fuel control - start, copilot instrument

Question 15

T/F - If the STBY PWR is not armed during preflight, the standby bus will not automatically be powered with the loss of all electrical power

Answer 15

TRUE

Question 16

The AC power system is powered by __ located in the __

Answer 16

Two inverters, nose compartment

Question 17

With the inverter select switch to AUTO how is AC power distributed

Answer 17

The No.1 inverter powers the primary and the No.2 powers the secondary buses by default

Question 18

With the inverter select switch to NO.1 how is AC power distributed

Answer 18

It forces the No.1 inverter to power the primary buses

Question 19

With the inverter select switch to NO.2 how is AC power distributed

Answer 19

No.2 powers the primary AC buses and No.1 powers the secondary AC buses

Question 20

What causes the AC BUS SHED annunciator to illuminate

Answer 20

No.2 inverter is being powered by the emergency bus and the No.1 inverter is failed

Question 21

While operating on emergency and/or standby power what hydraulic systems will be inoperative

Answer 21

Normal landing gear extension, flaps, speed brakes, anti-skid

Question 22

The T-1 hydraulic system controls

Answer 22

Flaps, landing gear, speed brakes, and normal braking

Question 23

What types of hydraulic pumps are utilized in the T-1

Answer 23

Variable displacement, rotary plunger type pumps

Question 24

The hydraulic pumps delivery and pressure varies from __ gpm at __ psi to __ gpm at __ psi

Answer 24

0, 1500, 3.9, 1400