Test 1 - New Hire CBT Validation Test

Question 1

How is an IDG reconnected?

Answer 1

D. On the ground by maintenance

Question 2

Which of the following items are powered by the main AC buses?

Answer 2

• Flight instrument transfer buses
• Transformer Rectifier Units
• Utility and Galley buses

Question 3

The ground service bus can be powered on the ground and in flight? (T/F)

Answer 3

True

Question 4

Which buses can be powered by the Standby power system?

Answer 4

-Standby AC and DC buses
-Battery bus
-Hot Battery Bus

Question 5

When are the Engine Fire/Overheat and APU Fire Detection Loops monitored for faults?

Answer 5

Continuously

Question 6

During normal operation, both engine fire detector loops must detect a fire or overheat condition to activate a fire warning or overheat caution? (T/F)

Answer 6

True

Question 7

When a fault is detected in one of the APU fire detector loops, the system does what?

Answer 7

-Automatically reconfigures for single detector operations

Question 8

What occurs when an engine fire switch is pulled?

Answer 8

-The engine and spar fuel valves are closed
-The fire warning bell is silenced
-The engine generator breaker opens

Question 9

How is air drawn into the smoke detector from the cargo compartment?

Answer 9

-By fans dedicated for that purpose

Question 10

What is the primary function of the rudder ratio system?

Answer 10

-To limit rudder authority at high speeds while providing full rudder authority at low speeds

Question 11

How is electric stabilizer trim affected when a STAB TRIM light on the overhead panel is illuminated?

Answer 11

-Trim is one-half the normal rate

Question 12

What is cut off by the STAB TRIM CUTOUT switches?

Answer 12

-Hydraulic power for stabilizer trim

Question 13

What moves the flaps and slats when using the Alternate Flap and Slat system?

Answer 13

b.
 Electric motors

Question 14

During a trailing edge flap asymmetry, power to the slats is removed? (T/F)

Answer 14

FALSE

Question 15

The pitch enhancement system (PES) supplies power to?

Answer 15

Stabilizer Trim

Question 16

The normal brake system is powered by which hydraulic system?

Answer 16

(RIGHT) SYSTEM

Question 17

Which of the following systems are available with the normal brake system?

Answer 17

ALL OF ANSWERS
-Parking brake

-Brake accumulator

-Anti-skid protection to each wheel individually

-Auto brake

Question 18

What action(s), if any, must the flight crew accomplish for the alternate brake system to become active?

Answer 18

No action is required since it automatically occurs

Question 19

What does an illuminated amber GEAR light indicate?

Answer 19

Any or all of the landing gear position(s) disagree with the gear lever position

Question 20

A BRAKE SOURCE annunciator and EICAS message indicate?

Answer 20

No hydraulic pressure is available for normal or alternate brakes

Question 21

Which statements) is/are correct about the APU?
(Select all Correct Answers)

Answer 21

-The APU provides air for engine starts
-The APU provides air for pneumatics up to an altitude of approximately 17,000 feet

Question 22

Which pump supplies fuel to the APU with the APU generator powering the aircraft?

Answer 22

Left forward boost pump

Question 23

When the APU gets a signal for a protective shutdown, the APU will?

Answer 23

• Immediately shutdown without a normal cooling cycle

Question 24

Which valve prevents cabin pressure from dropping significantly below ambient pressure?

Answer 24

Negative Pressure relief Valve

Question 25

The index mark on the auto rate selector represents a cabin altitude change of?

Answer 25

500 fpm climb and 300 fpm descending

Question 26

Which motors position the outflow valve in auto and manual modes?

Answer 26

The Auto modes use separate AC motors, and the Manual mode uses a DC motor

Question 27

If the message CABIN AUTO INOP appears on the upper EICAS panel, what condition is indicated?

Answer 27

AUTO 1 and AUTO 2 cabin altitude controllers are INOP or MAN mode is selected

Question 28

How are the engine and wing anti-ice valves controlled and operated?

Answer 28

Electrically controlled and Pneumatically operated

Question 29

Electric window heat provides anti-ice and anti-fog protection for flight deck windows.
 Which windows receive anti-ice protection?

Answer 29

CA and FO #1

Question 30

What will the EEC do if either wing or engine anti-ice is selected ON?

Answer 30

-REDUCE maximum N1limits

Question 31

A display of active flight control modes can be found?

Answer 31

On the Flight Mode Annunciators

Question 32

What is the source for the primary heading signals for the First Officer's RDMI?

Answer 32

-The left IRS

Question 33

If the Captain's EFl switch is selected to ALTN, which statement is TRUE?

Answer 33

The Captain's displays are driven by the center symbol generator

Question 34

A CDU entry field where data input is mandatory is indicated by?

Answer 34

Empty Boxes

Question 35

If a waypoint is entered into the LEGS page that shares a name with another waypoint, the FMC will?

Answer 35

Prompt the crew to select the desired waypoint

Question 36

Where can you check the oxygen pressure while on the flight deck?

Answer 36

EICAS STATUS page

Question 37

At what cabin altitude will the passenger oxygen masks deploy automatically?

Answer 37

14,000 feet MSL

Question 38

How is engine bleed air prevented from back flowing into the APU during engine start?

Answer 38

By the APU check valve, and the APU bleed valve automatically closing

Question 39

The upper EICAS displays the following engine indications?

Answer 39

N1, EGT

Question 40

What indications on the N1 gauge show LIMIT N1?

Answer 40

Amber Line

Question 41

During a normal engine start, the engine start switch is magnetically held in the GND position until?

Answer 41

50% N2

Question 42

The FUEL CONTROL switches control which valves?

Answer 42

The engine fuel and spar valves

Question 43

Hydraulic reservoirs are pressurized by?

Answer 43

Bleed Air

Question 44

Which statement is true regarding the ram air turbine?

Answer 44

It deploys automatically when both engines fail, in order to provide hydraulic power to the center system flight controls