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3 ATAs 27 - 29 - 32 A319/A320 /A32

Total questions: 25

Worksheet time: 13mins

Name
Class
Date
1.

FLIGHT CONTROLS – ATA 27. Mark only one oval. Which surfaces are primarily used for pitch control on the A320?

a)

Rudder and ailerons

b)

Two elevators and the Trimmable Horizontal Stabilizer (THS)

c)

Spoilers and flaps

2.

FLIGHT CONTROLS – ATA 27. Mark only one oval. How is roll control achieved in normal operation?

a)

By one aileron and spoilers 2 to 5 on each wing

b)

By elevators only

c)

By rudder and spoilers 1 to 3

3.

FLIGHT CONTROLS – ATA 27. Mark only one oval. Which computers normally control the ailerons?

a)

SEC 1 and SEC 2

b)

ELAC 1 (main) with ELAC 2 as backup

c)

FAC 1 and FAC 2

4.

FLIGHT CONTROLS – ATA 27. Mark only one oval. What is the main function of the Flight Augmentation Computers (FACs)?

a)

Slat and flap control

b)

Pitch trim control

c)

Yaw control and yaw damping

5.

FLIGHT CONTROLS – ATA 27. Mark only one oval. How many hydraulic actuators power the rudder?

a)

One

b)

Two

c)

Three

6.

FLIGHT CONTROLS – ATA 27. Mark only one oval. What happens if both ELACs fail for roll control?

a)

Only ailerons remain available

b)

Roll control is lost completely

c)

Only spoilers are available in direct law

7.

FLIGHT CONTROLS – ATA 27. Mark only one oval. The FLT CTL surfaces used to destroy the lift during landing and in case of rejected takeoff are:

a)

The Ground Spoilers 1 to 5

b)

The SLATS 3, 4, and 5

c)

The Speed Brakes 2, 3, and 4

8.

FLIGHT CONTROLS – ATA 27. Mark only one oval. What is the purpose of the Pressure-Off Brake (POB) in the slat/flap system?

a)

To increase flap extension speed

b)

To lock the transmission when the selected position is reached

c)

To synchronize left and right flaps

9.

HYDRAULIC SYSTEM – ATA 29. Mark only one oval. If the EDP #1 in the Green Hydraulic system is inoperative:

a)

The Green Hydraulic System is lost

b)

The PTU pressurizes the Green Hydraulic System

c)

You can pressurize it by Leak Measurement Valves operation

10.

HYDRAULIC SYSTEM – ATA 29. Mark only one oval. When is the RAT deployed automatically?

a)

In case of an electrical emergency, loss of main AC busses 1 and 2 and airspeed greater than 100 kts

b)

In case of a hydraulic system failure, more than two systems lost

c)

At any moment, when the pilot pushes the push button located on the hydraulic or electrical control panel

11.

HYDRAULIC SYSTEM – ATA 29. Mark only one oval. Can you pressurize the Blue Hydraulic system on ground with engines stopped?

a)

Yes, by the PTU

b)

Yes, by the Blue Pump Override pushbutton (50VU)

c)

Yes, by the RAT

12.

HYDRAULIC SYSTEM – ATA 29. Mark only one oval. When the pushbutton of any EDP is pushed to OFF position:

a)

The pump is disconnected from the engine

b)

Solenoid valve in the EDP is energized, and the pump runs in depressurized mode

c)

Solenoid valve is de-energized, hydraulic supply to the pump is shut

13.

HYDRAULIC SYSTEM – ATA 29. Mark only one oval. From where can you perform the Yellow Hydraulic fluid servicing?

a)

Yellow Ground Service Panel

b)

Blue Ground Service Panel

c)

Green Ground Service Panel

14.

From where can you perform the blue Hydraulic fluid servicing? Select only one option.

a)

Yellow Ground Service Panel.

b)

Blue Ground Service Panel.

c)

Green Ground Service Panel.

15.

What is the main function of the Power Transfer Unit (PTU)? Select only one option.

a)

Transfer hydraulic fluid between systems.

b)

Provide electrical power in emergency.

c)

Transfer hydraulic power without transferring fluid.

16.

The RAT Retraction Module is installed on: Select only one option.

a)

The Green Servicing Panel.

b)

The Yellow Servicing Panel.

c)

The Blue Servicing Panel.

17.

Which computers control the landing gear and door sequencing? Select only one option.

a)

BSCU 1 and 2.

b)

LGCIU 1 and 2.

c)

FAC 1 and 2.

18.

LGCIU's. When does the control changeover occur? Select only one option.

a)

Never, because LGCIU #1 always has priority over LGCIU #2.

b)

When the landing gear lever goes UP.

c)

When the landing gear lever goes DOWN.

19.

What system provides normal braking? Select only one option.

a)

Yellow hydraulic system.

b)

Green hydraulic system.

c)

Blue hydraulic system.

20.

In the Landing Gear System, what is the normal position for the SAFETY VALVE above 260 kts (high speed)? Select only one option.

a)

Open.

b)

Closed.

c)

Standby.

21.

What component sends brake temperature data to the BSCU? Select only one option.

a)

TPIC.

b)

BTMU.

c)

ABCU.

22.

Which computer provides Autobrake function & anti-skid protection? Select only one option.

a)

Brake Steering Control Unit (BSCU).

b)

Alternate Braking Control Unit (ABCU).

c)

LGCIU's.

23.

After FREE FALL Extension, the L/G Doors stay: Select only one option.

a)

OPEN.

b)

THEIR LAST POSITION.

c)

CLOSED.

24.

What is the function of the BTMU? Select only one option.

a)

Control brake pressure.

b)

Monitor tire pressure.

c)

Transmit brake temperature to the BSCU.

25.

What is the maximum steering angle using the rudder pedals? Select only one option.

a)

6°.

b)

30°.

c)

74°.