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Worksheets

DAY 1 - AGR 2023-2024

Total questions: 25

Worksheet time: 13mins

Name
Class
Date
1.

Is there any limitation on Take Off Configuration with respect to ADR2 fault?

a)

Config 2 is not allowed

b)

Config 1+F not allowed

c)

Non dispatchable

d)

No Auto Brake MAX

2.

Which of the following is/are lost after the ECAM alert ADR 1+2+3 Fault?

a)

Normal L/G extension

b)

Speed and Barometric Altitude

c)

Stall Warning

d)

Both A and B are Correct

3.

What is the FL limitation If there are cracks on cockpit side of the windows/windshield?

a)

FL250

b)

FL230

c)

FL200

d)

FL100

4.

Is case of ADR1+2+3 FAULT, if the BUSS doesn’t react to sidestick input, what should be used as a reference to fly?

a)

Normal Speed Scale

b)

BackUp Speed Scale

c)

Standby Instruments

d)

Pitch Thrust Table

5.

What happens to the rudder travel limiter in case of an NAV ADR 1+2+3 FAULT?

a)

Works Normally

b)

Frozen at the time of failure but full deflection available after slats extension

c)

Permanently inoperative

d)

Limited rudder deflection throughout the flight

6.

After an NAV RA1 and RA2 FAULT ( Dual RA Failure), Why is it necessary to fly raw data during final stages of approach?

a)

AP/FD behaviour may be unsatisfactory

b)

To avoid excessive roll rates

c)

AP gains are no longer updated with the RA signal

d)

All of these are correct

7.

When will APU EMER SHUT DOWN trigger?

a)

APU Fire Pb Pressed

b)

DC Power Loss

c)

ECB failure

d)

EGT Exceedance

8.

How is the refuelling done with the BCL fault?

a)

With the help of APU

b)

With the help of Batteries

c)

With the help of External Power

d)

With the help of Engine Power

9.

Should the APU be turned off if the BCL fault has occurred when the APU is already running?

a)

APU will do an EMER SHUT DOWN

b)

APU should be immediately shut down manually

c)

As the APU is already running no need to turn it off

d)

APU Fire pb has to be pressed

10.

How is the DC ESS BUS powered after encountering ELEC DC EMER CONFIG?

a)

DC BAT

b)

DC 2

c)

Permanently from Battery 1

d)

EmerGen by RAT deployed manually

11.

Is ELAC 2 available after a DC BAT BUS FAULT?

a)

ELAC2 is inoperative throughout flight

b)

ELAC 2 lost after 30 seconds and recovers after L/G extension

c)

ELAC 2 becomes inop but recovers 30 seconds after L/G extension

d)

ELAC 2 is powered by emergen until A/C speed <100 knots

12.

Can you operate both the packs in flight with one Engine Bleed Fault and if wing anti ice is required?

a)

Pack on affected side should be sleected OFF

b)

Both Packs should be selected OFF

c)

Both Packs can be operated

d)

Both Packs can be operated but limited to FL335

13.

Can you recover the engine bleed If both engine bleeds are lost due to Start Air Valve failed open?

a)

Engine bleed recoverable below FL100

b)

Engine bleed recoverable after turning on APU

c)

Engine bleed recoverable after turning on APU and below FL200

d)

Engine Bleed cannot be Recovered

14.

How will AIR PACK 1(2) FAULT have an impact on cabin altitude if the blower and extract are set to OVRD in flight?

a)

The cabin altitude may reach 9700ft

b)

The cabin altitude will not be affected as CPCs will take care

c)

CAB PR EXCESS CAB ALT

may be displayed on E/WD

d)

Both A and C are correct

15.

With PACK 1 or 2 FAULT , Is there any limitations without speedbrakes for 'C' repair interval?

a)

Limited to FL335

b)

Limited to FL230

c)

Limited to FL315

d)

No Limitations

16.

What to do If the hot air valve remains open even after commanding it closed by the pb and duct OVHT persists?

a)

Turn off one of the packs

b)

Turn off both the packs and descend to FL100

c)

Crew awareness no action required

d)

Blower and Extract OVRD

17.

How to confirm the operation of outflow valve with CAB PR SYS 1+2 FAULT?

a)

Use the cabin V/S indication to confirm OFV operation

b)

Do a visual check to confirm OFV operation

c)

Use the OFV position indication to confirm OFV operation

d)

Use the differential pressure indication to confirm OFV operation

18.

How long does it take to notice the change in the OFV position in the SD page during manual OFV operation?

a)

5 seconds

b)

10 seconds

c)

20 seconds

d)

30 seconds

19.

What happens to the blower fan if BLOWER is set to OVRD?

a)

Blower Fan runs at high speed

b)

Blower Fan runs at variable speeds

c)

Blower Fan stops

d)

Extract fan runs are high speed

20.

What happens to the idle speed of the aircraft engines when the EAI valve is open?

a)

Idle RPM reduces

b)

Maximum N1 Increases

c)

Idle RPM increases

d)

No thrust adaption happens

21.

What is the flight control law in case of HYD B+Y SYS LO PR?

a)

Normal Law

b)

ALTN Law with Reduced Protection

c)

ALTN Law without Protection

d)

Direct Law

22.

Is there any system inoperative / limitation on operation of avionics ventilation due to LGCIU2 FAULT ?

a)

The ground cooling system is inoperative

b)

Time limitation on ground for ELEC PWR Supply wrt OAT

c)

Ventilation System is not affected due to LGCIU 2 fault

d)

Both A and B are Correct

23.

When will the L/G GEAR NOT UPLOCKED caution appear?

a)

If the L/G sequence is not completed after 30 s

b)

If the L/G sequence is not completed with immediate selection

c)

If the L/G sequence is not completed after 60 s

d)

If the L/G sequence is not completed after 3 minutes

24.

What happens if you turn on wing Anti ice in flight with both L/G LGCIU 1+2 FAULT?

a)

WAI works normally

b)

WAI will only work for 30s and then becomes inop without ECAM/Aural alert

c)

WAI is inoperative with immediate effect

d)

WAI works only after gravity extension

25.

How many landing gear recycle attempts can be done?

a)

1 time

b)

2 times

c)

4 times

d)

5 times