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3 Flashcards

1
Q

At the start of the flight, what will be the condition of ATHR?

◦ A. ACTIVE at 1500 feet AAL.
◦ B. ACTIVE on selection of TOGA or FLX power.
◦ C. ARMED on selection of TOGA or FLX power.
◦ D. ARMED at 80 kts

A

C. ARMED on selection of TOGA or FLX power.

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2
Q

When is the FUEL USED indication (on the SD) reset to zero?

◦ A. When the associated MASTER SW is selected OFF (on ground only).
◦ B. When the associated MASTER SW is selected OFF (at any time).
◦ C. During associated engine start.
◦ D. Five minutes after engine shutdown on the ground.

A

◦ C. During associated engine start.

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3
Q

Regarding an Auto Start, which of the following is a correct statement?

◦ A. Loss of the N2 grey background signifies start valve closure.
◦ B. Engine No.2 normally uses igniter B.
◦ C. Loss of the N2 grey background signifies end of the start sequence.
◦ D. Putting the MODE SEL to START closes the bleed valve

A

C. Loss of the N2 grey background signifies end of the start sequence.

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4
Q

Which of the following indications may be ignored?

◦ A. Amber EGT during take-off.
◦ B. Red EGT during take-off.
◦ C. Amber N1 during take-off.
◦ D. Amber N2 during take-off

A

A. Amber EGT during take-off.

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5
Q

Regarding FADEC, which of the following statements is true?

◦ A. It can be energised on ground by putting ENG MODE SEL to START.
◦ B. Each FADEC has three channels.
◦ C. The FADEC is able to abort a MANUAL START.
◦ D. FADEC runs for 10 minutes after the aircraft is electrically powered-up.

A

A. It can be energised on ground by putting ENG MODE SEL to START.

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6
Q

. In flight, how is the crew advised that the engines are spooled-down?

◦ A. “ADVISORY” displayed on the ENG. S.D.
◦ B. Aural alert “ SPEED, SPEED, SPEED”.
◦ C. Master Caution and Single chime.
◦ D. “IDLE” displayed between the LP rotor speed (N1) gauges.

A

D. “IDLE” displayed between the LP rotor speed (N1) gauges.

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6
Q

After Take-Off, when does the ATHR become ACTIVE?

◦ A. 1500 feet above airfield elevation.
◦ B. 1500 feet R.A.
◦ C. Thrust Reduction altitude.
◦ D. Acceleration Altitude.

A

C. Thrust Reduction altitude.

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7
Q

During a manual start, what does the MAN START pushbutton do?

◦ A. It controls the FUEL VALVE.
◦ B. It controls the START VALVE and the FUEL VALVES.
◦ C. It opens the start valve and must be selected OFF to close the start valve.
◦ D. It opens the start valve: the start valve will close automatically.

A

D. It opens the start valve: the start valve will close automatically.

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8
Q

On the approach to land, what automatically activates the igniters?

◦ A. Selecting Config.1.
◦ B. Selecting Gear Down.
◦ C. Passing 2500’ R.A.
◦ D. Selecting Config.2 from Config. 1

A

A. Selecting Config.1.

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9
Q

How is an imminent change of trust highlighted?

◦ A. A pulsing EPR gauge.
◦ B. TLA movements on the N1 gauge.
◦ C. A blue arc on the N1 gauge.
◦ D. A magenta arc on the N1 gauge

A

C. A blue arc on the N1 gauge.

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10
Q

Regarding an AUTO START, which of the following is correct statement?

◦ A. Putting the Master Switch ON starts IGN immediately.
◦ B. The start sequence ends at 40% N2.
◦ C. If the start is aborted, the pilot must select CRANK on the mode selector.
◦ D. Igniter operation alternates A/B at each start

A

◦ D. Igniter operation alternates A/B at each start

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11
Q

What does FADEC do if there is no ignition during an automatic start cycle?

◦ A. Show an ECAM message : the crew must perform a dry crank.
◦ B. If no EGT after 30 seconds, it will activate the other igniter.
◦ C. Abort the start, then attempt another start using the other igniter.
◦ D. Abort the start and perform a dry crank

A

D. Abort the start and perform a dry crank

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12
Q

What is the maximum demonstrated crosswind for take-off.

◦ A. 29 (gusting 38) knots. - REVIEWER
 38 kt (gust included) - CFM 2014
◦ B. 33 (gusting 38) knots.
◦ C. 29 (gusting 33) knots.
◦ D. 34 knots.
A 
A. 29 (gusting 38) knots. - REVIEWER
 38 kt (gust included) - CFM 2014
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13
Q

What is the maximum wind speed for door operation?

◦ A. 70 knots.
◦ B. 65 knots.
◦ C. 55 knots(gusting 60 knots).
◦ D. 52 knots.

A

B. 65 knots.

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14
Q

. What is the limiting speed for selecting the gear down (VLE)?

◦ A. 220 kt.
◦ B. 250 kt.
◦ C. 260 kt.
◦ D. Green Dot

A

B. 250 kt.

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15
Q

What is the maximum runway slope?

◦ A. +/-1%
◦ B. +1% / -2%
◦ C. +/-2%
◦ D. +2% / -1%

A

C. +/-2%

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16
Q

What are the maximum acceleration (G) limits?

◦ A. Slats extended and flaps retracted, 0g to +2g.
◦ B. Slats and flaps extended, 0g to 2.5g.
◦ C. Clean -1g to +2.5g and flaps extended -1g to +2g.
◦ D. Clean, and slats extended, -1g to +2.5g.

A

A. Slats extended and flaps retracted, 0g to +2g.

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17
Q

What are the Power Plant Starter limitations?

◦ A. The maximum speed for starter engagement is 20% N1.
◦ B. The maximum speed for starter engagement is 30% N2.
◦ C. After 3 failed start attempts, maintenance action is necessary.
◦ D. Cooling period, after 4 start attempts: 15 min

A

D. Cooling period, after 4 start attempts: 15 min

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18
Q

What is the minimum speed for use of full reverse thrust?

◦ A. 50 kt.
◦ B. 60 kt.
◦ C. 70 kt.
◦ D. 75 kt

A

C. 70 kt.

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19
Q

What is the maximum speed for FLAP 3?

◦ A. 177 kts.
◦ B. 185 kts.
◦ C. 200 kts.
◦ D. 205 kts

A

B. 185 kts.

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20
Q

What is the maximum cabin pressure differential?

◦ A. Positive 8.4 psi., Negative 1.0 psi.
◦ B. Positive 8.6 psi., Negative 1.2 psi.
◦ C. Positive 8.5 psi., Negative 0.4 psi.
◦ D. Positive 9 psi., Negative 1.0 psi.

A

D. Positive 9 psi., Negative 1.0 psi.

21
Q

What is the limiting factor for opening the Ram Air Valve?

◦ A. Aircraft altitude at or below 10,000 ft.
◦ B. Cabin differential pressure at or below 1 psi.
◦ C. Aircraft must be on ground.
◦ D. Aircraft must be fully depressurised

A

B. Cabin differential pressure at or below 1 psi.

22
Q

What is the maximum EPR with the park brake ON?

◦ A. 1.05
◦ B. 1.15
◦ C. 1.18
◦ D. 1.25

A

C. 1.18

23
Q

What is the maximum demonstrated crosswind for landing?

◦ A. 33 (Gusting 38) knots. - REVIEWER
 38 kt (gust included) - CFM 2014
◦ B. 33 (Gusting 37) knots.
◦ C. 29 (Gusting 33) knots.
◦ D. 34 (Gusting 33) knots
A 
A. 33 (Gusting 38) knots. - REVIEWER
 38 kt (gust included) - CFM 2014
24
Q

What is the maximum speed for flight with the side window open?

◦ A. 200 kts.
◦ B. 230 kts.
◦ C. Green Dot.
◦ D. 250 kts.

A

A. 200 kts.

25
Q

What is the limiting speed with the gear down locked?

◦ A. 250 kts.
◦ B. 280 kts.
◦ C. 300 kts.
◦ D. Green Dot

A

B. 280 kts.

26
Q

What is the limiting altitude for use of APU bleed?

◦ A. 15,000 feet.
◦ B. ENG START - UP TO 20 000 ft
 ONE PACK - UP TO 22 500 ft
 TWO PACKS - UP TO 15 000 ft
◦ C. 25,000 feet.
◦ D. 39,100 feet
A

B. ENG START - UP TO 20 000 ft

ONE PACK - UP TO 22 500 ft

27
Q

What is the maximum altitude for APU start on batteries only?

◦ A. 15,000 feet.
◦ B. 20,000 feet.
◦ C. 25,000 feet.
◦ D. 39,000 feet

A

C. 25,000 feet.

28
Q

What is the maximum EGT at TOGA THR?

◦ A. 710℃
◦ B. 950℃
◦ C. 765℃
◦ D. 690℃

A

B. 950℃

29
Q

Which of the following is a correct starter limitation?

◦ A. The max speed for starter engagement is 20% N2, (recommended 10%)

◦ B.

  • 4 consecutive cycles: Each lasts a maximum of 2 min
  • Pause between start attempts: 20 s
  • Cooling period, after 4 start attempts: 15 min
  • No running engagement of the starter, when N2 is above 20 %.

◦ C. After 4 failed start attempts, allow one hour cooling.
◦ D. Maximum continuous cranking is 3 minutes.

A

B.

  • 4 consecutive cycles: Each lasts a maximum of 2 min
  • Pause between start attempts: 20 s
  • Cooling period, after 4 start attempts: 15 min
  • No running engagement of the starter, when N2 is above 20 %.
30
Q

What is the max. speed for FLAP FULL?

◦ A. 177 kts.
◦ B. 185 kts.
◦ C. 200 kts.
◦ D. 205 kts.

A

A. 177 kts.

31
Q

. What is the maximum speed for the use of windscreen wipers?

◦ A. Green Dot.
◦ B. 230 kts.
◦ C. 240 kts.
◦ D. 250 kts.

A

B. 230 kts.

32
Q

What is the limiting groundspeed for the tyres?

◦ A. 185 kts.
◦ B. 190 kts.
◦ C. 195 kts.
◦ D. 198 kts.

A

C. 195 kts.

33
Q

What is the minimum fuel for take-off?

◦ A. 2000 kg.
◦ B. 1800 kg.
◦ C. 1500 kg.
◦ D. 1500 kg and WG TANK LO LVL not displayed.

A

D. 1500 kg and WG TANK LO LVL not displayed.

34
Q

In the MEL “remarks or Exceptions” column, what is signified by (0)?

◦ A. Aircraft may be flown back to base for rectification.
◦ B. A procedure to be carried out by the flight crew.
◦ C. A procedure to be carried out by maintenance.
◦ D. Dispatch is not allowed.

A

B. A procedure to be carried out by the flight crew.

35
Q

In the MEL “remarks or Exceptions” column, what is signified by an (*)?
◦ A. A crew operational procedure.
◦ B. Maintenance action is required.
◦ C. Inoperative equipment must have a placard.
◦ D. Aircraft may operate back to base.

A

C. Inoperative equipment must have a placard.

36
Q

What do we do if the brakes fail during an RTO?

◦ A. Brake pedals PUSH, reverse max, brakes RELEASE, A/SKID & N/W STRG SW off, brakes use max 1000
psi.
◦ B. Reverse max, recycle A/SKID & N/W STRG, brakes use as normal.
◦ C. Brake pedals PUSH and hold, A/SKID & N/W STR SW off, brakes use as normal.
◦ D. Reverse max, brake pedals release, A/SKID & N/W STRG off, brakes use max 1000 psi.

A

D. Reverse max, brake pedals release, A/SKID & N/W STRG off, brakes use max 1000 psi.

37
Q

After donning oxygen, what are the initial actions required in order to start an emergency descent
following rapid decompression (structural failure)?

◦ A. FCU:ALT - Select lower and PULL : HDG - turn left or right and PULL : SPD - PULL : MACH /
SPD adjust target.
◦ B. FCU:ALT - Select lower and PULL : HDG - turn left or right and PULL : MACH / SPD change over switch
PUSH.
◦ C. FCU:ALT - Select lower and PUSH : HDG - turn left or right and PULL when IAS increasing, select FULL
speedbrake.
◦ D. FCU:ALT - Select lower and EXPEDITE : HDG - turn left or right and PULL : THR levers to IDLE : select
half speedbrake.

A

A. FCU:ALT - Select lower and PULL : HDG - turn left or right and PULL : SPD - PULL : MACH /
SPD adjust target.

38
Q

Following a TCAS “CLIMB” message, what are the initial actions?

◦ A. A/P OFF : TOGA power : VERT SPD to Green Band
◦ B. ATHR OFF : VERT SPD to Green Band.
◦ C. A/P OFF : FD’s OFF : VERT SPD to Green Band.
◦ D. V/S SELECT +1500 : CLM power

A

C. A/P OFF : FD’s OFF : VERT SPD to Green Band.

39
Q

Immediate actions with unreliable IAS on take-of before SLAT retraction?

◦ A. AP/FD OFF : FLAPS - do not move.
◦ B. AP/FD ON : FLAPS - do not move.
◦ C. FD OFF : FLAPS - retract on schedule.
◦ D. AP OFF : FLAPS - retract on schedule.

A

A. AP/FD OFF : FLAPS - do not move.

40
Q

Initial actions in the event of a GPWS alert including “PULL UP”?

◦ A. AP ON : TOGA power : Select V/S 3000 ft/min.
◦ B. AP OFF : TOGA power : Select 17° pitch-up.
◦ C. AP OFF : sidestick hard back : TOGA power.
◦ D. AP OFF : TOGA power : follow pitch demands on FD

A

◦ C. AP OFF : sidestick hard back : TOGA power.

41
Q

” In order to leave the cockpit in an emergency, you should …

◦ A. … leave via a sliding window, using its associated escape rope only.”
◦ B. … leave via a sliding window only, using either escape rope.”
◦ C. … kick out the panel in the cockpit door.”
◦ D. … leave via a sliding window, or force the cockpit door in either direction.

A

D. … leave via a sliding window, or force the cockpit door in either direction.

42
Q

Initial actions in event of a rejected Take-Off at more than 72 kts.?

◦ A. Call “STOP” : REVERSE THR MAX : Maximum foot brakes.
◦ B. Call “STOP” : REVERSE THR MAX : Reverse idle by 80 kts.
◦ C. Call “STOP” : REVERSE THR MAX :SPD BRAKES FULL.
◦ D. Call “STOP” : REVERSE THR MAX .

A

D. Call “STOP” : REVERSE THR MAX .

43
Q

Initial actions when airborne after a “WINDSHEAR” warning?

◦ A. TOGA PWR : follow FD pitch demand.
◦ B. TOGA PWR : ignore FD - pitch to 17.5°
◦ C. TOGA PWR : follow FD pitch demand : raise landing gear.
◦ D. TOGA PWR : sidestick fully back : maintain gear / flap config

A

TOGA PWR : follow FD pitch demand.

44
Q

What are the initial actions, after selecting MAX REVERSE, in event of loss of braking when Autobrake is
selected OFF?

◦ A. Recycle A/SKID & NW STEERING switch : use brakes normal.
◦ B. Apply Parking Brake intermittently max 1000 psi.
◦ C. Switch to ALTN BRAKING, brakes use max 1000 psi.
◦ D. Brakes release, A/SKID & NW STEERING off, brakes max 1000 psi

A

D. Brakes release, A/SKID & NW STEERING off, brakes max 1000 psi

45
Q

What is the sequence of actions, on the FCU, in order to start an emergency descent (structural failure)?

◦ A. Select lower ALT and PULL : HDG knob - turn left or right and PULL : SPEED knob : PULL :
MACH / SPEED target adjust.

◦ B. PULL and select lower ALT : HDG knob - PULL and turn left or right : MACH / SPEED changeover button
- PRESS.

◦ C. Select lower ALT and PULL : HDG knob - PULL and turn left or right : SPEED knob : PULL and descend
at Mᴍᴏ/Vᴍᴏ minus 10 kts.

◦ D. Select lower ALT and PUSH : HDG knob - PULL and turn left or right : SPEED knob : PULL : MACH /
SPEED changeover button - PRESS.

A

◦ A. Select lower ALT and PULL : HDG knob - turn left or right and PULL : SPEED knob : PULL :
MACH / SPEED target adjust.

46
Q

Following a TCAS “Descend, descend now”, what are the initial actions?

◦ A. Follow Flight Director commands.
◦ B. A/P OFF : ATHR OFF : increase rate of descent from present value.
◦ C. A/P OFF : Both FD’s OFF : set vertical speed to Green area.
◦ D. A/P OFF : THR LVRS idle : set vertical speed to Green area.

A

C. A/P OFF : Both FD’s OFF : set vertical speed to Green area.

47
Q

Immediate actions with speed indications unreliable above THR RED ALT?

◦ A. AP off, F/D off, A/T off, Flaps maintain config, speedbrakes retract.
◦ B. Set CLB THR : above FL 100, set pitch +5° : below FL 100 set pitch + 10°.
◦ C. Maintain present pitch attitude and set CLB THR.
◦ D. Set TOGA THR : set pitch +5°.

A

B. Set CLB THR : above FL 100, set pitch +5° : below FL 100 set pitch + 10°.

48
Q

Initial actions in the event of a GPWS alert which includes “PULL UP”?

◦ A. Set TOGA THR : set pitch + 17 ½°.
◦ B. Set TOGA THR : climb aircraft at alpha prot.
◦ C. Sidestick fully aft : TOGA thrust : A/P OFF.
◦ D. Sidestick fully aft : TOGA thrust : then follow FD commands.

A

C. Sidestick fully aft : TOGA thrust : A/P OFF.

49
Q

“In order to leave the cockpit in an emergency, you should …

◦ A. … force the cockpit door open by pulling it.”
◦ B. … lock the sliding window fully open using the locking pin.”
◦ C. … leave via a sliding window using associated escape rope only.”
◦ D. … leave via a sliding window using either escape rope.”

A

D. … leave via a sliding window using either escape rope.”

----- (6 decks)

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