Airbus A320 - Engines

The EGT limit appears when a takeoff or a go-around mode is selected, or when the thrust reversers are selected, or if the alpha floor protection is activated.

True.

False.

Correct! Wrong!

The EGT limit does NOT appear when a takeoff or a go-around mode is selected, or when the thrust reversers are selected, or if the alpha floor protection is activated.

What is the difference between variable thrust and the speed mode?

In the fixed thrust mode, thrust is variable and speed is controlled by the elevator.

In the variable thrust mode, thrust is fixed and speed is controlled by the elevator.

In the fixed thrust mode, thrust is fixed and the elevator controls the speed.

Correct! Wrong!

If an A/THR disconnect switch is pushed and held for more than _____, the A/THR system is disconnected for the reminder of the flight. This includes the Alpha floor protection.

6 Seconds.

12 Seconds.

18 Seconds.

15 Seconds.

Correct! Wrong!

IGNITION FOR STARTING – On the ground, the ignition comes on automatically when N2 reaches _ and cuts off automatically when N2 reaches _.

18% and 55%

16% and 50%

15% and 55%

12% and 50%

Correct! Wrong!

What is considered to be the active range of the A/THR system?

During single engine operations from just above the IDLE stop to the FLX/MCT detent.

During two engine operations from just above the IDLE stop to the CL detent.

All statements are correct.

Correct! Wrong!

The EGT red line appears between the EGT red limit and the end of the scale. The EGT red limit is:

950 deg.C.

850 deg.C

750 deg.C

900 deg.C

Correct! Wrong!

Which steps of a manual start are being taken care of by the FADEC?

Starter valve opening and ignition cut off.

Starter valve closure and ignition cut off.

Starter valve closure and ignition start.

Starter valve opening and ignition start.

Correct! Wrong!

There is no reverse idle detent. When the pilot moves the lever out of the idle stop by pulling up the reverse lever on the front of the thrust lever, he selects reverse idle.

True.

False.

Correct! Wrong!

During an automatic starting, the FADEC detects a hot start, a hung start, or a stall, but the "no light up" is not monitored.

True.

False.

Correct! Wrong!

The FADEC detects a hot start, a hung start, a stall, or no light up.

The FADEC manages ____ idle modes.

Four (Regulated idle, Modulated idle, Approach idle and Reverse idle).

Two (Modulated idle and Approach idle).

Three (Modulated idle, Approach idle and Reverse idle).

Correct! Wrong!

A few seconds after selecting reverse, the amber REV indication changes to green. What does this mean?

The reversers are now fully deployed.

The reversers have been re-stowed.

The reverse thrust selection has been activated by the FADEC.

The reversers are unlocked.

Correct! Wrong!

How many FADECs are installed on the aircraft?

Four in total. Two per engine.

One, with two Engine Control Units (ECU).

Two, one per engine.

Correct! Wrong!

During a manual start, what function does the FADEC perform?

The FADEC does not perform any function during a manual start and all actions have to be carried out by the pilots.

To control the start sequence and take corrective action in case of a failure or malfunction.

Passive monitoring of the start sequence, to close the start valve and cut off the ignition on the ground.

Correct! Wrong!

The FADEC is normally powered by:

The DC aircraft electrical system.

The AC aircraft electrical system.

Its own magnetic alternator.

The DC then the AC aircraft electrical system.

Correct! Wrong!

The system has a magnetic alternator for an internal power source. FADEC is mounted on the fan case.

If the thrust lever is set between two detents, the FADEC selects the rating limit corresponding to the:

Higher detent.

Lower or higher detent depending of the N1 RPM.

Lower detent.

Lower or higher detent depending of the N2 RPM.

Correct! Wrong!

Can the engines be overboosted in the TOGA position?

No, because the EIU is responsible for monitoring N1 and N2.

No, because the ECU provides engine protection limit by monitoring N1, N2, and HMU fuel flow adjustments.

Yes, if the autothrust function is not active.

Correct! Wrong!

The FADEC will automatically abort an abnormal start thereby providing engine limit protection, but will the FADEC also automatically dry crank the engine?

Yes, as long as the ENG MASTER switch remains in the ON position.

No, that is why there is a CRANK selection on the ENG MODE selector.

Yes, even if the crew interrupts the start by placing the ENG MASTER switch to OFF.

Correct! Wrong!

You are in the middle of a manual engine start. What are you looking for when you select ENG MASTER 2 ON?

The fuel used is reset, both igniters are powered and fuel flow is indicated.

The fuel flow is reset, an igniter is powered and fuel used is indicated.

The fuel used is reset, both igniters are powered and N2 is increasing.

The fuel used is reset, fuel flow is indicated and IGNITION message on the E/WD.

Correct! Wrong!

Oil pressure and temperature are monitored upstream of the oil filter.

True.

False.

Correct! Wrong!

Oil pressure and temperature are monitored downstream of the oil filter.

Auto Thrust System - When are the throttles in the engagement range?

A single throttle of an operating engine is above idle but not above the MCT detent when one engine is running.

All statements are correct.

Both throttles are above idle but not above the CLB detent when both engines are running.

Correct! Wrong!

For an inflight start, the FADEC decides whether the engine is windmilling fast enough or needs assistance from the starter in view of current engine parameters and flight environment parameters.

False.

True.

Correct! Wrong!

A/THR engagement is confirmed when A/THR is displayed in _____ in the right column of the FMA.

White.

Green.

Blue.

Correct! Wrong!

Alpha floor protection is available:

From lift off and down to 100 feet radio altitude in the landing configuration.

From lift off and down to 50 feet radio altitude in the landing configuration.

From lift off and down to 500 feet radio altitude in the landing configuration.

From lift off and down to 750 feet radio altitude in the landing configuration.

Correct! Wrong!

Using manual thrust, the thrust lever position will determine the thrust setting for the engine.

True. They will operate like conventional throttles.

False. The next higher detent will be the thrust limit.

True, but care must be taken not to overspeed the engines.

Correct! Wrong!

In flight, both igniters are supplied, when the ENG MASTER sw is ON.

False.

True.

Correct! Wrong!

Continuous ignition is provided automatically when:

ENG ANTI ICE is selected ON and/or engine flameout is detected in flight and/or the EIU fails.

ENG ANTI ICE is selected ON and/or engine flameout is detected in flight

ENG ANTI ICE is selected ON.

Correct! Wrong!

The left column, first line of the FMA is used to indicate:

The mode of the A/THR in use when A/THR is armed or active.

Amber caution messages.

The thrust indication.

If A/THR is off, armed, or active.

Correct! Wrong!

How do you arm the A/THR in flight?

A/THR switch ON when throttles are not in the engagement mode.

A/THR switch ON when throttles are in the engagement mode.

Correct! Wrong!

When does oil quantity indication begin to pulse?

There is an oil quantity detector fault.

The oil quantity goes below the oil advisory limit (3 QT), that corresponds to the amber mark.

The oil quantity is the red area.

During engine start.

Correct! Wrong!

Data for the FADECs is directly sourced from the ADIRS, engine sensors and thrust levers. All other required data is amalgamated and supplied by an Engine Interface Unit (EIU).

True.

False.

Correct! Wrong!

During normal operation, in what detent are the thrust levers positioned once the thrust reduction altitude has been reached?

FLX.

CL.

CRZ.

MCT.

Correct! Wrong!

If the thrust levers are set in the idle detent, is Alpha floor protection still available?

Yes. Thrust lever position is disregarded.

No, because the IDLE detent is out of the A/THR active range.

Yes. As long as A/THR appears in column five.

Correct! Wrong!

In normal operation, autothrust is available when the thrust levers are in the range between the idle stop and CLB detent.

False.

True.

Correct! Wrong!

Does the FADEC provide EGT limit protection constantly?

No, EGT limit protection is only available during ground auto starts and single-engine operations.

Yes, in all phases of flight.

No, EGT limit protection is only available during ground auto starts.

Correct! Wrong!

Thrust reduction must not exceed 25 % of the full rated takeoff thrust. To meet this requirement, the flexible temperature must not be higher than ISA +60 °C(T MAX FLEX).

False.

True.

Correct! Wrong!

What does this indication mean ?

Alphafloor is in the alternate mode.

Alphafloor is active.

Alphafloor is in the direct mode.

Alphafloor is inoperative.

Correct! Wrong!

During a manual start, how is the start valve opened?

By depressing the ENG MAN START pb on the overhead panel.

It is automatic once the ENG MASTER is placed to the ON position.

By depressing the ENG MAN START pb on the overhead panel while the ENG MODE selector is out of the NORM position.

Correct! Wrong!

What would happen during the takeoff roll if the thrust levers were set to the FLX/MCT detent without FLEX temperature being entered?

The thrust setting would be MCT and there would be no corresponding warnings.

Nothing, the thrust setting would be at FLEX since FADEC automatically calculates a reduced thrust setting.

A LEVEL TWO warning would sound along with the appearance of an ECAM message.

Correct! Wrong!

During an automatic start, the FADEC controls:

The start valves, igniters, HP and LP fuel valves, and fuel flow.

The start valves, igniters, HP and LP fuel valves.

The start valves, igniters and fuel flow.

The igniters and fuel flow.

Correct! Wrong!

What does the FLEX represent in the FLX/MCT detent?

This is a derated thrust according the ground temperature of the day.

This is the thrust setting that should be chosen in the case of a single-engine go-around.

This is a reduced thrust setting used for takeoff.

This is the maximum continuous thrust setting for single-engine operations.

Correct! Wrong!

During the automatic start sequence of ENG 2, you notice that only igniter B is powered. Is it normal?

Yes, igniter A is only used for engine anti-ice.

Yes, igniter B is always used for ENG 2 start.

Yes, igniters are used alternately for engine start.

No, normally both igniters are used for all engine starts.

Correct! Wrong!

You are at the start of a descent and a blue N1 arc is displayed showing the new thrust demand. When does this happen?

Whenever there is power change with auto thrust engaged.

Whenever there is a power change with the autopilot engaged.

Whenever there is a power change in manual thrust.

Whenever the thrust levers are moved out of the CLIMB position.

Correct! Wrong!

When Alpha floor is activated, what power setting is automatically commanded and what FMA annunciation would appear in Column one?

MCT / THR LK.

CLB / CLB.

TOGA / A. FLOOR.

THR / LK.

Correct! Wrong!

What is Alpha floor protection?

It helps prevent the aircraft from stalling by limiting the angle of climb at high airspeeds.

It is a function of the flight control laws to prevent the aircraft from stalling.

It helps prevent the aircraft from stalling and protects against windshear encounters during takeoff and approach.

It helps prevent the aircraft from stalling by limiting the angle of bank at low airspeeds.

Correct! Wrong!

After takeoff the A/THR will not become active until:

The thrust levers are placed in the CLIMB position.

The autopilot is engaged.

The thrust levers are moved out of the TO/GA or FLEX/MCT detents.

The A/THR pushbutton is manually selected ON.

Correct! Wrong!

During engine start the amber FAULT light on the ENG MASTER panel illuminates. What does this indicate?

A failure in the engine fire extinguishing system.

A failure of the ENG MODE SELECTOR.

A failure in the automatic start sequence.

Correct! Wrong!

The ignition system is for engine starting on the ground and restarting in flight. It consists of two identical independent circuits for each engine, normally controlled by the FADEC channel A and channel B. Each FADEC channel can control both igniters.

False.

True.

Correct! Wrong!

If fuel flow data is lost for more than _____, the last two digits are dashed.

45 seconds.

20 seconds.

30 seconds.

One minute.

Correct! Wrong!

If the automatic start fails, the FADEC energizes both igniters at the same time during the second attempt at an engine start.

True.

False.

Correct! Wrong!

Is any thrust lever action required if an engine failed at rotation while using FLEX takeoff power?

No.

Yes.

Correct! Wrong!

The A/THR is armed on the ground provided at least one FD (Flight Director) is on by:

Engine start.

Setting the throttles to TO/GA.

Pressing the A/THR pb manually.

Correct! Wrong!

The Full Authority Digital Engine Control (FADEC) controls:

Engine limits.

Automatic and manual starting.

All statements are correct.

Fuel metering.

Correct! Wrong!

The FADEC will automatically command the reverse to stow, if at least one door is unstowed and reverse thrust is not selected while the engine is running.

True.

False.

Correct! Wrong!

Auto restow is totally inhibited in flight, and on ground, with N1 greater than 70 %.

When an engine out condition is detected, autothrust is available between the idle stop and MCT/FLX detent.

False.

True.

Correct! Wrong!

The FADEC system is self-powered:

Above 5% N1

Above 12 % N2.

When AC power is fully distributed and above 5% N1.

When AC power is fully distributed.

Correct! Wrong!

If a throttle is set between two detents, the FADEC selects the rating limit:

Corresponding to the lower mode.

Corresponding to the higher mode.

Determined by the throttle position.

Correct! Wrong!

For automatic starts, the FADEC opens the HP fuel valve at _____. For manual starts, the HP fuel valve opens when the engine master switch is turned on.

15% N2 on the ground and 22% N2 in flight.

10% N2 on the ground and 15% N2 in flight.

15% N2 on the ground and 10% N2 in flight.

22% N2 on the ground and 15% N2 in flight.

Correct! Wrong!

The FADEC prevents the thrust from exceeding the limit for the thrust lever position in automatic mode only.

True.

False.

Correct! Wrong!

The FADEC prevents the thrust from exceeding the limit for the thrust lever position in both manual and automatic modes.

Verification that Autothrust (A/THR) is active can be made by:

Watching the automatic movement of the thrust levers.

Only when the thrust levers are set at TOGA.

Only by looking at column five of the FMA.

Correct! Wrong!

The thrust levers can only be moved manually. There are 3 detents and 2 stops on the thrust quadrant.

False.

True.

Correct! Wrong!

There are 2 detents and 3 stops on the thrust quadrant. These are the TOGA stop, MCT/FLX detent, CL detent, Idle stop and Max reverse stop.

What is required for the FADEC to compute a reduced thrust setting?

A FLEX temperature must be entered on the ENG PERF page of the MCDU.

Nothing, it is an automatic function of the FADEC.

A FLEX temperature must be entered on the TAKE OFF PERF page of the MCDU.

A FLEX temperature must be entered on the INIT page of the MCDU.

Correct! Wrong!

While flying the airplane with A/THR active, the speed knob is pulled and turned to a selected speed that happens to be slower than Alpha prot. What speed will the airplane slow to?

VLS.

Green dot.

Green dot + 10 kt.

Green Dot + 5 kt.

Correct! Wrong!

For reverser actuation, the left engine uses hydraulic system pressure and the right engine uses hydraulic system pressure.

Blue - Green.

Yellow - Blue.

Yellow - Green.

Green - Yellow.

Correct! Wrong!

Maximum reverse should not be used below _____. Idle reverse is permitted down to aircraft stop.

80 kt.

60 kt.

70 kt.

90 kt.

Correct! Wrong!

Thrust reverser system – Each pivoting door moves independently but the doors are synchronized.

True.

False.

Correct! Wrong!

Each pivoting door moves independently (the doors are NOT synchronized). The total actuation time is less than two seconds.

The idle setting on the aircraft is capable of modulating due to certain conditions. During descent, what might cause the IDLE N1 setting to increase?

For a higher than normal bleed air demand or warmer than normal engine oil temp in flight.

The slats are extended.

All statements are correct.

Correct! Wrong!

When the A/THR system is in use:

The throttles can only be moved manually.

The throttles move automatically according to FADEC commands.

The throttles will move when the A/THR p/b is used.

Correct! Wrong!

During an engine start sequence, the gray background on N2 disappears at about 57%. What does this indicate?

There is a start fault and a dry crank is in progress.

The igniters are no longer being powered.

The start valve air pressure has dropped.

The start sequence has finished and all engine parameters have stabilized.

Correct! Wrong!

For manual starts, the FADEC has very limited authority to abort a start. The sole case is when on the ground and a start EGT exceedance occurs before 50% N2. In all other cases, it is the pilot's responsibility to interrupt the start sequence by either deselecting the manual start button or turning the engine master switch off as appropriate.

True.

False.

Correct! Wrong!

Is it possible to disconnect Alpha floor?

Yes, by depressing the autothrottle push button on the FCU.

Yes, by placing the thrust levers to IDLE.

No, Alpha floor protection is always available.

Correct! Wrong!

A/THR - Holding the instinctive disconnect pb for more than 15 seconds will:

Disengage the A/THR (including Alpha Floor) until below 1000 feet AGL for the reminder of the flight.

Disengage the A/THR (including Alpha Floor) for the reminder of the flight.

Disengage the A/THR (including Alpha Floor) until below 500 feet AGL for the reminder of the flight.

Disengage the A/THR (excluding Alpha Floor) for the reminder of the flight.

Correct! Wrong!

How many thrust lever positions are there, and how are they labeled?

There are 6 thrust levers positions: TO/GA, FLX/MCT, CL, IDLE, REV IDLE and MREV.

There are 7 thrust levers positions: TO/GA, MCT, FLEX, CL, IDLE, REV IDLE, and MREV.

There are 5 thrust levers positions: TO/GA, FLX/MCT, CL, IDLE and REV IDLE.

There are 4 thrust levers positions: TO/GA, FLX/MCT, CL, IDLE.

Correct! Wrong!

Is there any mechanical linkage between the thrust levers and the engines?

There is a mechanical linkage in case the ECU fails.

There is a fiber optic backup.

No, it is totally electrical.

No, it is electrically powered and hydraulically actuated.

Correct! Wrong!

Airbus A320 – Engines

Quiz

Airbus A320 - Engines

The EGT limit appears when a takeoff or a go-around mode is selected, or when the thrust reversers are selected, or if the alpha floor protection is activated.

What is the difference between variable thrust and the speed mode?

If an A/THR disconnect switch is pushed and held for more than _____, the A/THR system is disconnected for the reminder of the flight. This includes the Alpha floor protection.

IGNITION FOR STARTING – On the ground, the ignition comes on automatically when N2 reaches _____ and cuts off automatically when N2 reaches _____.

What is considered to be the active range of the A/THR system?

The EGT red line appears between the EGT red limit and the end of the scale. The EGT red limit is:

Which steps of a manual start are being taken care of by the FADEC?

There is no reverse idle detent. When the pilot moves the lever out of the idle stop by pulling up the reverse lever on the front of the thrust lever, he selects reverse idle.

During an automatic starting, the FADEC detects a hot start, a hung start, or a stall, but the "no light up" is not monitored.

The FADEC manages ____ idle modes.

A few seconds after selecting reverse, the amber REV indication changes to green. What does this mean?

How many FADECs are installed on the aircraft?

During a manual start, what function does the FADEC perform?

The FADEC is normally powered by:

If the thrust lever is set between two detents, the FADEC selects the rating limit corresponding to the:

Can the engines be overboosted in the TOGA position?

The FADEC will automatically abort an abnormal start thereby providing engine limit protection, but will the FADEC also automatically dry crank the engine?

You are in the middle of a manual engine start. What are you looking for when you select ENG MASTER 2 ON?

Oil pressure and temperature are monitored upstream of the oil filter.

Auto Thrust System - When are the throttles in the engagement range?

For an inflight start, the FADEC decides whether the engine is windmilling fast enough or needs assistance from the starter in view of current engine parameters and flight environment parameters.

A/THR engagement is confirmed when A/THR is displayed in _____ in the right column of the FMA.

Alpha floor protection is available:

Using manual thrust, the thrust lever position will determine the thrust setting for the engine.

In flight, both igniters are supplied, when the ENG MASTER sw is ON.

Continuous ignition is provided automatically when:

The left column, first line of the FMA is used to indicate:

How do you arm the A/THR in flight?

When does oil quantity indication begin to pulse?

Data for the FADECs is directly sourced from the ADIRS, engine sensors and thrust levers. All other required data is amalgamated and supplied by an Engine Interface Unit (EIU).

During normal operation, in what detent are the thrust levers positioned once the thrust reduction altitude has been reached?

If the thrust levers are set in the idle detent, is Alpha floor protection still available?

In normal operation, autothrust is available when the thrust levers are in the range between the idle stop and CLB detent.

Does the FADEC provide EGT limit protection constantly?

Thrust reduction must not exceed 25 % of the full rated takeoff thrust. To meet this requirement, the flexible temperature must not be higher than ISA +60 °C(T MAX FLEX).

What does this indication mean ?

During a manual start, how is the start valve opened?

What would happen during the takeoff roll if the thrust levers were set to the FLX/MCT detent without FLEX temperature being entered?

During an automatic start, the FADEC controls:

What does the FLEX represent in the FLX/MCT detent?

During the automatic start sequence of ENG 2, you notice that only igniter B is powered. Is it normal?

You are at the start of a descent and a blue N1 arc is displayed showing the new thrust demand. When does this happen?

When Alpha floor is activated, what power setting is automatically commanded and what FMA annunciation would appear in Column one?

What is Alpha floor protection?

After takeoff the A/THR will not become active until:

During engine start the amber FAULT light on the ENG MASTER panel illuminates. What does this indicate?

The ignition system is for engine starting on the ground and restarting in flight. It consists of two identical independent circuits for each engine, normally controlled by the FADEC channel A and channel B. Each FADEC channel can control both igniters.

If fuel flow data is lost for more than _____, the last two digits are dashed.

If the automatic start fails, the FADEC energizes both igniters at the same time during the second attempt at an engine start.

Is any thrust lever action required if an engine failed at rotation while using FLEX takeoff power?

The A/THR is armed on the ground provided at least one FD (Flight Director) is on by:

The Full Authority Digital Engine Control (FADEC) controls:

The FADEC will automatically command the reverse to stow, if at least one door is unstowed and reverse thrust is not selected while the engine is running.

When an engine out condition is detected, autothrust is available between the idle stop and MCT/FLX detent.

The FADEC system is self-powered:

If a throttle is set between two detents, the FADEC selects the rating limit:

For automatic starts, the FADEC opens the HP fuel valve at _____. For manual starts, the HP fuel valve opens when the engine master switch is turned on.

The FADEC prevents the thrust from exceeding the limit for the thrust lever position in automatic mode only.

Verification that Autothrust (A/THR) is active can be made by:

The thrust levers can only be moved manually. There are 3 detents and 2 stops on the thrust quadrant.

What is required for the FADEC to compute a reduced thrust setting?

While flying the airplane with A/THR active, the speed knob is pulled and turned to a selected speed that happens to be slower than Alpha prot. What speed will the airplane slow to?

For reverser actuation, the left engine uses ____ hydraulic system pressure and the right engine uses ____ hydraulic system pressure.

Maximum reverse should not be used below _____. Idle reverse is permitted down to aircraft stop.

Thrust reverser system – Each pivoting door moves independently but the doors are synchronized.

The idle setting on the aircraft is capable of modulating due to certain conditions. During descent, what might cause the IDLE N1 setting to increase?

When the A/THR system is in use:

During an engine start sequence, the gray background on N2 disappears at about 57%. What does this indicate?

Is it possible to disconnect Alpha floor?

A/THR - Holding the instinctive disconnect pb for more than 15 seconds will:

How many thrust lever positions are there, and how are they labeled?

Is there any mechanical linkage between the thrust levers and the engines?

IGNITION FOR STARTING – On the ground, the ignition comes on automatically when N2 reaches _ and cuts off automatically when N2 reaches _.

For reverser actuation, the left engine uses hydraulic system pressure and the right engine uses hydraulic system pressure.