ENGINES/THRUST LEVERS

Question 1

What controls the engines in all operating regimes?

Answer 1

FADECs (Full Authority Digital Engine Controls)

Question 2

What functions does the FADEC Control?

Answer 2

• Fuel metering
• Engine limits based on thrust lever angle
• Start sequencing
• Provides Engine indications and thrust limit displays on the E/WD

Question 3

What redundancy does the FADEC have?

Answer 3

Dual channel redundancy- one channel is active while the other is standby.

Question 4

What is the power source for the FADEC?

Answer 4

• The system has its own alternator making it independent of the aircraft electrical system when N2 is above 10%.
• If this alternator fails the FADEC automatically switches to aircraft electrical power.

Question 5

When will FADEC abort an automatic start?

Answer 5

• Hot start
• Stalled start
• No ignition

Question 6

The FADEC detects a fault during automatic start. What crew intervention is required?

Answer 6

There is no crew intervention necessary. The FADEC will discontinue the start, clear the engine, and attempt a restart (if warrant) automatically.

Question 7

When does the FADEC command a higher engine idle speed?

Answer 7

• Bleed demands
• Approach configuration
• High Engine or IDG temperature

Question 8

How many igniters fire during a normal automatic ground start sequence?

Answer 8

• One igniter with the other serving as a backup

- The FADEC automatically alternates the igniters (A and B) at each start.

Question 9

How many igniters fire on manual or in-flight starts?

Answer 9

Two, both A and B

Question 10

When does continuous ignition automatically operate?

Answer 10

• NEO aircraft
  
  • Engine flameout detection
  • Failure of the EIU
  • In-Flight unscheduled sub idle or surge
  • Master switch cycled from ON to OFF then back to ON position
• Non-NEO
  
  • all of the above
  • Engine anti-ice ON
  • approach idle
  • MAX/FLEX power selected

Question 11

What are the five detent position of the thrust levers?

Answer 11

• TOGA= Takeoff/go around
• FLX/MCT= Flex/maximum continuous Thrust
• CL= climb
• IDLE= Idle
• MAX REV = Maximum Reverse Thrust

Question 12

On the ground, how can the A/THR be armed?

Answer 12

• By setting the thrust levers in the TOGA or FLEX gate ( with a FLEX temperature inserted in the MCDU)
• At least one FD must be On for A/THR to arm during takeoff

Question 13

What is the active range of the A/THR?

Answer 13

• Just above IDLE to the CL detent (2 engine)

- Just above IDLE to the MCT detent (1engine)

Question 14

What is normal operational position of the thrust levers when A/THR is active?

Answer 14

The CL detent

Question 15

What determines the maximum thrust the A/THR system will be able to command?

Answer 15

The thrust lever angle

Question 16

What are three ways to disconnect the A/THR?

Answer 16

• A/THR pushbutton
• Instinctive disconnect pushbutton
• Thrust levers to IDLE

Question 17

What is the preferred method of disconnecting A/THR?

Answer 17

Set the thrust lever angle to the existing EPR and push the instinctive disconnect pushbutton.

Question 18

How would the A/THR be disconnected for the remainder of the flight?

Answer 18

Press and hold the instinctive disconnect pushbutton for 15 seconds. The A/THR cannot be re-engaged once this is done. ALPHA FLOOR is also lost if this is done.

Question 19

What happens to thrust and what annunciates on the FMA during ALPHA FLOOR?

Answer 19

• Thrust= TOGA

- FMA= “A.FLOOR”

Question 20

When does the aircraft leave ALPHA FLOOR and what does the FMA change to?

Answer 20

Upon reaching a lower angle of attack. The FMA changes to “TOGA LK”

Question 21

Following ALPHA FLOOR, how would the crew return normal A/THR function?

Answer 21

• Press the instinctive disconnect pushbutton
• Return Thrust levers to CL detent
• Push the A/THR pushbutton to engage A/THR

Question 22

When is ALPHA FLOOR protection active?

Answer 22

-From lift-off through 100 ft RA on approach

Question 23

When would Thrust Lock occur?

Answer 23

• Thrust levers in CL detent and A/THR pushbutton on the FCU is pushed, or
• A/THR disconnects due to a failure.

Question 24

How is A/THR normally armed?

Answer 24

By advancing the thrust levers to TOGA or FLX

Question 25

What would the FMA indication be during a takeoff roll using FLEX thrust on RWY with localizer?

Answer 25

MAN FLX, SRS, RWY, A/THR (blue)

Question 26

What would the FMA indications be during takeoff using TOGA thrust on a runway without Localizer?

Answer 26

MAN TOGA, SRS, A/THR (blue)

Question 27

What would the FMA indications be during takeoff roll of the A/THR didn’t arm on a runway with a localizer? Should the takeoff be aborted?

Answer 27

- SRS, RWY - Continuing the Takeoff is a safe option, but the thrust levers must be moved to the climb detent at thrust reduction altitude and the crew must manually engaged A/THR

Question 28

How should A/THR be turned off?

Answer 28

Match the blue thrust lever angle indicators to the present thrust setting and push the instinctive disconnect pushbuttons or move THRUST LEVERS to IDLE.

Question 29

What should the pilot do to get out of THRUST LOCK?

Answer 29

Match the thrust lever angle with ENG output.

Question 30

What should pilot do to get out of TOGA LOCK?

Answer 30

Push the instinctive disconnect pushbuttons and move the THRUST LEVERS to the CL detent.

Question 31

What is the A/THR active zone for two-engine operations?

Answer 31

From slightly above IDLE to CL

Question 32

What is the A/THR active zone for single-engine operations?

Answer 32

From slightly above IDLE to MCT

Question 33

What controls the engine LP fuel valves?

Answer 33

- Engine MASTER switch | - ENGINE FIRE pushbutton

Question 34

What does a FAULT light on the ENG panel indicate?

Answer 34

- Automatic start abort | - Switch disagreement between HP valve and it’s commanded position.

Question 35

What is the rated thrust of each engine?

Answer 35

- A319 V2524-A5= 23,500 lbs - A320 CEO V2527-A5= 27,000 lbs - A321 V2533-A5= 32,500 lbs - A320 NEO PW1127G= 27,000 lbs

Question 36

What is the required engine warm up time?

Answer 36

IAE V2500 Shutdown -2 hrs = 3mins IAE V2500 Shutdown +2hrs = 5mins PW 110OG Shutdown = 5mins

Question 37

What is the required engine cool down time after landing?

Answer 37

IAE V2500 = 0 mins. Rev Idle IAE V2500 = 3mins. Greater than reverse idle PW1100G = minimum of 3 mins, 5 mins recommended

Question 38

What does the cooling indication mean on the E/WD for NEO Aircraft?

Answer 38

- Steady indication =Automatic dry cranking is about to begin and the timer indicates the time left before dry crank begins. - Pulsing indication= Automatic dry cranking is in progress.

Question 39

If icing conditions exist on the ground, how is the Engine Run-Up procedure different for NEO and Non-NEO aircraft?

Answer 39

- IAE V2500= Accelerate to Minimum of 50% N1 at intervals not more than 15 minutes apart - PW1100G= Accelerate to Minimum of 60%N1 at intervals not more than 30 minutes apart

Question 40

If during start, the ground crew reports a fuel leak from the engine, what should be done by the flight crew?

Answer 40

- IAE V2500= Run the engine for 5 minutes, if leak disappears, the flight can continue without Maintenance action. - PW 1100G = Abort engine start sequence, Maintenance action is required

Question 41

How is Approach Idle on NEO vs Non-NEO aircraft?

Answer 41

- Non-NEO Minimum Approach Idle Speed occurs when: * Aircraft is in flight and the flaps are extended - NEO Minimum Approach Idle Speed occurs when: * Aircraft is in flight and the flaps are at CONFIG 3 or FULL or when the landing gear is down.