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30 Cards in this Set

  • Front
  • Back
What controls the engines in all operating regimes?
FADECs (Full Authority Digital Engine Control)
What functions does the FADEC control?
- Fuel metering

- Engine limits based on thrustt lever angle

- Start sequencing

- Provides engine indications and thrust limit displays on the E/WD
What redundancy does the FADEC have?
Dual channel redundancy - one channel is active while the other is standby
What is the power source for the FADEC?
- The system has its own alternator making it independent of the aircraft electrical system when N2 is above a set value

- If this alternator fails, the FADEC automatically switches to aircraft electrical power
When will the FADEC abort a start?
- Hot Start

- Stalled Start

- No Ignition
If the FADEC detects a fault during automatic start, is any crew intervention required?
No. The FADEC will discontinue the start, clear the engine, and attempt a restart (if warranted) automatically
When does the FADEC command a higher engine idle speed?
- Bleed Demands

- Approach Configuration

- High engine or IDG temperatures
How many igniters fire during a Normal automatic ground start sequence?
- One igniter with the other serving as a backup

- The FADEC automatically alternates the igniters (A and B) at each start
How many igniters fire on a manual or in-flight start?
Both A and B
When does continuous ignition automatically operate?
- Engine Anti-ice ON

- Engine flameout detection

- Failure of the EIU
What are the 5 detent positions of the thrust levers?
-TOGA

- FLX MCT

- CL

- IDLE

- MAX REV
On the ground, how do you arm the A/THR?
- By setting the thrust levers in the TOGA or FLEX gate (when a FLEX temp inserted in the MCDU)

- At least one FD must be ON for the A/THR to arm during takeoff
What is the active range of the A/THR?
- Just above IDLE to the CL detent (2 Engines)

- Just above IDLE to the MCT detent (1 Engine)
What is the normal operational position of the thrust levers when A/THR is active?
The CL detent
What determines the maximum thrust the A/THR system will be able to command?
The position detent of the thrust lever
What are 3 ways to disconnect the A/THR?
- A/THR pushbutton

- Instinctive Disconnect buttons

- Thrust Levers to IDLE
What is the preferred method of disconnecting A/THR?
Set the thrust levers to match the TLA to the existing N1 and disconnect using the instinctive disconnect pushbutton
How do you disconnect the A/THR for the remainder of the flight?
Press and hold the Instinctive Disconnect button for 15 seconds
Will you be able to restore A/THR if you held down the Instinctive Disconnect Pushbutton for more than 15 seconds?
No
What would you lose if you held down the Instinctive Disconnect Pushbutton for more than 15 seconds?
Alpha Floor Protection
What happens to thrust and what annunciates on the FMA when you reach Alpha Floor?
- Thrust: TOGA

- FMA: A.FLOOR
What occurs during Alpha Floor protection after speed increases above Vls?
FMA changes to TOGA LK
How do you then regain normal A/THR?
- Move Thrust Levers to the TOGA detent

- Press the Instinctive Disconnect button

- Return Thrust Levers to CL detent

- Push the A/THR pushbutton to engage A/THR
When is Alpha Floor Protection active?
From lift-off through 100' RA on approach
When would Thrust Lock occur?
- Thrust levers in CL detent and A/THR pushbutton on the FCU is pushed, or

- A/THR disconnects due to a failure
Explain the Normal Start sequence.
- ENG MODE to IGN/START

- ENG MASTER to ON

- Observe Start Valve Open and gray N2 background

- At 16% N2 Ignition (A or B) on

- At 22% N2 HP Fuel

- At 50% N2 starter cutout

- Approximately 58% gray N2 background disappears

- Idle at 60%
Explain the Manual Start sequence.
- ENG MODE to IGN/START

- ENG MAN START pushbutton ON

- At maximum N2 motoring speed (Min 20%), ENG MASTER ON

- Observe AB ignition, fuel flow increase, EGT and N1 increase in 15 seconds

- At 50% observe N1 starter cutout and Ignition off

- ENG MAN START pushbutton OFF
What control the engine LP fuel valves?
- Engine MASTER switch

- ENGINE FIRE pushbutton
What does a fault light on the ENG panel indicate?
- Auto Start Abort

- Switch disagreement between HP valve and its commanded position
What is the rated thrust of each engine?
- A319: 23,500 lbs

- A320: 27,000 lbs