Engine

Question 1

The engine is controlled via a dual channel

Answer 1

FADEC system

Question 2

How many igniters are energized during normal engine start?

Answer 2

One igniter during ground and both in flight engine starts

Question 3

The FADEC provides no protection for

Answer 3

Hot or hung starts during in flight engine starting

Question 4

What are the indications of an in-flight auto relight?

Answer 4

A WML icon is displayed next to the respective engine N2

Question 5

The Thrust Reverser System is

Answer 5

Hydraulically actuated

Question 6

During engine ground starts, FADEC will not allow fuel flow if ITT is above___

Answer 6

120C

Question 7

The ATTCS can be selected ON or OFF for takeoff. By default, ATTCS will be selected

Answer 7

ON

Question 8

The ATTCS automatically commands RSV whenever it is armed, thrust levers are at TOGA position, and one of
following conditions occurs except:

1. Difference between both engine N1 values is greater than 15%
2. One engine failure during takeoff or go-around
3. Windshear detection
4. During a normal Go-Around

Answer 8

During a normal Go-Around

Question 9

The indication FLEX TO-1 or FLEX TO-2 will be displayed on the ____ for the respective flexible takeoff thrust.

Answer 9

EICAS

Question 10

TO-1 or TO-2 is the thrust used for a ____

Answer 10

Normal takeoff; FADEC calculates the maximum N1 for conditions set on the MCDU Takeoff Data Set
Menu

Question 11

The go around mode is activated in flight whenever____

Answer 11

The TOGA switch is pressed

Question 12

Final Approach Idle is activated below 1200 feet AGL and

Answer 12

Landing flaps and landing gear down

Question 13

Placing the START/STOP Selector Knob to STOP commands the FADEC to shut down the engine provided

Answer 13

The associated thrust lever is in the IDLE position

Question 14

If you use a FLEX temperature for takeoff, where is this temperature displayed?

Answer 14

EICAS below the ATTCS display

Question 15

When is the ATTCS system engaged?

Answer 15

Thrust levers set to the TOGA position

Question 16

The FADEC will command both igniters for engine start, except?

Answer 16

Normal engine starts

Question 17

Where is the oil quantity displayed?

Answer 17

MFD Status

Question 18

If the FADEC does not detect a light-off within ___ after fuel flow, it will automatically turn off the ignition and fuel.

Answer 18

15 seconds

Question 19

In the event of a reverser failure, if both TLA are in the MAX REV position, the operating reverser will provide?

Answer 19

Minimum reverse thrust

Question 20

The FADEC will command engine shutdown whenever N2 reaches_____

Answer 20

102%

Question 21

When is the engine N1 automatically increased for Anti-Ice operation?

Answer 21

Flight Idle and Approach Idle

Question 22

When should an auto-relight attempt be considered unsuccessful and manually terminated?

Answer 22

If relight does not occur within 30 seconds or N2 falls below 7.2%

Question 23

When activated on takeoff, the ATTCS system will?

Answer 23

Cancel any FLEX and command either TO-1 RSV or TO-2 RSV as appropriate

Question 24

Inflight, selecting Ignition to OFF will____

Answer 24

Have no effect, as the FADEC disregards the OFF position inflight