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Flashcards in Engines/APU Deck (49)
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1

The FADEC controls all but which of the following

Engine Anti-Ice

2

When the engines are running the FADEC is powered by

Its own alternator

3

The FADEC automatically_____ the igniters at each start

Alternates

4

During the automatic start sequence of ENG 1 you notice that only igniter A is powered IS this Normal

yes, igniters are used alternately for automatic engine start, in this case igniter A

5

If the FADEC detects a non normal condition during an automatic start with N2 below 50% it

Aborts the start and auto-cranks the engine

6

The FADEC normal control mode meters fuel to maintain a reference

EPR

7

The FADEC alternate control meters fuel to maintain a reference

N1

8

IF the EPR mode fails, the FADEC automatically reverts to the _____ mode

N1

9

Are engine limit protections provided in the N1 unrated Mode?

No protections are provided

10

Which is not a source of air for engine start

PTU

11

During a manual start _____ is not available

Automatic Abort

12

Verify a _____ bleed pressure indication during a manual start

Green

13

Durning a manual start, what function does the FADEC perform

Provides ECAM start fault detection, however, automatic abort and crank capabilities are not available

14

Which igniters is/are used during a manual start?

Both A and B

15

Why are both igniters powered during the ENG1 start sequence shown on the graphic

This is a manual start and both igniters are always used

16

What does a FAULT light indicate on the Engine Start and Ignition Panel?

Automatic aborted start

17

Continuous ignition is selected manually by positioning ENG MODE selector to

IGN/START

18

What action is required if continuous ignition is desired after engine start?

The ENG MODE selector must be cycled to NORM and then back to IGN/START

19

Continuous ignition NOT automatically provided for which of the following conditions

Turbulent Air

20

When is continuous ignition NOT automatically provided in flight

Engine low oil pressure indicated

21

How should you cancel a "ENG THR LEVERS NOT SET" caution during takeoff?

Advance the thrust levers to TO/GA

22

Which is NOT a position defined by a stop or detent

REV IDLE

23

The A/THR is armed on the ground by setting the thrust levers to _____ with at least one FD on

FLX with a FLEX temperature entered in the FMGC

24

The auto thrust will not arm when the thrust levers are advanced for takeoff if both _____ are off

FDs

25

Autothrust arming is confirmed when A/THR is displayed in _____ in the right column (column 5) of the FMA and the A/THR button is illuminated green

Blue

26

The A/THR is engaged in flight by

Setting thrust levers in the engagement range with the auto thrust system armed

27

The engagement range of the A/THR with both engines running is

Forward of IDLE to CL

28

The engaged mode of the A/THR is displayed in _____ in the left column (column 1) of the FMA

Green

29

An engaged auto thrust system reverts to which mode when the flight directors and autopilots are selected off

SPEED

30

The engagement range of the A/THR with one engine running is

Forward of IDLE detent to FLX/MCT detent