Engine

Question 1

The magenta N1 bugs must match within % of each other.

Answer 1

1% of each other. AFM Pg. 2-17.

Question 2

The Maximum ITT limit during engine start is / º (AR/BR Engine) degrees Cº

Answer 2

941º/991º (AR/BR Engine) degrees Cº

AFM Pg. 1-17/17.2

Question 3

( ) must be off during take off, landing and single engine operation.

Answer 3

Engine Sync. PTM Pg. 7-27

Question 4

An amber ( ) indication on the EICAS between the N1 indicators occurs when the Engine Sync is on and the landing gear is down.

Answer 4

SYNC indication. AFM Pg. 4-28

Question 5

After an unsuccessful first/second/third start attempt, the aircrew must wait / / minutes for cooling before the next start attempt.

Answer 5

1/2/30. AFM Pg. 1-14.

Question 6

The pilot sets engine power through ( ’s )located within the thrust levers, which sends an electri-
cal signal to the respective DEEC.

Answer 6

RVDT’s. PTM Pg. 7-9

Question 7

When operating in ( ), the pilot sets power using the thrust levers and thrust lever
cable linkage.

Answer 7

Manual Fuel Mode. PTM Pg. 7-7

Question 8

A white ( ) indication will be displayed in the N1 indicator when Manual Fuel is selected.

Answer 8

MAN indication. PTM Pg. 7-9

Question 9

An amber  (   )     will display in the respective N1 indicator when the DEEC detects a malfunction
and reverts the Engine Fuel Control to Manual.

Answer 9

MAN. PTM Pg. 7-10

Question 10

During engine start, the ( ) turns on the corresponding standby fuel pump. PTM Pg. 7-26

Answer 10

DEEC. PTM Pg. 7-26

Question 11

Normal oil pressure is ( ) to ( ) psi; however, with oil pressure below 65 psi, the pilot should not ad-
vance the thrust lever above idle. AFM Pg. 3-19

Answer 11

50 to 80 psi. AFM Pg. 3-19

Question 12

IAW the AFM, satisfactory oil pressure limits are ( ) to ( ) psi, even with an amber oil pressure indication.

Answer 12

50 to 100 psi. PTM Pg. 7-31

Question 13

During start, engine light off should occur within ( ) seconds. AFM Pg. 2-15

Answer 13

10 seconds. AFM Pg. 2-15

Question 14

The DEEC will ( ) activate the engine ignition plugs during engine start. PTM Pg. 7-24

Answer 14

Automatically. PTM Pg. 7-24

Question 15

When both engine ignition plugs are activated, a ( ) IGN is displayed on the EICAS.

Answer 15

Green. PTM Pg. 7-25

Question 16

With only one engine ignition plug activated, a ( ) IGN is displayed on the EICAS.

Answer 16

White. PTM Pg. 7-25

Question 17

When the DEEC commands ignition and neither ignition plug activates, an ( ) IGN will be displayed on the EICAS.

Answer 17

Amber IGN. PTM Pg. 7-25

Question 18

The Left/Right engine ignition plugs can be selected “ ” by depressing the Left/Right IGN switch indicators.

Answer 18

ON. PTM Pg. 7-25

Question 19

Take Off Power can be maintained for a maximum of ( ) minutes.

Answer 19

5 Minutes. AFM Pg. 1-17/17.2

Question 20

During engine start, the ( ) rpm will rotate prior to the N1 rpm.

Answer 20

N2. PTM Pg. 7-26

Question 21

In the event of a hot start, the pilot should move the thrust lever to, “ ”. PTM Pg. 7-26

Answer 21

Cut Off. PTM Pg. 7-26

Question 22

Engine oil level should to be checked within ( ) hour of engine shutdown or an inaccurate indication
may result.

Answer 22

1 Hour. PTM Pg. 7-29

Question 23

If ( ) fan speed or N2 turbine speed are inappropriate for thrust lever position with no CAS message,
the aircrew should refer to Abnormal Engine Operation checklist in the amber section of the QRH.

Answer 23

N1 fan speed. QRH Pg. A-22.

Question 24

If an engine flame out occurs, the aircrew should refer to the ( ) Failure checklist in the red section of the QRH.

Answer 24

Engine Failure checklist. QRH Pg. E-19

Question 25

During cruise flight, if the engine oil pressure indicates ( ) psi (amber box), the aircrew should refer
to the Oil Pressure Low checklist located in the red section of the QRH.

Answer 25

55 psi (amber box). QRH Pg. E-18

Question 26

In the event of engine failure during final approach, the pilot should ensure flaps:

Answer 26

Are repositioned to 20 degrees and fly Vref plus 5 KIAS. AFM Pg. 3-21

Question 27

In the event an ( ) occurs, if the aircrew decides an Air Start is warranted, the Engine Shutdown in Flight checklist should still be accomplished prior to the Engine Air Start checklist.

Answer 27

Engine flameout/failure. QRH Pg. A-29

Question 28

In the event of an engine ( ) indication, the affected thrust lever should be placed to idle (unless a
critical thrust situation exists) for 15 seconds unless there are other indications of a fire.

Answer 28

FIRE. AFM Pg. 3-18

Question 29

In the event of an engine fire, if the Fire light goes out prior to ( ) seconds after placing the affected
thrust lever to idle, the most likely cause of the Fire light is a bleed air leak within the engine cowling.

Answer 29

15 seconds. PTM Pg. 8-3

Question 30

Engine acceleration in the ( ) mode will be slower than normal and should be considered in a
go-around situation.

Answer 30

Manual. AFM Pg. 4-19

Question 31

Do not attempt an ( ) start following engine failure which was accompanied by indications of inter-
nal engine damage or fire.

Answer 31

Air. AFM Pg. 3-22

Question 32

When operating the engine in MAN mode of operation above 30,000’ feet, maintain an N1 speed
greater than (      %).

Answer 32

66. AFM 4-19

Question 33

Minimum Oil Pressure is:

Answer 33

50 PSI

Question 34

Maximum Oil Pressure:

Answer 34

100 - 125 PSI

Question 35

Maximum Oil Temperature:

Answer 35

127 Degrees Celsius - 140 Degrees Celsius

Question 36

Minimum Oil Temperature:

Answer 36

30 Degrees Celsius

Question 37

Oils conforming to specification ( ) are approved for use in the aircraft engines.

Answer 37

EMS 53110