Engines Atlas Flashcards

1
Q

During engine start what is the recommended optimum duct pressure?

A

21PSI with the start valve open

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2
Q

What is the position of the thrust reverses if the REV annunciations are green?

A

Fully extended

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3
Q

What does the starter cut out message indicate with N2 above 50% rpm?

A

The start valve has remained open after being commanded to close

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4
Q

With the right oil filter message displayed what is the first thing you will do?

A

Call for the QRH

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5
Q

What does a REV ISLN light on the ground indicate?

A

One thrust reverser may not deploy

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6
Q

When will the in-flight start envelope be displayed?

A

When an engine is shut down in flight and the secondary engine display is in view, and the associated ENG fire handle has not been pulled.

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7
Q

What malfunction has occurred if the right engine oil pressure light is on, the R ENG OIL PRESS message is displayed and the oil pressure indicates normal for the right engine?

A

Oil pressure switch fault

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8
Q

When the ignition is selected to the number one or two position, how many igniters will operate on each engine when continuous ignition is required?

A

1

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9
Q

After landing, when can the reverse levers be raised to the interlock stop?

A

When the thrust levers are at the idle position

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10
Q

How soon after the engine fuel control switch is positioned to RUN must EGT be observed rising (GE)? Who time is this?

A

25 seconds and the first officer

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11
Q

At what recommended N2 rpm do you need fuel and ignition to continue the start?

A

Max motoring (less than 1% rise in five seconds)

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12
Q

When should the engine start selector automatically move to AUTO?

A

50% N2

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13
Q

When must continuous ignition be on?

A

Moderate to heavy rain
Moderate to severe turbulence
Volcanic ash
Icing conditions
Standing water or slush on runway

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14
Q

When is continuous ignition automatically selected on?

A

When engine A/I is on or LE flaps Extended

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15
Q

What colour does the EGT change to if the EGT limit is reached?

A

Red

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16
Q

What EEC normal mode protection is not available in EEC ALTN (or off) mode?

A

Overboost protection

17
Q

How is the engine thrust reverser actuated on GE engines? PW engines?

A

767–300 GE: Pneumatically actuated by Fan air from respective engine
767–300 PW: Hydraulically actuated by respective HYD system

18
Q

The thrust rating of the CF6-80C2B7F Engine is?

A

62,100

19
Q

What is indicated when the start switch is in the AUTO position and VALVE light extinguished?

A

The start valve is closed, ignition off

20
Q

Which rotor speed is indicated by N1?

A

Low pressure, fan section

21
Q

What will occur if EGT exceed the red line limit?

A

Maximum exceedance value will be displayed and remain unless cleared by using the max indication reset button

22
Q

How is fuel flow normally displayed?

A

Both Digital read out and pointer

23
Q

What is the position of the Start valve with the start switch in GRD, and the VALVE light extinguished?

A

Open

24
Q

What is the status of the engine ignition system with the fuel control switch in CUTOFF?

A

Off

25
Q

What indicates that the start valve has opened and the air driven starter is turning the high-pressure compressor?

A

N2 Increasing

26
Q

When that TMC computes a reference N1, where does the reference N1 appear?

A

Above the N1 digital counter

27
Q

When must you have some indication of oil pressure during engine start?

A

Stabilised idle

28
Q

What is the position of the reversers when the REV annunciations are not displayed?

A

Stowed and locked

29
Q

Reverse thrust is supplied from?

A

The fan

30
Q

What is the thrust reverser status if the Amber REV annunciation is displayed?

A

Unlocked or in transit

31
Q

What colour is the REV annunciation when the thrust reverser is in transit?

A

Amber

32
Q

When does the engine idle speed change to approach idle?

A

Approach idle is commanded whenever:
1. the engine anti Ice is on
2. CONT ignition is selected, or
3. When landing flaps are selected (25-30)