Engine Flashcards

1
Q

What is the thrust reverser system’s actuation method?

A

Hydraulically actuated

The thrust reverser system is controlled from the cockpit via the thrust levers.

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2
Q

What type of engine is the Pratt and Whitney PW1900G?

A

Axial-flow twin spool turbofan with a high-bypass ratio

It features a low speed gear-driven fan.

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3
Q

What is the purpose of the fan drive gear system?

A

Allows the engine fan to operate at slower speeds than the low-pressure compressor and turbine

This increases bypass ratio, resulting in lower fuel consumption, emissions, and noise.

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4
Q

What does the Dual-channel FADEC architecture control?

A

Engine protection, control of requested and maximum N1, control of ATTCS

FADEC stands for Full Authority Digital Engine Control.

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5
Q

What does the MAX setting on the thrust lever do?

A

Sets the maximum thrust available for dual or single engine operation

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6
Q

What happens when the thrust lever is pulled against a spring?

A

Reaches the MAX REV position for maximum reverse thrust

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7
Q

What does the IGNITION selector knob’s AUTO position do?

A

FADEC automatically controls the ignition system

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8
Q

What does an amber boxed FAIL indication signify?

A

An engine has flamed out or shut down without pilot action

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9
Q

What does a green tick-mark on the N1 dial indicate?

A

The maximum allowable N1 (maximum thrust) for the current thrust rating and operating conditions

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10
Q

What is indicated by a red FIRE warning on the ITT dial?

A

An engine fire condition

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11
Q

What does the Fuel Distribution System consist of?

A
  • Integrated Fuel Pump and Control (IFPC)
  • Fuel/Oil Manifold (FOM)
  • Fuel/Oil Heat Exchanger (FOHX)

These components work together to ensure proper fuel flow and management.

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12
Q

What is the main function of the engine oil system?

A

Lubricate engine bearings, gears, shafts, and splines; provides thermal management

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13
Q

What does the Air Turbine Starter (ATS) do?

A

Rotates the rotor speed to start the engine using bleed air

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14
Q

What happens when the FADEC detects a surge during engine start?

A

Commands a fuel depulse, cycling fuel off for 2 seconds and back on for 12 seconds

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15
Q

What is the function of the thrust reverser system after an engine failure?

A

The thrust reverser is blocked and cannot be deployed

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16
Q

What does the FADEC De-power Function do?

A

Turns the FADECs OFF on the ground, 5 minutes after engine shutdown

17
Q

What does the ATTCS indicate when armed and engaged?

A
  • ATTCS in white: system is armed
  • ATTCS in green: system is engaged
18
Q

What is flexible takeoff thrust based on?

A

Assumed temperature; must be higher than TO TEMP

19
Q

What does the GA mode stand for?

A

Go-Around Thrust Mode

20
Q

What is the function of the maximum continuous thrust?

A

Used in emergency situations where higher thrust than usual is required

21
Q

What is the FADEC protection against hot start?

A

Commands fuel depulse, auto-restart, or start abort

22
Q

What happens if N1 or N2 reaches 105%?

A

FADEC automatically commands an engine shutdown

23
Q

What does the FADEC do in the event of shaft shear detection?

A

Automatically commands an engine shutdown