Power Plant quiz

Power Plant quiz

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Question 1 of 19
1. Question
The major components of the Superjet 100 Powerplant are: ________________ .
- the Engine, the Mounts and all the Cowlings that enclose the Engine (the Nacelle).
- the Engine, the Mounts and the Accessory Gear Box.
- the Fuel System, the Oil System and the Air System.
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Question 2 of 19
2. Question
What are the SaM146 functional components?
- The Booster, the Low and the High Pressure Systems, the FADEC.
- The Inlet, the Low and the High Pressure systems, the Exhaust and the Accessory Drive systems.
- The Inlet, the Pylon, the Low and the High Pressure Systems, the Nacelle.
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Question 3 of 19
3. Question
A hazard / danger area is defined around Engine at idle mode: _______________________ .
- suction until 2.5 m and rear margin until 30 m.
- suction until 3.5 m and rear margin until 100 m.
- suction until 3.5 m and rear margin until 600 m.
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Question 4 of 19
4. Question
What functions does the Air Intake not perform?
- calibrates airflow
- reduces noise
- increases engine thrust
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Question 5 of 19
5. Question
The whole Compressor Control System is commanded by the _____________ .
- Actuator Control Unit (ACU)
- Engine Over Speed Unit (EOCU)
- Digital Engine Control Unit (DECU)
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Question 6 of 19
6. Question
The Fan consists of ______________.
- a single stage fan
- a two stage fan
- a three stage fan
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Question 7 of 19
7. Question
The gas detent produced by Combustion Chamber delivers high energy to ______________.
- the Fan
- the Turbine
- the Compressor
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Question 8 of 19
8. Question
The Turbine consists of ______________.
- the High Pressure Turbine and the Middle Pressure Turbine
- the Middle Pressure Turbine and the Low Pressure Turbine
- the High Pressure Turbine and the Low Pressure Turbine
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Question 9 of 19
9. Question
The Engine Exhaust Section ____________________ primary and secondary airflows.
- only participates in Engine noise reduction due to
- directs and balances pressure and temperature of the mixed exhaust gas from
- increases pressure and temperature of the mixed exhaust gas from
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Question 10 of 19
10. Question
The roller bearing absorbs ________________.
- only radial loads
- only axial loads
- axial and radial loads
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Question 11 of 19
11. Question
The Oil System enables _________________ of all the bearings and gears.
- the heating and lubrication
- the heating and cleaning
- the cooling and lubrication
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Question 12 of 19
12. Question
What functions does the Engine Fuel System not perform?
- delivers fuel to the engine combustion chamber
- cools down the engine oil
- supplies fuel to Thrust Reverser System
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Question 13 of 19
13. Question
The left and right Thrust Levers are located on___________________, in the cockpit.
- the Central Pedestal
- the left and right Control Panel
- the left and right Overhead Panel
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Question 14 of 19
14. Question
The Engine is controlled by a Full Authority Digital Engine Control system (FADEC), with the help of data received from _______________.
- engine sensors
- aircraft sensors
- flight crew
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Question 15 of 19
15. Question
The Control and Monitoring System is based on two electronic units architecture:____________________.
- The Digital Engine Control Unit (DECU) and the Fuel Metering Unit (FMU)
- The Digital Engine Control Unit (DECU) and the Engine Over Speed Unit (EOSU)
- The Fuel Metering Unit (FMU) and the Engine Over Speed Unit (EOSU)
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Question 16 of 19
16. Question
The Pneumatic System supplies ________ stage Engine Compressor bleed air to airplane user systems.
- 2nd or 4th
- 3rd or 6th
- 4th or 6th
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Question 17 of 19
17. Question
The Starting System converts ___________________ that is transmitted to the AGB, enabling the rotation of the spool.
- electric power into mechanical power
- mechanical power into pneumatic power
- pneumatic power into mechanical power
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Question 18 of 19
18. Question
In which area of the EWD is the main engine data displayed?
- the left upper area
- the right upper area
- the central area
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Question 19 of 19
19. Question
The Engine is attached to the Pylon by ___ mounts.
- two
- six
- eight
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