Embraer 190 - Normal Procedures (Sopm)
10 Questions
| Total Attempts: 431
GROUND OPERATIONS QUESTION MADE FROM S. O. P. MGOOD LUCK!SANTIAGO STOCKER
Questions and Answers
- 1.Batteries Voltage .........................................CHECK...............RSP
- A.
Verify batteries voltage at or above 20 V
- B.
Verify batteries voltage at or above 22 V
- C.
Verify batteries voltage at or above 24 V
- 2.If batteries voltage is between 21 V and 22 V (ANAC/TCCA certification) or 21 V and 22.5 V (FAA/EASA certification), ...
- A.
Recharge the batteries prior to takeoff, through any AC source.
- B.
Change the batteries.
- 3.The Electrical PBIT is automatically performed after the airplane is powered by any AC source and takes about ___________ to complete.
- A.
1 minutes
- B.
2 minutes
- C.
3 minutes
- 4.The Electrical PBIT will be interrupted if ...
- A.
Electric hydraulic pump is running
- B.
Parking brake is set
- C.
AC power is interrupted while the test is running
- D.
FLIGHT CONTROLS MODE Panel switches are cycled
- 5.FIRE EXTINGUISHER Panel (Overhead)....CHECK .............. RSP Press and hold the TEST button and observe aural warning and ...
- A.
2 Master Warning, 8 overhead lights and 7 EICAS indications, 17 lights total.
- B.
2 Master Warning, 6 overhead lights and 7 EICAS indications, 15 lights total.
- 6.N1 Target ......................................................CHECK...............RSP The N1 target indication on the EICAS must be equivalent to theN1 target indication available via performance calculation.The difference between N1 given by FADEC (indicated onEICAS) and the computed value is zero or this difference is positive and lower than or equal to ...
- A.
1.5%.
- B.
1.0%.
- C.
0.5%.
- 7.GO AROUND In case of flight director is inoperative, rotate the airplane to __ nose up.
- A.
8°
- B.
18°
- 8.To prevent electrical power interruptions, it is recommended to wait _____________ after GPU button is pushed in or after APU is stabilized to shutdown the remaining engine.
- A.
10 seconds
- B.
30 seconds
- C.
60 seconds
- 9.ECS OFF TAKEOFF APU BLEED valve will supply bleed air for both PACKS operation during takeoff until ____ ft.
- A.
500 ft
- B.
1000 ft
- C.
1500 ft
- 10.ECS OFF TAKEOFF If APU BLEED is unavailable the PACKS will remain OFF until ____ ft AGL.
- A.
500 ft
- B.
1000 ft
- C.
1500 ft
ELECTRICAL QUESTIONS MADE FROM THE AOM VOL. 2GOOD LUCK! SANTIAGO STOCKER.
Questions: 36 | Attempts: 2796 | Last updated: Mar 22, 2022
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Sample QuestionBoth IDGs and the APU generator are rated at _______________________ , three-phase.
AUXILIARY POWER UNIT QUESTIONS MADE FROM THE AOM VOL. 2GOOD LUCK! SANTIAGO STOCKER.
Questions: 22 | Attempts: 1871 | Last updated: Mar 20, 2022
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Sample QuestionThe Auxiliary Power Unit (APU) is a gas turbine engine located in the airplane tailcone, which provides pneumatic and electrical AC power. The pneumatic power is used for engine starting and to supply bleed air to the air conditioning packs of the Environmental Control System (ECS). An electrical AC generator supplies _____________ to the electrical system.
FUEL SYSTEM QUIESTIONS MADE FROM AOM VOL. 2GOOD LUCK!SANTIAGO STOCKER.
Questions: 29 | Attempts: 1817 | Last updated: Mar 22, 2022
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Sample QuestionFuel is stored in____ integral wing tanks, interconnected by a crossfeed valve.
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