Embraer 190 - Fire Protection
FIRE PROTECTION QUIESTIONS MADE FROM AOM VOL. 2GOOD LUCK!SANTIAGO STOCKER.
- 1.The fire protection system provides fire detection and extinguishing capabilities for:
- A.
Engines, APU, Cargo Compartments and Lavatories.
- B.
Engines, APU and Lavatories.
- 2.The Engine fire DETECTION electrical power is supplied by:
- A.
DC ESS BUSES
- B.
HOT BATT BUS 1 and HOT BATT BUS 2
- 3.The Engine fire EXTINGUISHING electrical power is supplied by:
- A.
HOT BATT BUS 1 and HOT BATT BUS 2
- B.
DC ESS BUSES
- 4.The Engine Fire Detection System is monitored by __________________________ . When a fire condition is detected the signal goes to the MAU which generates the associated EICAS messages and alarms.
- A.
One detector loop
- B.
Two detector loops
- 5.Anytime the fire handle is pulled it commands the following shutoff valves to close:
- A.
The engine fuel shutoff valve; and the engine hydraulic shutoff valves.
- B.
The engine fuel shutoff valve only.
- C.
The engine fuel shutoff valve; the engine hydraulic shutoff valves and; the engine bleed air shutoff valve.
- 6.A total of ____ fire extinguisher bottles named A and B are installed in the airplane to serve either or both engines.
- A.
Two
- B.
Three
- 7.When an engine fire extinguishing bottle is discharged, fire handle illumination may be lost. In this case if the CAS message is still active the fire condition ...
- A.
Persists.
- B.
Does not persists.
- 8.The APU fire DETECTION electrical power is supplied by:
- A.
DC ESS BUSES
- B.
HOT BATT BUS 1 and HOT BATT BUS 2
- 9.The APU fire EXTINGUISHING electrical power is supplied by: – APU fire extinguishing:
- A.
HOT BATT BUS 1 and HOT BATT BUS 2.
- B.
DC ESS BUS 2
- 10.The APU Fire Detection System is comprised of ___ detectors loops.
- A.
Two
- B.
Three
- 11.When a fire condition is detected the signal goes to the ____ which generates the associated EICAS messages and alarms.
- 12.When the APU FIRE EXTINGUISHER button is pressed the system:
- A.
Discharges the APU fire bottle, shuts down the APU through the APU FADEC, closes the APU fuel shutoff valve (SOV) and displays an EICAS ADVISORY message APU FIREX BTL DISCH.
- B.
Discharges the APU fire bottle, shuts down the APU through the APU FADEC and displays an EICAS ADVISORY message APU FIREX BTL DISCH.
- C.
Discharges the APU fire bottle, closes the APU fuel shutoff valve (SOV) and displays an EICAS ADVISORY message APU FIREX BTL DISCH.
- 13._____ fire-extinguishing bottle is installed in the rear fuselage.
- A.
One
- B.
Two
- 14.As soon as the APU EMER STOP pushbutton is pressed the red strip bar is replaced by the white stripe bar indicating that ...
- A.
The APU has shut down.
- B.
The APU fire detection has detect fire.
- 15.After the APU EMER STOP pushbutton is pressed the APU fire extinguisher pushbutton illuminates indicating that ...
- A.
The extinguisher bottle is not armed.
- B.
The extinguisher bottle is armed.
- 16.When an APU fire is detected, the upper half of the button illuminates ...
- A.
White.
- B.
Red.
- 17.If a fire condition is still present and the APU emergency stop button is not pressed, the APU fire extinguisher pushbutton illuminates after ________ indicating that the extinguisher bottle is armed.
- A.
1 minute
- B.
2 minutes
- 18.On ground, the APU will automatically shut down __________ after the fire condition is present.
- A.
60 seconds
- B.
10 seconds
- 19.The forward and aft cargo compartments on the E-JETS are ...
- A.
Class A.
- B.
Class B.
- C.
Class C.
- 20._____________________ are protected by the CARGO SMOKE DETECTION SYSTEM and CARGO FIRE PROTECTION SYSTEM.
- A.
The forward cargo compartment
- B.
The aft cargo compartment
- C.
Both cargo compartments
- 21.Each cargo compartment has ________________ smoke detection system.
- A.
The same
- B.
An independent
- 22.After fire or smoke is detected in the forward cargo compartment the following actions are automatically commanded by the system:
- A.
Air circulation fan is turned off; The FWD fire extinguishing bottle is armed and; The forward cargo compartment ventilation outflow valve is commanded closed.
- B.
The AFT fire extinguishing bottle is armed.
- 23.After fire or smoke is detected in the aft cargo compartment the following action is automatically commanded by the system:
- A.
Air circulation fan is turned off; and; The forward cargo compartment ventilation outflow valve is commanded closed.
- B.
The AFT fire extinguishing bottle is armed.
- 24.The Cargo Fire Extinguishing System is comprised of:
- A.
One high-rate extinguisher bottle and; One low-rate extinguisher bottle.
- B.
Two high-rate extinguisher bottle and; Two low-rate extinguisher bottle.
- 25.Both extinguisher bottles are installed in the ______________________ and used in either forward or aft cargo compartment.
- A.
Center avionics bay
- B.
Forward avionics bay
Questions: 36 | Attempts: 2902 | Last updated: Mar 22, 2022
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Sample QuestionBoth IDGs and the APU generator are rated at _______________________ , three-phase.
Questions: 22 | Attempts: 1908 | 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.
Questions: 29 | Attempts: 1857 | 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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