#1. The avionics compartment is the only area where there is no fire extinguishing system installed.
#2. Engine fire loops are installed in the
#3. If a break in both engine fire loops occurs within _____ seconds of each other a _____ will occur.
#4. The aircraft has dual fire detector loops to ensure that a fault in one fire loop will not affect fire detection capabilities.
#5. If there is an APU fire in flight the APU:
#6. Fire protection for the cargo compartments includes:
#7. The engine extinguishing agent switch is armed when:
#8. The APU test switch on the APU Auto Exting panel when pushed will
#9. When the APU FIRE SWITCH is released out:
#10. The GEN 1 LINE smoke light indicates:
#11. Can the APU FIRE test be performed using battery power only?’
#12. When the aircraft is on the ground and the APU is started on battery power only, is fire protection available?
#13. How many fire extinguishing bottles are available for fighting an APU fire?
#14. APU fire detection is accomplished by:
#15. Engine heat sensing are located in pylon nacelle, engine core and fan section.
#16. After an APU fire has been detected how long will the chime continue to sound?
#17. STATUS page: INOP SYS indicates “ENG1 LOOP B”.
#18. Which of the following have automatic fire extinguishing systems?
#19. The aft cargo compartment smoke detection system consists of:
#20. If an engine fire is detected, when will the pedestal mounted red FIRE annunciator light extinguish?
#21. How long will the red APU FIRE pb on the overhead be illuminated?
#22. With reference to cargo compartment fire extinguishing, which statement is true?
#23. Should you lose both loops or FDU, fire detection is no longer available for the respective engine or the APU
#24. What is indicated by a missing red APU thermal plug during an exterior preflight?
#25. If an engine fire is detected, when will the guarded red ENG FIRE push button light extinguish?
#26. In the event a lavatory smoke detector detects smoke:
#27. Are there any warnings to alert ground personnel when there is a fire in the APU compartment?
#28. What systems are affected when the guarded red ENGINE FIRE push button is pushed and released?
#29. The avionics smoke detection system consists of the following:
#30. DISCH light on either the engine or APU fire agent switches indicates:
#31. Will an APU fire test shut down the APU?
#32. Illumination of the GEN 1 LINE SMOKE light indicates:
#33. In the event an aft cargo compartment smoke detector detects smoke:
#34. How many halon fire extinguishing cylinders are there per engine?
#35. The APU provides for automatic fire extinguishing:
#36. You have detected avionics smoke. You have selected the GEN 1 LINE push button off and the RAT has been deployed. Generator 2 has been removed from the system. Which of the following is TRUE?
#37. After depressing the CARGO SMOKE TEST push button once, a satisfactory test of the aft cargo compartment smoke detector consist of:
#38. In conjunction with illumination of the GEN 1 LINE SMOKE light and MASTER CAUT light:
#39. If you perform the APU FIRE TEST with only DC power available, you get the MASTER WARN on the ECAM.
#40. In the event an aft cargo compartment smoke detector detects smoke:
#41. How does the APU fire test on battery power differ from the APU fire test with all busses powered?
#42. During the walk-around, you have to check that the APU Fire extinguisher overpressure indication (green disc) is in place. This is an indication that the fire bottle has not been discharged.
#43. The AFT SMOKE light closes the aft cargo inlet and outlet isolation valves and shuts off the aft cargo extraction fan.
#44. Each lavatory is equipped with:
#45. Each engine nacelle and pylon area is equipped with:
#46. In addition to the CRC and red MASTER WARN light, a good engine fire test will display which of the following (AC power available)?
#47. If an APU fire is detected on the ground, the APU shuts down automatically and the agent is discharged ______ after the warning is activated.
#48. The aircraft has dual fire detector loops for the engines and APU to ensure that a fault in one fire loop will not affect fire detection capabilities.
#49. Engine fire loops are installed in the:
#50. If a break in both engine fire loops occurs within 5 seconds of each other, a _____ will occur.
#51. The engine fire extinguishing squib is armed when:
#52. STATUS page: INOP SYS indicates ‘ENG1 LOOP B’.
#53. If an engine fire is detected, when will the pedestal mounted red FIRE annunciator light extinguish?
#54. If an engine fire is detected, when will the guarded red ENG FIRE push button light extinguish?
#55. What systems are affected when the guarded red ENGINE FIRE push button is pushed and released?
#56. In addition to the CRC and red MASTER WARN light, a good engine fire test will display which of the following (AC power available)?
#57. How many fire extinguishing bottlse are there per engine?
#58. If there is an APU fire in flight the APU:
#59. When the APU FIRE P/B SWITCH is released out:
#60. DISCH light on either the engine or APU AGENT P/B switches indicates:
#61. Can the APU FIRE test be performed using battery power only?
#62. The APU and engine FIRE test can be performed with battery power only.
#63. When the aircraft is on the ground and the APU is started on battery power only, is fire protection available?
#64. How many fire extinguishing bottles are available for fighting an APU fire?
#65. APU fire detection is accomplished by:
#66. Should you loose both loops or Fire Detection Unit, fire detection is no longer available for the respective engine.
#67. Are there any warnings to alert ground personnel when there is a fire in the APU compartment?
#68. Will an APU fire test shut down the APU?
#69. The APU provides for automatic fire extinguishing:
#70. If you perform the APU FIRE TEST with only DC power available, you get the MASTER WARN
#71. How does the APU fire test on battery power differ from the APU fire test with all busses powered?
#72. During the walk-around, you have to check that the APU Fire extinguisher overpressure indication (green disc) is in place. This is an indication that the fire bottle has not been discharged.
#73. What is indicated by a missing red APU thermal plug during an exterior preflight?
#74. If an APU fire is detected on the ground, the APU shuts down automatically and the agent is discharged ______ after the warning is activated.
#75. Illumination of the GEN 1 LINE SMOKE light indicates:
#76. In case of Avionics Smoke, in conjunction with illumination of the GEN 1 LINE SMOKE light and MASTER CAUTION light:
#77. The avionics compartment is the only area where there is no fire extinguishing system installed.
#78. You have detected avionics smoke. You have selected the GEN 1 LINE push button off and the RAT has been deployed. Generator 2 has been removed from the system. Which of the following is TRUE?
#79. Fire protection for the cargo compartments includes:
#80. In the event an aft cargo compartment smoke detector detects smoke:
#81. Which of the following have automatic fire extinguishing systems?
#82. The APU test switch on the APU Auto Exting panel when pushed will:
#83. When smoke is detected in the ventilation extraction duct:
#84. With reference to the cargo compartment fire extinguishing system, which statement is true?
#85. As regards SMOKE in Cargo appearing on ground with Cargo Doors closed:
#86. Select correct statements for SMOKE warning in FWD Cargo compartment. 1. When the FWD SMOKE light comes on, the flight crew selects AGENT 1 with the FWD toggle switch 2. 60 min after the discharge of the first bottle, the AGENT 2 DISCH light appears. 3. AGENT 2 DISCH light indicates that the flight crew has to discharge AGENT 2 to maintain the required extinguishant concentration. 4. AGENT 2 DISCH light goes off, when the Agent 2 squib is ignited. 5. Bottle 2 takes approximately 90 min to completely discharge & is controlled by a
