Fire Protection Flashcards
What does the fire and smoke protection system include?
- Fire and overheat detection for the engines and APU
- Smoke detection for the cargo compartments, lavatories, and avionics bay
- Fire extinguishing for the cargo compartments, engines, APU, and lavatories
- Portable fire extinguishers in the cockpit and cabin areas.
What are the components of the fire and overheat detection system for the engines and APU?
Two identical detection loops (A and B) mounted in parallel and a Fire Detection Unit (FDU).
What does each fire detection loop consist of?
- Three or four engine fire sensing elements in the pylon nacelle, engine core, and engine fan section
- One fire sensing element in the APU compartment.
What happens when a sensing element is subjected to heat?
It sends a signal to the Fire Detection Unit (FDU).
What triggers the fire warning system?
When loops A and B detect temperature above a preset level.
True or False: A fault in one detection loop affects the warning system.
False
Where are the portable fire extinguishers located in the aircraft?
In the cockpit and cabin areas.
What is the role of the Fire Detection Unit (FDU)?
To receive signals from the fire sensing elements.
How does the fire detection system ensure continued protection if one loop fails?
The unaffected loop still protects the aircraft.
What is the function of the fire extinguisher bottles in engines?
Each engine has two fire extinguisher bottles with electrically-operated squibs to discharge their agents.
How does the flight crew control the fire extinguisher bottles in the engines?
The flight crew controls the discharge from the FIRE panel in the cockpit.
What happens when an APU fire is detected on the ground?
The APU automatically shuts down and the extinguisher bottle discharges automatically.
What triggers a fire warning?
A fire warning appears if:
* Both loops A and B send a fire signal
* One loop sends a fire signal and the other one is failed
* Breaks occur in both loops within 5 s of each other
* A test is performed on the FIRE panel.
What does a loop-fault caution indicate?
A loop-fault caution appears if the associated loop is failed.
What actions are performed when the ENG 1(2) FIRE PB-SW is pushed?
The following occurs:
* Silences the aural fire warning
* Arms the fire extinguisher squibs
* Closes the low-pressure fuel valve
* Closes the hydraulic fire shut off valve
* Closes the engine bleed valve
* Closes the pack flow control valve
* Cuts off the FADEC power supply
* Deactivates the IDG.
What indication is given when the ENG 1(2) FIRE warning is activated?
On ENG 1(2) FIRE PB-SW
The red lights come on, regardless of the PB-SW position.
When does the AGENT 1(2) PB is activated?
When flight crew releases the ENG 1(2) FIRE pb-sw.
What does a brief push on the AGENT pb do?
It discharges the corresponding fire agent.
What is indicated by the ‘SQUIB’ light?
‘SQUIB’ comes on white when the flight crew releases the ENG 1(2) FIRE pb-sw to help identify the activated AGENT pb.
What does the ‘DISCH’ light signify?
‘DISCH’ comes on amber when the corresponding fire extinguisher bottle has lost pressure.
What does the ENG 1(2) FIRE TEST PB do?
It tests the operation of the fire detection and extinguishing system for ENG 1(2).
What are the indications when the ENG 1(2) FIRE TEST PB is pressed?
The following occurs:
* A CRC sounds
* The MASTER WARNING lights flash
* ENG FIRE warning appears on ECAM
* ENG 1(2) FIRE pb-sw lights up red
* SQUIB lights come on white if discharge supplies are available
* DISCH lights come on amber.
What does the APU FIRE PB-SW do when pressed?
It performs the following:
* Shuts down the APU
* Silences the aural warning
* Arms the squib on the APU fire extinguisher
* Closes the low-pressure fuel valve
* Shuts off the APU fuel pump
* Closes the APU bleed valve and X bleed valve
* Deactivates the APU generator.
What does the APU FIRE TEST PB do?
It tests the operation of the APU fire detection and extinguishing system.