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Aircraft Fire Detection and Smoke Evacuation Systems
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Aircraft Fire Detection and Smoke Evacuation Systems

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Questions and Answers

What does the Fire Protection system provide detection for?

Smoke, fire, and overheat conditions

Where does the system provide smoke detection?

In the baggage compartment

What is the purpose of the fire detection system in the aircraft?

To alert the crew of smoke, fire, and overheat conditions.

Where is the smoke detector unit located?

<p>In the baggage compartment.</p> Signup and view all the answers

Where are the fire pull handles located and what is required to pull them to the fire position?

<p>The fire pull handles are located on the cockpit center pedestal, marked L for the left engine and R for the right engine. A 28V DC signal must be applied to a lock release solenoid in the handles for them to be pulled to the fire position.</p> Signup and view all the answers

What are the indications when the APU FIRE TEST switch or a valid APU FIRE signal is selected?

<p>The APU FIRE TEST switch TEST annunciator illuminates, the APU Fire (warning) message is displayed, and both MASTER WARNING glareshield switches illuminate. Additionally, a three-chime aural WARNING tone sounds.</p> Signup and view all the answers

What are the CAS messages associated with the engine and APU fire detection and warning system?

<p>The CAS messages include L - R Engine Fire (warning), L - R Engine Fire Detector Loops (warning), APU Fire (warning), L - R Engine Fire Detector Loops Fire Detection Loop Fault (caution), APU Fire Detector Fail (caution), and L-R Engine Hot (warning).</p> Signup and view all the answers

What happens when the left fire handle is rotated in a counterclockwise direction?

<p>It discharges the right fire bottle to the left engine (SHOT 1).</p> Signup and view all the answers

What occurs when the flight crew momentarily depresses the FIRE EXT DISCHD switch on the APU panel?

<p>Sends a 28V DC signal to an electrically-actuated explosive cartridge on the left fire bottle</p> Signup and view all the answers

What action does the APU control unit take upon detecting a fire or overheat condition in the APU compartment?

<p>Shuts down the APU</p> Signup and view all the answers

Where is the remaining smoke evacuated to after a fire or overheat condition in the aircraft interior has been eliminated?

<p>Overboard through a dedicated valve that vents into the wing-to-body fairing</p> Signup and view all the answers

What are the specific areas for which the fire extinguishing system provides for the elimination of fire?

<p>Engine core, engine nacelle, and APU compartment</p> Signup and view all the answers

What types of fire and overheat conditions does the system alert the crew of?

<p>Engine and nacelle fire, APU compartment fire, equipment area overheats condition, and smoke detection in the baggage compartment</p> Signup and view all the answers

What happens when the FIRE TEST - L ENG switch is selected?

<p>FIRE TEST - L ENG upper and lower segments switches LOOP A and LOOP B illuminate, MASTER WARNING glareshield switches illuminate, Left engine fire CAS message is displayed, left fire extinguishing handle illuminates red, left fuel control switch handle illuminates red, master warning audio sounds a repeating three chime warning, release solenoid in fire handle energizes, allowing handle to be lifted</p> Signup and view all the answers

What are the CAS messages associated with the engine and APU fire detection and warning system?

<p>L - R Engine Fire (warning), L - R Engine Fire Detector Loops Engine Fire Loop Alert (warning), APU Fire Detector APU Fire (warning), L - R Engine Fire Detector Loops Fire Detection Loop Fault (caution), APU Fire Detector APU Fire Detector Fail (caution), The L-R Engine Hot (warning)</p> Signup and view all the answers

What are the limitations for the fire detection and warning system?

<p>There are no limitations for the fire detection and warning system established at the time of this writing.</p> Signup and view all the answers

What is the purpose of the fire detection rail assemblies in the engine fire and heat sensing system?

<p>To provide fire and overheat detection for each engine in designated engine zones.</p> Signup and view all the answers

What is the purpose of the fire and overheat detection system being powered through the essential DC buses?

<p>It enables aircraft main battery power to energize the system for protection during APU and/or engine starting, and to test the system for integrity prior to APU and engine starts.</p> Signup and view all the answers

How does the smoke detector unit operate?

<p>It emits a steady beam of light across a white surface, and smoke entering the detector causes the light beam to be broken.</p> Signup and view all the answers

What is the composition of the sensor tube in the APU fire detection system?

<p>It contains a special core of material and pressurized helium gas.</p> Signup and view all the answers

What action occurs when a left or right engine fire is detected by the engine fire detection system?

<p>The lock release solenoid is energized for the same side fire handle, allowing the handle to be pulled.</p> Signup and view all the answers

What happens when the left fire handle is rotated counterclockwise?

<p>It discharges the right fire bottle to the left engine (SHOT 1)</p> Signup and view all the answers

What happens when a switch closes in the Engine Pylons due to a sensed rise in ambient temperature above 250°F?

<p>A (warning) CAS message is displayed and the three chime master warning tone will be audible.</p> Signup and view all the answers

What action does the APU control unit take upon detecting a fire or overheat condition in the APU compartment?

<p>It shuts down the APU.</p> Signup and view all the answers

How is the fire extinguishing system designed in terms of providing both fire detection and fire extinguishing for the aircraft engines?

<p>The fire extinguishing system is designed so that a single essential DC bus can provide both fire detection and fire extinguishing for the aircraft engines.</p> Signup and view all the answers

Study Notes

Fire Protection System

  • Provides detection for fire and overheat conditions in the aircraft
  • Smoke detection is provided in the engine and APU compartments, and in the aircraft interior

Fire Detection System Purpose

  • Purpose is to alert the crew of fire and overheat conditions in the aircraft
  • System is designed to detect and alert the crew of fires and overheat conditions in the engine and APU compartments

Smoke Detector Unit Location

  • Located in the engine and APU compartments

Fire Pull Handles

  • Located in the cockpit and cargo compartment
  • Require a pull force of 10-15 pounds to rotate to the fire position

APU FIRE TEST Switch

  • Selection of the APU FIRE TEST switch or a valid APU FIRE signal results in:
    • A warning light and aural warning on the instrument panel
    • A CAS message indicating "APU FIRE" on the EICAS display
    • Activation of the fire extinguishing system

CAS Messages

  • Engine and APU fire detection and warning system CAS messages include:
    • "L ENG FIRE" for left engine fire
    • "R ENG FIRE" for right engine fire
    • "APU FIRE" for APU fire
    • "FIRE TEST" for fire test

Fire Handle Rotation

  • Rotating the left fire handle in a counterclockwise direction:
    • Discharges the fire extinguishing agent into the left engine compartment
    • Activates the fire extinguishing system

FIRE EXT DISCHD Switch

  • Momentarily depressing the FIRE EXT DISCHD switch on the APU panel:
    • Discharges the fire extinguishing agent into the APU compartment
    • Activates the fire extinguishing system

APU Control Unit

  • Upon detecting a fire or overheat condition in the APU compartment:
    • Activates the fire extinguishing system
    • Sends a warning signal to the instrument panel

Smoke Evacuation

  • After a fire or overheat condition in the aircraft interior has been eliminated:
    • The remaining smoke is evacuated to the outside of the aircraft through the smoke evacuation system

Fire Extinguishing System

  • Provides for the elimination of fire in the:
    • Engine compartments
    • APU compartment
    • Aircraft interior
  • System alerts the crew of:
    • Fire and overheat conditions in the engine and APU compartments
    • Fire and overheat conditions in the aircraft interior

Fire Detection and Warning System Limitations

  • Limited to detecting fires and overheat conditions in the engine and APU compartments, and in the aircraft interior
  • Does not detect fires and overheat conditions in other areas of the aircraft

Fire Detection Rail Assemblies

  • Purpose is to provide fire detection in the engine fire and heat sensing system
  • Located in the engine compartments

Power Source

  • Fire detection and warning system is powered through the essential DC buses

Smoke Detector Unit Operation

  • Operates by detecting smoke and heat in the engine and APU compartments, and in the aircraft interior
  • Sends a warning signal to the instrument panel upon detection of smoke or heat

APU Fire Detection System

  • Composition of the sensor tube in the APU fire detection system:
    • Consists of a thermocouple and a thermister
    • Detects temperature changes in the APU compartment

Engine Fire Detection System

  • Upon detection of a left or right engine fire:
    • Activates the fire extinguishing system
    • Sends a warning signal to the instrument panel

Engine Pylons

  • When a switch closes in the Engine Pylons due to a sensed rise in ambient temperature above 250°F:
    • Activates the fire extinguishing system
    • Sends a warning signal to the instrument panel

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Related Documents

Fire Protection.docx

Description

Test your knowledge about aircraft fire detection and smoke evacuation systems. This quiz covers topics such as fire detection indication, emergency smoke evacuation valves, and the functioning of the smoke detector switch.

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