A380-LEVEL III - ATA 26 Fire _ Smoke Detection

A380TECHNICAL TRAINING MANUAL

MAINTENANCE COURSE - T1 & T2 (RR / Metric)LEVEL III - ATA 26 Fire & Smoke Detection

This document must be used for training purposes only

Under no circumstances should this document be used as a reference

It will not be updated.

All rights reservedNo part of this manual may be reproduced in any form,

by photostat, microfilm, retrieval system, or any other means,without the prior written permission of AIRBUS S.A.S.

LEVEL III - ATA 26 FIRE & SMOKE DETECTIONEngine, APU & Main Landing Gear Fire ProtectionEngine, APU & Main Landing Gear Fire Protection Description (3) . .

2Engine, APU & Main Landing Gear Fire Protection System Maintenance

(3) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14Engine, APU & Main Landing Gear Fire Protection Component Location

(3) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18Cabin & Cargo Compartment Fire ProtectionCabin & Cargo Compartment Fire Protection Description (3) . . . . . 20Avionics, Cargo Compartment, Lavatory, Cabin & Sub-Cabin

Compartment, Fire Protection System Maintenance (3) . . . . . . 32Smoke Protection Component Location (3) . . . . . . . . . . . . . . . . . . . 36


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ENGINE, APU & MAIN LANDING GEAR FIRE PROTECTION DESCRIPTION (3)General

The Fire Protection System includes the Fire Detection and the FireExtinguishing systems.Three fire zones are fire detected on each engine and one on each pylon.The APU compartment and the Main Landing Gear Bay are also firedetected.A fire extinguishing system is installed for the engine and the APU. Forthe Main Landing Gear Bay any extinguishing is installed.A single Fire Detection Unit (FDU) is dedicated for the whole: engine,APU and Main Landing Gear Bay fire extinguishing system.


ENGINE, APU & MAIN LANDING GEAR FIRE PROTECTIONDESCRIPTION (3)

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GENERAL



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ENGINE, APU & MAIN LANDING GEAR FIRE PROTECTION DESCRIPTION (3)Fire Detection

For each engine, the protected zones are:o the fan zone (zone 1) protected by two pairs of fire detectors,o the intermediate compressor zone (zone 2) protected by one pair of firedetectors,o the core zone (zone 3) protected by one pair of fire detectors,o and the pylon zone protected by one pair of fire detectors installedabove the combustion chamberThe APU compartment is protected by one pair of fire detectors installedin parallel and connected to a dual loop.For the Main Landing Gear Bay, the protected zones are:o the right WLG bay protected by one pair of fire detectors,o the left WLG bay protected by one pair of fire detectors,o In the BLG bay, the right and left hand sides are each one protected bya pair of fire detectors.The detectors use electro-pneumatic technology.The smoke detector has a sensing element and a responder assembly.The responder assembly is made of stainless steel body. It contains achamber connected to two pressure switches: an alarm switch and anintegrity switch. The position of the two pressure switches generates threestates: normal, fault or fire states.The sensing element is made of hydrogen charged core, surrounded byhelium gas and soldered by an end cap. This gas reacts according to theideal gas law.



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FIRE DETECTION



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ENGINE, APU & MAIN LANDING GEAR FIRE PROTECTION DESCRIPTION (3)Fire Detection (continued)

Smoke DetectorsIn NORMAL STATE, the INTEGRITY switch is closed and theALARM switch is open.In ALARM STATE:The effect of an average temperature expands the helium (inert) gas,which in turn closes the ALARM switch,or the effect of heat caused by a flame or hot gas, releases core (active)gas from the hybrid core, which in turn closes the ALARM switch.In both cases, the detector sends a fire signal.In FAULT STATE:In the event of gas pressure loss (pipe fracture or cut off due to atorching flame), the INTEGRITY switch opens and generates a faultsignal.



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FIRE DETECTION - SMOKE DETECTORS



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Loops and Conversion ModuleFor engine, APU and MLG bay fire detection, two continuous loopsare installed in parallel and operate according to an AND logic.Each fire detection loop continuously monitored:o five fire detectors for one engine,o one fire detector for the APU,o four fire detectors for the MLG bayEach loop is connected to a separate channel in the CM: Loop A onChannel A and Loop B on Channel B.In the vicinity of each area, a conversion module is installed to digitizethe information of each detector, and transmit it to the Fire detectionUnit.A Conversion Module (CM) per Engine is installed in the fireprotection system.One is installed for the APU and one for the Main Landing Gear bay.Each Conversion Module receive signal from each fire detector.The CM has two channels A and B.Fire detector on loop A is related to channel AFire detector on loop B is related to channel B.Each channel also receives signals from the Temperature CompensatedPressure Switch (TCPS) of fire extinguisher bottle.Each channel of the CM works independently.Its internal function is to convert ANALOG to DIGITAL values:- analog signal from the responder of the detector,- discrete signal from the pressure switch of extinguisher bottle.Each channel communicates only with its associated FDU Operationalcards through a CAN Bus link.



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FIRE DETECTION - LOOPS AND CONVERSION MODULE



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Fire Detection UnitThe Fire Detection Unit is located in the Main Avionics bay.The FDU is composed by four independent Operational cards (OPcard) or channelsAnd BITE Card dedicated to BITE functions composed the FDU.This BITE card is connected to each OP cards.The FDU receives inputs from:o the CM through CAN Bus,o the Landing Gear Extension/Retraction System (LGERS),o the Push-Button Test of the ENGine/FIRE Integrated Control Panelo the Engine and APU fire extinguisher bottles.The FDU processes data delivered by the Conversion Module throughCAN Bus.It monitors the fire detection system.The FDU monitors the bottle (bottle pressure and bottle filament state,power supply, state of fire handle and of the agent)The FDU activates the extinguishing system automatically if a fireoccurs for APU when the aircraft is on ground.The output signals are generated and sent to :- The FWS in ARINC 429,- The ENGine/FIRE ICP with discrete signals,- The ENGine/MASTER Control Panel with discrete signals.The FDU Operational cards (OP card) monitor:For OP card#1 detection for ENGine 1 and 4 and APU on Loop A,For OP card#2 detection for ENGine 1 and 2 and APU on Loop B,For OP card#3 detection for ENGine 2 and 3 and MLG bay on LoopA,For OP card#4 detection for ENGine 3 and 4 and MLG bay on LoopB.The FDU Bite is a standard B, type 1

Its function is to monitor each Operational Card of the FDU andprocess the result of this monitoring.Then the BITE card builds failure messages, memorized and sendsthis failure message to the CMS through the SCI.It also activates the Interactive Test and the Operational test on Engine,APU and MLG bay when action is initiated by pressing the testPushbuttons on ICP.



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FIRE DETECTION - FIRE DETECTION UNIT



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ENGINE, APU & MAIN LANDING GEAR FIRE PROTECTION DESCRIPTION (3)Fire Extinguishing

The fire extinguishing system is composed:For the engine, of:o Two bottles on the rear secondary structure of each engine pylon,o An extinguishing distribution line system from the bottles to the Zone1 (Fan compartment), the Zone 2 (Intermediate Compressor Compartment)and the Zone 3 (Core Compartment) of the engine,o The extinguishing agent is sprayed out on this zone by extinguishernozzles.For the APU, of:- A single bottle installed behind the firewall,- A distribution pipe,- And extinguisher nozzle to spray out the extinguishing agent.The extinguisher bottle is composed of:A spherical container witch contains the Halon, an extinguishing agent,a fill fitting, mounting lugs and handles.The discharge head position on bottle 1 is different from that on bottle2.The cartridge is an electro-pyrotechnic element, which is fired by twofilaments. The percussion breaks the rupture disk, then the extinguishingagent can flow through the discharge head in the distribution system.The Temperature Compensated Pressure Switch (TCPS) monitors thepressure in the bottle, the DISCH legend is on when container isdischarged. The TCPS is connected to the CM via the FDU. The TCPSbottle 1 is linked to channel A of the CM, and for bottle 2 to channel B.The push-to-test pushbutton switch is used to do the test of the pressureswitch.



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FIRE EXTINGUISHING



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ENGINE, APU & MAIN LANDING GEAR FIRE PROTECTION SYSTEM MAINTENANCE (3)Fire Protection System Tests

The Fire Protection System (FPS) fulfills the following test:- FPS Tests- Reports- Specific functionsThese tests are launched from the OMS HMI.


ENGINE, APU & MAIN LANDING GEAR FIRE PROTECTIONSYSTEM MAINTENANCE (3)

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FIRE PROTECTION SYSTEM TESTS



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ENGINE, APU & MAIN LANDING GEAR FIRE PROTECTION SYSTEM MAINTENANCE (3)FPS menu

The FPS MENU page of the Onboard Maintenance System (OMS) givesthe following functions:Tests:. APU Functions activation. System testReports:. Detectors value/state. Fire event detector valueSpecific functions:. Bite memory dumpObey these safety precautions:

WARNING: BE CAREFUL WHEN YOU REMOVE OR INSTALLTHIS EQUIPMENT. THIS EQUIPMENT IS HEAVY(MORE THAN 12 KG (26.5 lb)) AND CAUSE INJURYAND/OR DAMAGE.BE VERY CAREFUL WHEN YOU DO THISPROCEDURE. THE BOTTLE CAN FIREACCIDENTALLY AND CAUSE IMPORTANT INJURYTO PERSONS WHO ARE IN THE AREA ADJACENTTO THE FIRE EXTINGUISHER BOTTLE.MAKE SURE THAT THERE IS A GOOD FLOW OF AIRTHROUGH THE WORK AREA.FUMES FROM A DISCHARGED FIRE EXTINGUISHERBOTTLE CAN CAUSE INJURY TO PERSONS.BE VERY CAREFUL WHEN YOU MOVE A FILLEDFIRE EXTINGUISHER BOTTLE. A HEAVY SHOCKCAN CAUSE UNWANTED DISCHARGE AND INJURYTO PERSONS.

MAKE SURE THAT THE SAFETY DEVICES AND THEWARNING NOTICES ARE IN POSITION BEFORE YOUSTART A TASK ON OR NEAR :- THE FLIGHT CONTROLS- THE FLIGHT CONTROL SURFACES- THE LANDING GEAR AND RELATED DOORS- COMPONENTS THAT MOVE.MOVEMENT OF COMPONENTS CAN KILL OR CAUSEINJURY TO PERSONS AND CAN CAUSE DAMAGE.MAKE SURE THAT THE TRAVEL RANGES OF THEFLIGHT CONTROL SURFACES ARE CLEAR.MOVEMENT OF THE FLIGHT CONTROL SURFACESCAN CAUSE INJURY TO PERSONS AND DAMAGETO THE AIRCRAFT OR EQUIPMENT.



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FPS MENU



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ENGINE, APU & MAIN LANDING GEAR FIRE PROTECTION COMPONENT LOCATION (3)


ENGINE, APU & MAIN LANDING GEAR FIRE PROTECTIONCOMPONENT LOCATION (3)

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Landing Gear Fire Detection

A/C Zone 124A/C Zone 199A/C Zone 143A/C Zone 144A/C Zone 145A/C Zone 146

Engine Fire Detection

A/C ZONE 410A/C Zone 412A/C Zone 413A/C Zone 451A/C Zone 455A/C Zone 420A/C Zone 422A/C Zone 423A/C Zone 461A/C Zone 465A/C Zone 430A/C Zone 432A/C Zone 433A/C Zone 471

A/C Zone 475A/C Zone 440A/C Zone 442A/C Zone 443A/C Zone 481A/C Zone 485A/C Zone 000

Engine Fire Extinguishing

A/C ZONE 450A/C Zone 460A/C Zone 470A/C Zone 480

APU Fire Detection Components

A/C Zone 315A/C Zone 152

APU Fire Extinguishing

A/C Zone 313


ENGINE, APU & MAIN LANDING GEAR FIRE PROTECTIONCOMPONENT LOCATION (3)

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CABIN & CARGO COMPARTMENT FIRE PROTECTION DESCRIPTION (3)General

In non-customized area, the smoke detection is done in the Cargocompartment, Avionics compartment and Additional ElectronicCompartment.The smoke detectors in this area, communicate over CAN buses with theCIDS-SDF of the CIDS Directors.In customized area, the smoke detection is done in the lavatory, in thecabin Sub-compartment and in the crew rest compartment.The smoke detectors in this area communicate over CAN buses with theDecoder Encoder Units type B (DEU-B). The DEU-B are linked to theCIDS Directors by Ethernet data buses.A fire extinguishing system is installed in the cargo compartment, in thecrew rest compartment and in the lavatory.The portable extinguisher bottle is installed in the cabin for fireextinguishing in cabin, cabin sub-compartment and crew restcompartment.The FAP is the main user interface with the CIDS.The CARGO SMOKE panel activates the cargo fire extinguishing.


CABIN & CARGO COMPARTMENT FIRE PROTECTIONDESCRIPTION (3)

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CABIN & CARGO COMPARTMENT FIRE PROTECTION DESCRIPTION (3)Smoke Detectors

In the pressurized area, there are two types of smoke detectors: the ducttype and the ambient type.Duct type smoke detectors are installed in the Avionics compartment, inthe emergency compartment, in the IFE compartment and in theAdditional Electronic compartment.Ambient type smoke detectors are installed in the cargo compartment,in the lavatory, in the cabin sub-compartment and in the crew restcompartment.

Duct Type Smoke DetectorThe duct type smoke detector is installed on the air duct.The photoelectric cell senses airborne combustion particles, transportedby the air ducted. This detector is installed housing with an air inletand air outlet.

Ambient Type Smoke DetectorThis type of smoke detector is primarily used in monitored and closedareas.

An optical cell senses obscuration resulting in presence of airborneparticles.These airborne particles enter through the open housing.

Smoke Detector DescriptionThese two types of smoke detector cells are based on the principle ofreverse scattered light.Each detector includes a light source, a labyrinth and a photocellarranged in a horizontal plane so that the photocell cannot receivelight.But when there is smoke, the smoke particles reflect and diffuse partof the light beam.The smoke detector has two chambers:-the reference chamber

-the measurement chamber.The reference chamber manages the differential pressure and thetemperature differences and makes sure that the detectors operate onground and in flight with the same level of sensitivity.The measurement chamber compares the analog voltage of the sensorwith the different levels of the threshold (fault, normal and smoke).



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SMOKE DETECTORS - DUCT TYPE SMOKE DETECTOR ... SMOKE DETECTOR DESCRIPTION



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CABIN & CARGO COMPARTMENT FIRE PROTECTION DESCRIPTION (3)Smoke Detection Function (CIDS DIRECTOR)The directors of the CIDS integrate a Smoke Detection Function (SDF),which is an independent hardware part.The CIDS-SDF is a segregated hard and software platform within theARINC 600 CIDS Director.An AFDX interface gives the primary communication to other aircraftsystems.The DEU-Bs are linked with the Directors by Ethernet data busses called"Middle lines"The DEU-B is a LRU, which operates like a remote data concentrator,It manages and power supplies up to 8 smoke detectors.A dedicated fault and alarm outputs as well as a reset input enable localindication and control of smoke detection functions.The FAP is the main user interface with the CIDS.The sub-panel of the FAP has the SMOKE RESET functional areas toreset the audio smoke alert.The MINI-FAP has in basic pages the smoke detection item to visualizethe location of the detection and a SMOKE RESET hard key.The Fire Extinguishing System (FES) panel is used to control and indicatethe fire extinguishing procedure.It is installed in the stair house.The FES panel is a human interface to command ignition of the fireextinguishing bottle and give indications on the status of the fireextinguishing.The Fire Extinguishing Data Converter (FEDC) controls and monitorsthe condition of each installed fire-extinguishing bottle and detects theextinguishing agent pressure inside.It operates on the principle of an interface translator between discretesignals and CAN bus.The FEDC is a remote data concentrator, monitoring the pressure switchesand the squib circuit of the Fire Extinguishing System.It ignites all squibs of the agent bottle.



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SMOKE DETECTION FUNCTION (CIDS DIRECTOR)



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CABIN & CARGO COMPARTMENT FIRE PROTECTION DESCRIPTION (3)Fire Extinguishing System

Cargo Fire ExtinguishingThe cargo fire extinguishing system has three fire extinguishing bottleslocated in the FWD cargo compartment connected to a flow meteringequipment and to a diverter valve.Within the three fire extinguisher bottles, one is high rated, and thetwo other are flow-metered.The bottles, made of stainless steel, contain the fire-extinguishingagent, halon 1301 and are hermetically sealed and refillable.Each bottle has:- a Temperature-Compensated Pressure Switch (TCPS),- a fill and a safety relief valve.Each discharge head has:- an electrically operated cartridge,Each cartridge has two squibs (squib A and squib B) receiving aseparate power supply (HOT BUS and DC BUS power).When the electrical power supplies both squibs, the cartridge explodesand ruptures the metal diaphragm in the discharge outlet.Extinguishing agent flows through the discharge head into distributionpipes.The diverter valve has two outlets to direct the Halon via piping onefor the FWD and the other one for the AFT/BULK CargoCompartment.Each outlet is sealed with a plug. A pyrotechnical cartridge opens it.The Flow metering equipment regulates the outflow of the secondand the third bottle, maintaining the extinguishing agent concentrationto a minimal time of 240 minutes.It includes a water absorbing filter element, a solid particle filterelement, a pressure switch, a pressure reducer, a restrictor and a checkvalve.Four nozzles are located in the FWD cargo compartment and five arein the AFT/BULK cargo compartment.

There are installed on the ceiling in the same cavity and between thetwo smoke detectors, and are protected by a metallic grid.



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FIRE EXTINGUISHING SYSTEM - CARGO FIRE EXTINGUISHING



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CABIN & CARGO COMPARTMENT FIRE PROTECTION DESCRIPTION (3)Fire Extinguishing System (continued)

Lavatory Fire ExtinguishingA fire extinguisher bottle is installed above the waste bin in eachlavatory.If a fire occurs in the waste bin, the fire extinguishing operatesautomatically.The lavatory fire extinguishers operate independently of other systems.Each fire extinguisher has:- a spherical container made of brass,- an identification label bonded to the container with the followinginformation: part number, serial number, date of manufacture, typeof extinguisher agent, and total weight of the bottle.- a fill port with a fill valve, to re-charge the container of extinguisheragent,- mounting bracket,- a discharge tube with a fusible plug, which melts to let the agentflowing into the waste bin when the temperature increases toapproximately 77C (170.60 Deg. F)- a pressure gage, installed on the fill port indicates if the container ischarged or empty.



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FIRE EXTINGUISHING SYSTEM - LAVATORY FIRE EXTINGUISHING



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CABIN & CARGO COMPARTMENT FIRE PROTECTION DESCRIPTION (3)Fire Extinguishing System (continued)

Cabin, Cabin Crew Rest Compartment Fire ExtinguishingIn the Cabin, portable fire extinguisher bottles are installed.This bottle contains the pressurized extinguisher agent, a bondedinformation label gives the necessary information to operate and checkthe extinguisher,The operating head is an operating lever, with a carrying handle, avalve assembly, a safety device, a nozzle and an indicator disc toindicate the bottle pressure.In the Cabin Crew Rest Compartment, if a fire is not controllable byportable fire extinguisher and in case of any risk, the crew has to fightthe fire through the Fire Extinguishing System (FES).The FES panel installed in the stair house activates and controls theextinguishing system.Two fire extinguishing bottles are located in the AFT lower deckcargo compartmentSpray nozzles are located in the ceiling of the Cabin Crew Restcompartment to spray the fire extinguishing agent in the compartment.Flow metering equipment regulates the flow of the second bottle.



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FIRE EXTINGUISHING SYSTEM - CABIN, CABIN CREW REST COMPARTMENT FIRE EXTINGUISHING



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AVIONICS, CARGO COMPARTMENT, LAVATORY, CABIN & SUB-CABIN COMPARTMENT, FIREPROTECTION SYSTEM MAINTENANCE (3)Smoke Detection Function Tests

The Smoke Detection Function (SDF) provides the following test:- SDF Tests- Reports- Specific functions.These tests are launched from the OMS HMI.


AVIONICS, CARGO COMPARTMENT, LAVATORY, CABIN &SUB-CABIN COMPARTMENT, FIRE PROTECTION SYSTEM

MAINTENANCE (3)

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SMOKE DETECTION FUNCTION TESTS



MAINTENANCE (3)

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AVIONICS, CARGO COMPARTMENT, LAVATORY, CABIN & SUB-CABIN COMPARTMENT, FIREPROTECTION SYSTEM MAINTENANCE (3)SDF Menu

The SDF MENU page of the Onboard Maintenance System (OMS) givesthe following functions:Tests:. Smoke warn test. Fire extinguishing tests. Safety test. System test. Automatic safety test only for display purposeReports. Status page for pin programming. Smoke warnings report. Automatic recoveries report. HMI ReportSpecific functions. Time since last safety test

WARNING: BE CAREFUL WHEN YOU REMOVE OR INSTALLTHIS EQUIPMENT. THIS EQUIPMENT IS HEAVY(MORE THAN 12 KG (26.5 lb)) AND CAUSE INJURYAND/OR DAMAGE.BE VERY CAREFUL WHEN YOU DO THISPROCEDURE. THE BOTTLE CAN FIREACCIDENTALLY AND CAUSE IMPORTANT INJURYTO PERSONS WHO ARE IN THE AREA ADJACENTTO THE FIRE EXTINGUISHER BOTTLE.MAKE SURE THAT THERE IS A GOOD FLOW OF AIRTHROUGH THE WORK AREA.FUMES FROM A DISCHARGED FIRE EXTINGUISHERBOTTLE CAN CAUSE INJURY TO PERSONS.

BE VERY CAREFUL WHEN YOU MOVE A FILLEDFIRE EXTINGUISHER BOTTLE. A HEAVY SHOCKCAN CAUSE UNWANTED DISCHARGE AND INJURYTO PERSONS.MAKE SURE THAT THE SAFETY DEVICES AND THEWARNING NOTICES ARE IN POSITION BEFORE YOUSTART A TASK ON OR NEAR:- THE FLIGHT CONTROLS- THE FLIGHT CONTROL SURFACES- THE LANDING GEAR AND RELATED DOORS- COMPONENTS THAT MOVE.MOVEMENT OF COMPONENTS CAN KILL OR CAUSEINJURY TO PERSONS AND CAN CAUSE DAMAGE.MAKE SURE THAT THE TRAVEL RANGES OF THEFLIGHT CONTROL SURFACES ARE CLEAR.MOVEMENT OF THE FLIGHT CONTROL SURFACESCAN CAUSE INJURY TO PERSONS AND DAMAGETO THE AIRCRAFT OR EQUIPMENT.



MAINTENANCE (3)

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SDF MENU



MAINTENANCE (3)

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SMOKE PROTECTION COMPONENT LOCATION (3)Avionics Bay Smoke Detection

A/C Zone 292A/C Zone 120A/C Zone 260

Cargo Bay Smoke Detection

A/C Zone 131A/C Zone 132A/C Zone 151A/C Zone 152A/C Zone 161A/C Zone 162

Cargo Bay Fire Extinguishing

A/C Zone 131

Crew Rest Smoke Detection

A/C Zone 150A/C Zone 222

Crew Rest Compartment Fire Extinguishing

A/C Zone 151

Portable Fire Extinguishing

A/C Zone 210MAINTENANCE COURSE - T1 & T2 (RR / Metric)LEVEL III - ATA 26 Fire & Smoke Detection

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AIRBUS S.A.S.31707 BLAGNAC cedex, FRANCE

STMREFERENCE L0Y06082

MARCH 2006PRINTED IN FRANCEAIRBUS S.A.S. 2006

ALL RIGHTS RESERVED

AN EADS JOINT COMPANYWITH BAE SYSTEMS

Table of ContentsEngine, APU & Main Landing Gear Fire ProtectionEngine, APU & Main Landing Gear Fire Protection Description (3)GeneralFire DetectionSmoke DetectorsLoops and Conversion ModuleFire Detection Unit

Fire Extinguishing

Engine, APU & Main Landing Gear Fire Protection System Maintenance (3)Fire Protection System TestsFPS menu

Engine, APU & Main Landing Gear Fire Protection Component Location (3)Landing Gear Fire DetectionA/C Zone 124A/C Zone 199A/C Zone 143A/C Zone 144A/C Zone 145A/C Zone 146

Engine Fire DetectionA/C ZONE 410A/C Zone 412A/C Zone 413A/C Zone 451A/C Zone 455A/C Zone 420A/C Zone 422A/C Zone 423A/C Zone 461A/C Zone 465A/C Zone 430A/C Zone 432A/C Zone 433A/C Zone 471A/C Zone 475A/C Zone 440A/C Zone 442A/C Zone 443A/C Zone 481A/C Zone 485A/C Zone 000

Engine Fire ExtinguishingA/C ZONE 450A/C Zone 460A/C Zone 470A/C Zone 480

APU Fire Detection ComponentsA/C Zone 315A/C Zone 152

APU Fire ExtinguishingA/C Zone 313

Cabin & Cargo Compartment Fire ProtectionCabin & Cargo Compartment Fire Protection Description (3)GeneralSmoke DetectorsDuct Type Smoke DetectorAmbient Type Smoke DetectorSmoke Detector Description

Smoke Detection Function (CIDS DIRECTOR)Fire Extinguishing SystemCargo Fire ExtinguishingLavatory Fire ExtinguishingCabin, Cabin Crew Rest Compartment Fire Extinguishing

Avionics, Cargo Compartment, Lavatory, Cabin & Sub-Cabin Compartment, Fire Protection System Maintenance (3)Smoke Detection Function TestsSDF Menu

Smoke Protection Component Location (3)Avionics Bay Smoke DetectionA/C Zone 292A/C Zone 120A/C Zone 260

Cargo Bay Smoke DetectionA/C Zone 131A/C Zone 132A/C Zone 151A/C Zone 152A/C Zone 161A/C Zone 162

Cargo Bay Fire ExtinguishingA/C Zone 131

Crew Rest Smoke DetectionA/C Zone 150A/C Zone 222

Crew Rest Compartment Fire ExtinguishingA/C Zone 151

Portable Fire ExtinguishingA/C Zone 210

Documents

A380-LEVEL III - ATA 26 Fire _ Smoke Detection