ATR 42 - Cabin Crew Operating Manual

5/24/2018 ATR 42 - Cabin Crew Operating Manual

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CABIN CREW OPERATING MANUAL

C.C.O.M.

AVIONS DE TRANSPORT REGIONAL

1, Allee Pierre Nadot

31712 BLAGNAC Cedex

France


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0.00 CONTENTS

0.01 LIST OF TEMPORARY REVISIONS (L.T.R)

0.02 REASON OF TEMPORARY REVISIONS (R.T.R)

0.03 SHIPPING NOTE TEMPORARY PAGES (S.N.T.P)

0.04 LIST OF EFFECTIVE TEMPORARY PAGES (L.E.T.P)

0.05 LIST OF NORMAL REVISIONS (L.N.R)

0.06 REASON OF THE REVISIONS (R.N.R)

0.07 SHIPPING NOTE NORMAL PAGES (S.N.N.P)

0.08 LIST OF EFFECTIVE NORMAL PAGES (L.E.N.P)

0.09 ORGANISATION OF THE MANUAL

0.10 LIST OF FIGURES

0.11 LIST OF TABLES

0.12 STANDARD NOMENCLATURE

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NTR DATE IN DESTROYED POSITION REMARKS

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DATE REASON FOR REVISIONS CHAPTER INVOLVED

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NREV EDITION DATE INSERTION DATE NAME

01 JAN 12 TOTAL 1stEDITION


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DATE REASON OF REVISIONS CHAPTER INVOLVED

JAN 12 Total 1stEdition, and in particular:- New CMS on ATR 600

- Correction on options offered onoxygen system

- ALL- 1.09; 3.06 ; 4.01 ; 4.02 ;4.04 ; 4.06 ; 5.01 ; 5.02 ;50.3 ; 9.02; 10.03- 4.05

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Initial edition

PART CHAPTER PAGE VALIDITY DATEPreliminary 0.00 Contents

0.01 List of temporary revisions0.02 Reason of temporary revisions0.03 Shipping note temporary pages0.04 List of effective temporary pages0.05 List of normal revisions0.06 Reason of the revisions0.07 Shipping note normal pages0.08 List of effective normal pages

0.09 Organization of the manual

0.10 List of figures

0.11 List of tables0.12 Standard nomenclature

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Aeroplane

general

1.00 Contents

1.01 Introduction1.02 Range of operation1.03 Performance1.04 Dimensions

1.05 Doors and exits / Unpressurized areas1.06 Location of cargo/baggagecompartments1.07 Danger areas1.08 Hotel mode1.09 Power

1.10 Flight controls1.11 Ice contamination

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LIST OF EFFECTIVE NORMAL PAGES

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Flight crew

compartment

2.00 Contents

2.01 General location

2.02 Flight crew seats2.03 Observer seat

2.04 Flight crew compartment door

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Cabinfamiliarisation

3.00 Contents3.01 Configuration and lay out

3.02 Passenger service units3.03 Galley

3.04 Lavatory

3.05 Cabin crew seats

3.06 Flight Attendant Panel

3.07 Tail prop ATR 72

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PART CHAPTER PAGE VALIDITY DATEAeroplane

systems

4.00 Contents

4.01 Air conditioning system/Temperaturecontrol

4.02 Smoke warning system

4.03 Lavatory automatic fire extinguisher4.04 Emergency lighting system

4.05 Oxygen system

4.06 Inflight entertainment system

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Communication 5.00 Contents5.01 Cabin signs5.02 Interphone and public address system

5.03 Passengers calls

5.04 Pilot communication hatch

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PART CHAPTER PAGE VALIDITY DATEDoors and exits 6.00 Contents

6.01 General

6.02 Flight crew compartment exit

6.03 Cabin doors and emergency exits

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Emergencyequipment

7.00 Contents7.01 MMEL/MEL7.02 Portable equipment

7.03 Fixed equipment

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Emergencyequipmentdiagrams

8.00 Contents8.01 Flight crew compartment8.02 ATR 72-500/600 cabin8.03 ATR 72-200 cabin8.04 ATR 42-500/600 cabin8.05 ATR 42-300 cabin

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Normalprocedures

9.00 Contents9.01 Introduction9.02 Cabin pre-flight checks

9.03 Phases of flight

9.04 Specific procedures

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Emergencyprocedures

10.00 Contents

10.01 Crew communication andcoordination10.02 Turbulence

10.03 fire

10.04 Decompression

10.05 Flight crew incapacitation10.06 Emergency evacuation

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The Cabin Crew Operating Manual (CCOM) provides operating cabin crew members

with information on ATR 42-300/500/600 and 72-200/500/600 technical description,procedures and performances characteristics. It may be used a as cabin crewmanual for training purposes and flight operations.

ATR 300 series refers to 42-300 aeroplaneATR 200 series refers to 72-200 aeroplaneATR 500 series refers to both 42-500 and 72-500 aeroplaneATR 600 series refers to both 42-600 and 72-600 aeroplane

The CCOM comprises:

Manual management in chapter 0

Aeroplane general in chapter 1 Flight crew compartment in chapter 2 Cabin familiarisation in chapter 3 Aeroplane systems in chapter 4 Communication in chapter 5 Doors and exits in chapter 6 Emergency equipment in chapter 7 Emergency equipment diagrams in chapter 8 Normal procedures in chapter 9 Emergency procedures in chapter 10

For any question, comment or suggestion regarding this manual we recommendusing the following e-mail:

[email protected].

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PAGINATION

1 C.C.O.M

2CABIN CREW OPERATING MANUAL3CABIN FAMILIARISATION4 CONFIGURATION AND LAYOUT

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1. ATR logo with manual type2. Manual type3. Chapter title4. Section title5. Chapter, section and page numbering6. Date of page issue or revision

A page is defined by a reference: Chapter/Section/page number Ex 6.03.2 page 8

FIGURES AND TABLES REFERENCE

All figures and tables have a reference number related to the chapter, section, pagenumber and figure or table number in the same page. Example as follow:

F5.03_P1A Figure A, chapter 5, section 3, page 1F5.03_P1B Figure B, chapter 5, section 3, page 1T9.02_P4A Table A, chapter 9, section 2, page 4

IMPORTANT: Throughout the manual, information marked within a blue framerelates to OPTIONAL equipment or systems.

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CHAPTER 1: AEROPLANE GENERAL

ATR family range of operation F1.02_P1AATR family dimensions F1.04_P2AATR 42 and 72 standard doors/Exits overview F1.05_P1AUnpressurized zones F1.05_P1BCargo/Baggage compartments F1.06_P1APropeller danger area (engines running) F1.07_P1AExhaust danger area (engines running) F1.07_P1BPropeller brake location, right engine F1.08_P1APropeller brake control switch (Flight crew compartment overhead panel) F1.08_P1BGround service BUS switches on Cabin Management System (CMS) F1.09_P1AGround service BUS switches on Flight Attendant Panel (FAP) F1.09_P2AAeroplane flight controls F1.10_P1AAnti-icing / De-icing systems F1.11_P1A

CHAPTER 2: FLIGHT CREW COMPARTMENT

Cabin to FWD cargo area door F2.01_P1AATR 42/72.600 flight crew compartment F2.01_P2ACaptains seat control levers F2.02_P1AObserver seat description F2.03_P1AObserver seat release pins location F2.03_P2AFlight crew compartment door F2.04_P1A

Flight crew compartment door locking system ON/OFF F2.04_P2AFlight crew compartment door control panel F2.04_P2BFlight crew compartment door call panel F2.04_P3AFlight crew compartment call options 2.04_P4AFlight crew compartment door emergency removal F2.04_P6AFlight crew compartment video surveillance system F2.04_P7A

CHAPTER 3: CABIN FAMILIARISATION

ATR aeroplane layout F3.01_P1AExample of Armonia cabin seats F3.01_P2ARear facing passenger seats option F3.01_P3A

Mid cabin overhead compartment F3.01_P3B Rear cargo loading instructions andlimitations placards F3.01_P4ARear cargo, safety net and anti-smoke curtain F3.01_P5APSU and Oxygen module ATR 500/600 F3.02_P1APSU and Oxygen outlet ATR 200/300 F3.02_P1BStandard galley (Right hand side) F3.03_P1AAdditional optional rear cargo compartment galley F3.03_P2A

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CHAPTER 3: CABIN FAMILIARISATION (CONTINUED)

Hot jugs / Hot jugs ON/OFF switches F3.03_P2BLavatory location F3.04_P1ALavatory F3.04_P1BLSU F3.04_P2AWater system servicing location F3.04_P3ACabin crew stations location F3.05_P1ARear cabin crew seat F3.05_P2AFWD cabin crew seat ATR 72 F3.05_P3ACabin crew seat safety equipment F3.05_P4AATR 600 CMS F3.06_P1AATR 500 FAP F3.06_P1BATR 200/300 FAP F3.06_P1CATR 600 CMS F3.06_P2ACMS Navigation bar F3.06_P2BCMS lighting control ATR 600 F3.06_P4AFAP lighting control ATR 500F3.06_P4B2 minutes lighting locations F3.06_P5AATR 72 tail prop F3.07_P1A

CHAPTER 4: AEROPLANE SYSTEMS

AC packs view F4.01_P1AAir circuit F4.01_P1B

Air conditioning pack left hand side F4.01_P2AAir conditioning pack right hand side F4.01_P2BFlight crew compartment overhead panel COMPT TEMP PANEL F4.01_P2CCabin temperature icon on CMS navigation bar F4.01_P3ACabin temperature display on CMS F4.01_P3BAFT cargo compartment smoke detector F4.02_P1ALavatory smoke detector duct F4.02_P1BFlight crew compartment smoke alerting window ATR 600 F4.02_P2AFlight crew compartment smoke alerting window ATR 200/300/500 F4.02_P2BAft cargo smoke detector light on FAP F4.02_P2CLavatory smoke detector light on FAP F4.02_P2DSmoke detector light on CMS F4.02_P3A

Aft cargo compartment extinguisher connector F4.02_P4AAft cargo compartment extinguisher diffuser F4.02_P4BLavatory waste bin automatic fire extinguisher F4.03_P1ALavatory waste bin flap cover F4.03_P1BEmergency lights description F4.04_P1AEmergency lights locationF4.04_P2AEmergency lights switch (Flight crew compartment Overhead panel) F4.04_P2BEmergency lights activation button on FAP F4.04_P2CEmergency lights activation button on CMS F4.04_P2D

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CHAPTER 4: AEROPLANE SYSTEMS (CONTINUED)

Oxygen supply control (Flight crew compartment overhead panel) F4.05_P1AAeroplane oxygen supply F4.05_P1BOxygen supply from flight crew compartment to cabin outlets ATR 200/300F4.05_P2AATR 200/300 oxygen outlet F4.05_P2BATR 200/300 oxygen mask F4.05_P2COxygen supply from flight crew compartment to cabin modules ATR 500/600F4.05_P3A

ATR 500/600 MRT in oxygen module F4.05_P3BATR 500/600 oxygen module openedF4.05_P3CATR 500/600 oxygen mask F4.05_P3D100% Oxygen control (Flight crew compartment overhead panel) F4.05_P5AEROS Quick Donning Mask description F4.05_P6AEROS Quick Donning Mask location F4.05_P6BDonning of the oxygen Quick Donning Mask F4.05_P7A

OPTIONAL IFE SYSTEM:

CMS USB sockets F4.06_P1ACMS Initialization phase 3 F4.06_P2ACMS initialization phase 4 F4.06_P2BCMS navigation bar-audio command F4.06_P2CCMS Audio page F4.06_P2DCMS navigation bar-video command F4.06_P3ACMS video page F4.06_P3BCMS navigation bar-parameters command F4.06_P4ACMS parameters video page F4.06_P4BVideo screens opened F4.06_P5AIFE overview F4.06_P7APVCU F4.06_P7BFAP, MMPU and VCCU F4.06_P8A

PVCU F4.06_P9AVideo screens location F4.06_P10AVideo screens opened F4.06_P10BMMPU activation F4.06_P12AVCCU commands F4.06_P12B

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CHAPTER 5: COMMUNICATION

Cabin No-smoking and Fasten seat belt signs F5.01_P1ALavatory return to seat sign F5.01_P1BNo-smoking and Fasten seat belts control switches (Flight crew compartmentoverhead panel) F5.01_P1CCabin Interphone and Public Address F5.02_P1AFlight crew compartment Interphone and Public Address systemF5.02_P2AType 1 handset (ATR 500/600 series) F5.02_P3AType 2 handset (ATR200/300 series) F5.02_P3BFlight crew call indicator ATR 600 CMS F5.02_P4AFlight crew call indicator ATR 500 FAP F5.02_P4BFlight crew call indicator ATR 200/300 FAP F5.02_P4CLine indicator ATR 500/600 F5.02_P5ALine indicator ATR 200/300 F5.02_P5BHandset and Push To Talk button all ATR F5.02_P5CNormal call line indicator ATR 500/600 F5.02_P6ANormal call line indicator ATR 200/300 F5.02_P6BFlight crew compt. normal call indicator, ATR 500/600 F5.02_P6CFlight crew compt. normal call indicator, ATR 200/300 F5.02_P6DEmergency call line indicator ATR 500/600 F5.02_P7AEmergency call line indicator ATR 200/300 F5.02_P7BFlight crew compartment Emergency call indicator, ATR 500/600 F5.02_P7CFlight crew compartment Emergency call indicator, ATR 200/300 F5.02_P7D

Additional optional handset ATR 72 F5.02_P8AHandset panel with additional option ATR 72 F5.02_P8BCall identification lights with additional handset option ATR 72 F5.02_P8CFlight crew compartment to cabin call indications, with additional option ATR 72F5.02_P9ACabin to cabin call indications, with additional option ATR 72 F5.02_P9BP.A indicator ATR 500/600 F5.02_P10AP.A indicator ATR 200/300 F5.02_P10BPax cabin call CMS indicator ATR 600 F5.03_P1APax cabin call FAP indicator ATR 500 F5.03_P1BPax cabin call FAP indicator ATR 200/300 F5.03_P2ALavatory call FAP/CMS indicator ATR 500/600 F5.03_P2B

Lavatory call FAP indicator ATR 200/300 F5.03_P2CFlight crew compartment document door F5.04_P1A

CHAPTER 6: DOORS AND EXITS

Standard ATR 42 and 72 doors/exits top view F6.01_P1ADoors and exits left hand side view F6.01_P2ADoors and exits right hand side view F6.01_P2BDoors control panel (Flight crew compartment) F6.01_P3A

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CHAPTER 6: DOORS AND EXITS (CONTINUED)

Escape hatch location F6.02_P1AEscape hatch inside view F6.02_P1BEscape hatch outside view F6.02_P2AEscape rope stowage (Electric rack) F6.02_P2BEscape rope use F6.02_P2CEntrance door opened, outside view F6.03_P1AEntrance door closed, inside view F6.03_P2ASafety pin position on ground (Handrail up when opening the door) F6.03_P2BSafety pin position in flight (Handrail down when opening the door) F6.03_P2CEntrance door closed, outside view F6.03_P3AEntrance door control handle/lever opened F6.03_P3BEntrance door control handle/lever closed F6.03_P4AEntrance door with adjustable handrail down (Emergency mode) F6.03_P5AOptional FWD left entrance door inside view F6.03_P6AOptional FWD left entrance door, outside control lever (Opened position) F6.03_P7AOptional FWD left entrance door, door flap casing F6.03_P7BOptional FWD left entrance door opened, inside view F6.03_P8AOptional FWD left entrance door opened, outside view F6.03_P8BService door inside view F6.03_P9AService door outside view F6.03_P10AFuselage hook holding door handle F6.03_P10BGust lock push button ATR 500/600 F6.03_P10CGust lock pull lever ATR 200/300 F6.03_P10D

Forward emergency exit outside view F6.03_P12AForward emergency exit inside view F6.03_P12BForward emergency exit operation F6.03_P12C

CHAPTER 7: EMERGENCY EQUIPMENT

Oxygen module opening with MRT (ATR 500/600) F7.02_P1AMRT (Manual Release Tool) F7.02_P1BPortable oxygen bottle Scott type 5500 F7.02_P2APortable oxygen bottle location F7.02_P2BOxygen mask F7.02_P4AHalon extinguisher F7.02_P5A

Using the halon extinguisher F7.02_P6AWater extinguisher F7.02_P7APBE stowage box F7.02_P8APBE deployed F7.02_P8BPBE description F7.02_P9APBE activation F7.02_P10AProtective gloves F7.02_P12ACrash axe F7.02_P12B

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CHAPTER 7: EMERGENCY EQUIPMENT (CONTINUED)

Megaphone F7.02_P15ALife jacket under seat location F7.02_P16ALife jacket pouch F7.02_P16BAerazur Life jacket F7.02_P16CAerazur life jacket on adult (Strap around waist) F7.02_P17AAerazur life jacket on child (Strap between legs) F7.02_P17BFirst Aid Kit F7.02_P18APortable ELT ADT 406 S (Survival) Flight bag and wall mounting bracketF7.02_P19AADT 406 S (Survival) F7.02_P19BPortable ELT ADT 406 S (Survival) details F7.02_P20AELT ADT 406 AF (Automatic Fixed) F7.03_P1AX MIT ALERT test, flight crew compartment overhead panel F7.03_P1B

CHAPTER 8: EMERGENCY EQUIPMENT DIAGRAMS

Flight crew compartment emergency equipment F8.01_P1AATR 72.500/600 emergency equipment diagram F8.02_P1AATR 72.200emergency equipment diagram F8.03_P1AATR 42.500/600 emergency equipment diagram F8.04_P1AATR 42.300 emergency equipment diagram F8.05_P1A

CHAPTER 9: NORMAL PROCEDURES

Ground service bus switches F9.02_P1AFAP Emergency lights switch ON F9.02_P4APhases of flight F9.03_P1A

CHAPTER 10: EMERGENCY PROCEDURES

Fire triangle F10.03_P1AOptional rear cargo anti-smoke curtain and door F10.03_P6AHalon extinguisher connector (Next to FAP) F10.03_P6BHalon extinguisher connection F10.03_P6CPassengers bracing positions F10.06_P9A

Passengers bracing positions (Continued) F10.06_P10ACabin crew bracing positions F10.06_P11AAeroplane position with nose landing gear collapsed F10.06_P13AAeroplane position with all landing gear collapsed F10.06_P13BAeroplane position with left or right main landing gear collapsed F10.06_P13CAeroplane positions on water (Right or left) F10.06_P16AWater level, immersed or not immersed wing F10.06_P16BATR doors/exits classification for evacuation F10.06_P17A

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CHAPTER 1: AEROPLANE GENERALATR range T1.02 _P1A

ATR family performances T1.03_P1AATR family dimensions T1.04_P1A

CHAPTER 2: FLIGHT CREW COMPARTMENTFlight crew compartment door operation T2.04_P5A

CHAPTER 4: AEROPLANE SYSTEMSATR Oxygen differences T4.05_P4AOPTIONAL IFE SYSTEM: VCCU commands T4.06_P7A

CHAPTER 5: COMMUNICATIONInterphone and P.A system summary T5.02_P3A

PA priorities T5.02_P10A

CHAPTER 6: DOORS AND EXITSDoors and exits dimensions T6.01_P2A

CHAPTER 9: NORMAL PROCEDURESInterphone system T9.02_P2APA system T9.02_P3APassenger call T9.02_P4AEmergency lights T9.02_P4BPre-flight duties T9.03_P2ACabin securing T9.03_P6AIn flight monitoring T9.03_P7APre landing duties T9.03_P9ARefuelling with pax on board T9.04_P2A

CHAPTER 10: EMERGENCY PROCEDURESTurbulences T10.02_P2AFire fighting T10.03_P8ADecompression signs T10.04_P1ATime of Useful Consciousness T10.04_P3ADecompression crew actions T10.04_P5AUnplanned emergency T10.06_P5A

Planned emergency evacuation on land T10.06_P12APlanned emergency evacuation on water (Ditching) T10.06_P15ADoors/exits classification for evacuation T10.06_P17AEvacuation drills on land T10.06_P18AEvacuation drills on water T10.06_P19A

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STANDARD NOMENCLATURE

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ABPs: Able Bodied PassengersAC: Alternative CurrentACW: Alternative Current WildAPU: Auxiliary Power UnitATR: Avion de Transport RegionalBCF: Bromo Chloro di Fluoro methaneBMG: Back Ground MusicCAM: CameraCAPT: CaptainCCOM: Cabin Crew Operating ManualCDU: Cabin Display Unit (video screen)CM: CentimetresCMS: Cabin Management SystemCO2: Carbon DioxideCRC: Continuous Repetitive ChimeCRM: Crew Resources ManagementCTRL: ControlDC: Direct CurrentDF: Royal Inventum Company (Ovenmanufacturer)

DME: Torch lights manufacturercorporationEASA: European Aviation SafetyAgencyELT: Emergency Locator TransmitterEU OPS: European Union regulationsfor commercial aviationFAA: Federal Aviation Authorities (USA)FAP: Flight Attendant PanelFCC: Flight Crew CompartmentFIG: FigureFO: First Officer

FT: FeetFWD: ForwardGPU: Ground Power UnitICAO: International Civil AviationOrganization

IFE: In Flight EntertainmentIMO: International MaritimeOrganizationINT: InterphoneKO2: Potassium SuperoxideLAV: LavatoryLCD: Liquid Cristal DisplayLED: Light Emitting DiodeLHS: Left Hand SideLRBL: Least Risk Bomb LocationLSU: Lavatory Service UnitMEL: Minimum Equipment ListMHz: MegahertzMMEL: Master Minimum Equipment ListMMPU: Multi Media Player UnitMRT: Manual Release ToolNM: Nautical MilesPA: Public AddressPAX: PassengersPBE: Portable Breathing Equipment

PTT: Push To TalkPSU: Passenger Service UnitPVCU: Power and Video Control UnitRHS: Right Hand SideSCCM: Senior Cabin Crew MemberTUC: Time of Useful ConsciousnessVCCU: Video Cabin Control UnitW: WattsX-MIT: ELT Remote Control Unit (Flightcrew compartment)XMRT: Emergency Locator TransmitterControl Panel (Flight crew compartment)


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This manual refers to all ATR aeroplane series:

ATR 42-300/500/600

ATR 72-200/500/600

1.00 CONTENTS

1.01 INTRODUCTION

1.02 RANGE OF OPERATION

1.03 PERFORMANCE

1.04 DIMENSIONS

1.04.1 EXTERNAL DIMENSIONS

1.04.2 EXTERNAL DIMENSIONS ATR 42


1.05 UNPRESSURIZED AREAS

1.06 LOCATION OF CARGO/BAGAGE COMPARTMENTS

1.07 DANGER AREAS

1.08 HOTEL MODE

1.09 ELECTRICAL POWER

1.10 FLIGHT CONTROLS

1.11 ICE CONTAMINATION

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AEROPLANE GENERAL

CONTENTS

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The ATR aeroplane is a narrow-bodied twin-turboprop, short-haul regional airliner

built by the Franco-Italian aeroplane manufacturer ATR (Avions de TransportRgional/ Aerei da Transporto Regionale) based in Toulouse - Blagnac, France.

The aeroplane fuselage and tail section are manufactured near Naples - Italy, wingsare assembled near Bordeaux France.

The engines are Pratt and Whitney and the propellers Hamilton standard.

Final assembly, flight testing, certification and delivery are done in Toulouse.

The production consists of ATR 42 and ATR 72, the appellations 42 and 72 beingderived from the aeroplanes capacity, which varies from 42 to 50 and 64 to 72 seatsrespectively.

Several different series have been produced over the years with differentconfigurations and engines performances, the main ones including:

42-300 and 72-200: 1st generation aeroplane (1984 - 1998) 42-500 and 72-500: More than 900 units (1995 - 2011) 42-600 and 72-600 : latest generation (2011 onward)

The ATR 600 series has a complete new flight crew compartment (Glass cockpit)with latest avionic technology.

Changes in the cabin mainly concern the overall appearance, with modernized seats.

Cabin crew are not affected by any system or emergency equipment changes

between ATR 500 series and ATR 600 series, unless specified in this manual.ATR aeroplane generally offers a single class configuration and is operated by:

2 flight crew and 1 cabin crew on ATR 42

2 flight crew and 2 cabin crew on ATR 72

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AEROPLANE GENERAL

INTRODUCTION

1.01

P 1

JAN 12


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F1.02_P1A: ATR family range of operation

Range with maximum passengers:

T1.02_P1A: ATR range

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AEROPLANE GENERAL

RANGE OF OPERATION

1.02

P 1

JAN 12

ATR 42 - 300 ATR 42 - 500 ATR 42 - 600

456 NM / 844 Km 801 NM / 1483 Km 801 NM / 1483 Km

ATR 72 - 200 ATR 72 - 500 ATR 72 - 600

872 NM / 1615 Km 890 NM / 1648 Km 890 NM / 1648 Km


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The maximum certified altitude is 25000 feet.

42 series

72 series

T1.03_P1A: ATR family performances

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AEROPLANE GENERAL

PERFORMANCE

1.03

P 1

JAN 12

ATR 42-300 ATR 42-500 ATR 42-600

Max. Take off weight 16,900Kg (37,257lbs) 18,600Kg (41,005lbs) 18,600Kg (41,005lbs)

Max. Landingweight 16,400Kg (36,155lbs) 18,300Kg (40,344lbs) 18,300Kg (40,344lbs)

Max. Zero Fuel

weight 15,540Kg (34,259lbs) 17,000Kg (37,478lbs) 17,000Kg (37,478lbs)

Operational EmptyWeight 10,900Kg (24,030lbs) 11,500Kg (25,353lbs) 11,500Kg (25,353lbs)

Max. Payload 4,640Kg (10,229lbs) 5,500Kg (12,125lbs) 5,500Kg (12,125lbs)

Max. Fuel Weight 4,500Kg (9,920lbs) 4,500Kg (9,920lbs) 4,500Kg (9,920lbs)

ATR 72-200 ATR 72-500 ATR 72-600

Max. Take off weight 22,000Kg (48,501lbs) 22,800Kg (50,265lbs) 23,000Kg (50,705lbs)

Max. Landingweight 21,350Kg (47,068lbs) 22,350Kg (49,272lbs) 22,350Kg (49,272lbs)

Max. Zero Fuelweight 20,000Kg (44,092lbs) 20,500Kg (45,194lbs) 21,000Kg (46,296lbs)

Operational EmptyWeight 13,000Kg (28,660lbs) 13,500Kg (29,762lbs) 13,500Kg (29,762lbs)

Max. Payload 7,000Kg (15,432lbs) 7,000 Kg (15,432lbs) 7,500Kg (16,534lbs)

Max. Fuel Weight 5000Kg (11,023lbs) 5000Kg (11,023lbs) 5000Kg (11,023lbs)


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1.04.1 EXTERNAL DIMENSIONS

T1.04_P1A: ATR family dimensions

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AEROPLANE GENERAL

DIMENSIONS

1.04

P 1

JAN 12

ATR 42 ATR 72

Length 22,670 m (74 ft 5 in) 27,166 m (89 ft 1,5 in)

Span 24,572 m (80 ft 7 in) 27,050 m (88 ft 9 in)

Height 7,586 m (24 ft 11 in) 7,650 m (25 ft 1 in)

Outside fuselage diameter 2,865 m (9 ft 5 in) 2,865 m (9 ft 5 in)

Wing surface 54,514 m2 (586 sq ft) 61 m2 (657 sq ft)

Wheel base 8,780 m (28 ft 10 in) 10,77 m (35 ft 4 in)

Track 4,100 m (13 ft 5 in) 4,100 m (13 ft 5 in)

Propeller diameter 3,930 m (12 ft 11 in) 3,960 m (13 ft)

Clearance fuselage/propeller 0,820 m (2 ft 8 in) 0,835 m (2 ft 8,9 in)

Distance between engines 8,10 m (26 ft 7 in) 8,10 m (26 ft 7 in)


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AEROPLANE GENERAL

DIMENSIONS

1.04

P 2

JAN 12

F1.04_P2A: ATR family dimensions


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The ATR 42 and 72 comprise two type I doors, two type III exits, one flight crew

compartment escape hatch and one cargo door.

The ATR aeroplane is fully pressurized, except the random (nose) part, the landinggear bay and the tail cone.

F1.05_P1B: Unpressurized zones

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AEROPLANE GENERAL

DOORS AND EXITS / UNPRESSURIZED AREAS

1.05

P 1

JAN 12

R1 (Type III)

(Type I)(Type I)

R2 Service doorEntrance door L2

L1 (Type III)

Cargo door(Not an emergency exit)

Flight crew compartmentescape hatch

F1.05_P1A: ATR 42 and 72 standard doors/exits overview


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There are three cargo compartments installed on the ATR.

The ATR cargo compartments have the particularity to be accessible from the cabin.Two of them are located between the flight crew compartment and the cabin area,and one is located at the rear of the aeroplane.

Forward right cargo Rear cargo

Forward left cargo Cargo area access for cabin crew

Cargo area access for ground personnel

An option consists of replacing the forward cargo door (Left hand side) with a

passenger entrance door. This optional door is not an emergency exit.If this option has been chosen, the forward left cargo compartment will then besuppressed and access to the forward right hand side cargo compartment onlypossible from outside.

F1.06_P1A: Cargo/Baggage compartments

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AEROPLANE GENERAL

LOCATION OF CARGO/BAGGAGE COMPARTMENTS

1.06

P 1

JAN 12

L2

R1 R2

L1

Cargo door

R2

L1 L2

R1Cargo door

Optional entrance door


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1.07_P1A: Propeller danger area (engines running)

1.07_P1B: Exhaust danger area (engines running)

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AEROPLANE GENERAL

DANGER AREAS

1.07

P 1

JAN 12


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The ATR aeroplane is not fitted with an Auxiliary Power Unit (APU) but has propeller

brake (referred as hotel mode) that stops the propeller #2 (right engine), allowingthe turbine to run and provide air conditioned and power to the aeroplane without thepropeller spinning. The hotel mode provides DC 28V current only.

This eliminates the need for added weight and cost of an APU.Engines are periodically switched during maintenance to ensure equal wear.

The propeller brake is activated on the ground only, from the flight crew compartmentoverhead panel.

F1.08_P1B: Propeller brake control switch (Flight crew compartment overhead panel)

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AEROPLANE GENERAL

HOTEL MODE

1.08

P 1

JAN 12

F1.08_P1A: Propeller brake location, right engine


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The power in the cabin is fed with 2 main types of electricity:

DC-28V (Direct Current) AC-115V (Alternative Current)

DC and AC power can come from different sources: the aeroplane itself (batteriesand engines generators) or ground power unit.The aeroplanes own batteries (Main Bat. and Emer. Bat.) deliver enough powerto activate 2 minutes of cabin lighting, cargo door operation and engine start.Note:Those batteries are distinct from the batteries that will provide the emergencylighting system in case of essential power failure.

Hotel mode provides 28V (DC) in the cabin GPU DC-28V provides 28V (DC) in the cabin GPU AC-115V provides is 115V (AC)in the cabin

When the propellers are running (Flight conditions) ACW (AC wild) is produced andconverted, therefore all power sources are available.

The cabin main power supply is controlled by two Ground Service Bus (One for DCand one for AC).The Ground Service Bus switches are located at the rear of the aeroplane on theFAP above the cabin crew seat.

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AEROPLANE GENERAL

POWER

1.09

P 1

JAN 12

F1.09_P1A: Ground service BUS switches on Cabin Management System(CMS)


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Note: Two sockets are available in the flight crew compartment (behind thefirst officers seat) delivering 28 V and 115 V. They can be used by groundservices for cleaning purposes.

C.C.O.M


AEROPLANE GENERAL

POWER

1.09

P 2

JAN 12

E X I T

ON ON

F1.09_P2A: Ground service BUS switches on Flight Attendant Panel (FAP)


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The position of the aeroplane is controlled by movable surfaces:

Rudder Elevators Ailerons Flaps Spoilers

PITCH

The aeroplane movement is nose up / nose down and this is achieved with mainlythe use of the ELEVATORS.

ROLL

The aeroplane movement is wing up/ wing down and this is achieved with mainly theuse of the AILERONS, and is assisted by hydraulically activated flaps.

YAW

The aeroplane movement is nose right / nose left and this is achieved with mainly theuse of the RUDDER.

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AEROPLANE GENERAL

FLIGHT CONTROLS

1.10

P 1

JAN 12

F1.10_P1A: Aeroplane flight controls


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ATR aeroplane is equipped with:

Electrical anti-icing system Pneumatic de-icing system

The anti-icing system prevents ice contamination by electrically heating specific partsof the aeroplane, such as:

Air data probes Flight crew compartment windshields and side windows Propeller blades Wings horns Rudder and horizontal tail horns

Pneumatic de-icing removes ice contamination by inflating expandable rubber bootslocated on wings and horizontal tail leading edges, and on the engines air intakes.This process is done in flight at regular intervals, with two different speed cyclesdepending on the outside temperature.

C.C.O.M


AEROPLANE GENERAL

ICE CONTAMINATION

1.11

P 1

JAN 12

F1.11_P1A: Anti-icing / De-icing systems

Anti-icing heated areas

De-icing pneumatic chambers


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2.00 CONTENTS

2.01 GENERAL LOCATION

2.02 FLIGHT CREW SEATS

2.03 OBSERVER SEAT

2.04 FLIGHT CREW COMPARTMENT DOOR

2.04.1 DESCRIPTION

2.04.2 LOCKING SYSTEM

2.04.3 CALL PANEL DESCRIPTION

2.04.4 NORMAL OPERATION

2.04.5 EMERGENCY OPERATION

2.04.6 OTHER EMERGENCY PROCEDURES

2.04.7 PROCEDURE TO ACCESS THE FLIGHT CREW COMPARTMENT

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FLIGHT CREW COMPARTMENT

CONTENTS

2.00

P 1

JAN 12


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The access to the flight crew compartment is done through the forward cargo area.A lockable door separates the cabin from the cargo area: it opens forward into the

cargo.A bulletproof reinforced door separates the cargo area from the flight crewcompartment.

The door separating the cabin from the forward cargo compartments can belocked/unlocked from the cargo side with a latch, and with a key from the cabin side.

In case of cargo fire, the door provides protection against smoke in the cabin.This door is also equipped with a spy hole and should be closed and locked at alltime during flight.

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GENERAL LOCATION

2.01

P 1

JAN 12

FWD right cargo

FWD cargo door

Flight crew compartment bulletproof door

Cabin to cargo door

Flight crew compartment

FWD left cargo

F2.01_P1A: Cabin to FWD cargo area door

Cabin side view

Latch horizontal= Locked

Cargo side view

R1L1


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The flight crew compartment is designed to accommodate two flight crew members

plus one observer.

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GENERAL LOCATION

2.01

P 2

JAN 12

Cup holder

First officersseat

Centralpedestal

Cup holder

Captainsseat

Overheadpanel

Instrumentspanel

Glareshield

Flight crew compartment

L1R1

F2.01_P2A: ATR 42/72-600 flight crew compartment

R1L1


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The captain and first officer seats are mounted each on a base secured to the floor

on each side of the center pedestal. They are mechanically adjustable along 3 axesfor individual comfort. They are equipped with adjustable folding armrests andshoulder harness with 3 point buckle.

The cabin crew members should know the main functions of the pilots seats in orderto be able to act in case of flight crew incapacitation.

All control levers are located inboard except for the recline control which is locatedoutboard.

The first officers seat is identical to the captains one, except that all control leversare located on the opposite sides.

NOTE:

ATR offers the possibility to provide with lumbar adjustment and thigh rests oncaptain and first officer seats.

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FLIGHT CREW SEATS

2.02

P 1

JAN 12

F2.02_P1A: Captains seat control levers

Shoulder harness lockingVertical adjust

Horizontal adjust

Recline control

Life jacket stowage


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The observer seat is located behind the pedestal and between the electronic andelectric racks. It is equipped with a life jacket stowage and a harness with 3 point

buckle. When not in use, the observer seat is stowed against the electronic rack andsecured with a bungee.

Note: It is also possible to stow the observer seat against the flight crewcompartment left hand side door panel.

C.C.O.M



OBSERVER SEAT

2.03

P 1

JAN 12

Observer seat deployedObserver seat folded

F2.03_P1A: Observer seat description

Life jacket stowage

Wall bracket

Oxygen quick donning mask and smoke goggles

3 point buckleharness


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To use the observer seat, remove the bungee from the hook, and rotate the seat tothe rear the seat will lock itself into the bracket mounted on the electric rack side

panel.To stow the seat back, push the locking control lever to the left to release it from thebracket, fold the seat back against the electronic rack and attach the bungee.

Safety pins enable the observer seat to be rocked backward in order to facilitateemergency evacuation in case of jamming or to assist an observer in first aidsituation. To remove the pins, pull them upward.

C.C.O.M



OBSERVER SEAT

2.03

P 2

JAN 12

Bungees

Seat locking lever

Observer seat rear view

F2.03_P2A: Observer seat release pins location


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2.04.1 DESCRIPTION

An aft opening double hinged door separates the flight crew compartment from theforward cargo compartment. It opens rearward into the cargo area.The door has an electromagnetic locking system controlled by the pilots. In normaloperations, the door is closed and locked to ensure flight safety.

The door is bulletproof and fully compliant with rapid decompression requirements.

This door shall be closed prior to engine start for take-off and will be locked whenrequired by security procedure or the Captain, until engine shut down after landing.

C.C.O.M



FLIGHT CREW COMPARTMENT DOOR

2.04

P 1

JAN 12

Flight crew compartment door

Cabin to forwardcargo area door

FWD left cargo FWD right cargo

Flight crew compartment door

L1 R1

F2.04_P1A: Flight crew compartment door


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2.04.2 LOCKING SYSTEM

The flight crew compartment door locking system ON/OFF control switch is locatedon the circuit breaker panel behind the first officer seat. When on ON position, theflight crew compartment door locking system is operative, whereas when on OFFposition, the system is inoperative.

A door control panel located on the central pedestal enables the flight crew to lockand unlock the flight crew compartment door. The flight crew will be made aware ofthe access request by a buzzer associated with a light on the door control panel. Toallow entry into the flight crew compartment, the pilots will place the toggle switch onOPEN, and to deny entry they will place the toggle switch on DENY.

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2.04

P 2

JAN 12

F2.04_P2B: Flight crew compartment door control panel

F2.04_P2A: Flight crew compartment door locking system ON/OFF

FAULT

OPEN

ATR 600 series ATR 200/300/500 series


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2.04.3 CALL PANEL DESCRIPTION

The door call panel is used by the cabin crew members to request pilots to open thedoor. There are 2 different access request modes: a normal access type and anemergency access request.

When requesting access to the flight crew compartment area, the cabin crew shouldhave closed the cabin to cargo door and stand in the axis of the flight crewcompartment door.

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2.04

P 3

JAN 12

Door call panel

F2.04_P3A: Flight crew compartment door call panel


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CALL push button switch:

The cabin crew presses this button to request normal accessto the flight crew compartment. When pressing this button, it willactivate a buzzer sound in the flight crew compartment for atleast 2 seconds.

OPEN green light:

The light illuminates steady when the door has been unlockedby the flight crew. The door will remain unlocked for 10 seconds.

Cabin crew will need to pull on the door panels to open.

DENIED red light:

The light illuminates steady when the flight crew has denied thecabin crew access to the flight crew compartment. The door willremain locked and the light will remain on for the next 3 minutes.Any action on the call panel will be inhibited for this time.

EMER. Push button switch:

A rotating plate to prevent inadvertent activation protects thisbutton.This button is used to initiate the emergency opening of thedoor.

The emergency mode is to be used only if there is no reply from the flight crewfollowing a normal call and an interphone call (possibility of both pilots incapacitated).

After pressing the button, the green light flashes for 30 seconds together with thecontinuous buzzer sound activated in the flight crew compartment, after which thedoor will unlock automatically.Cabin crew will need to pull on the door panels to open.

To avoid unlawful interference, a pilot can cancel the unlocking of the door by movingthe toggle switch onto DENY position within the 30 seconds period.

C.C.O.M




2.04

P 4

JAN 12

F2.04_P4A: Flight crew compartment call options


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2.04.4 NORMAL OPERATION

2.04.5 EMERGENCY OPERATION

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2.04

P 5

JAN 12

CREW REQUESTACCESS CALL

OPEN (Green Steady -10 seconds)

DENIED (Red steady 3 minutes)

Pull the door right panel to openUnlock the left panel to open

No further action

CREW REQUEST ACCESS CALL

No Reply

CALL via INTERPHONE Reply No further action

No Reply

Press EMER

OPEN Green Flashing for 30 sec.

Door opens after 30 sec.

T2.04_P5A: Flight crew compartment door operation


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2.04.6 OTHER EMERGENCY PROCEDURES

Electrical power loss

In case of electrical power failure the door will automatically unlock.Flight crew members can lock the door manually with the locking bolts, but theemergency access to the flight crew compartment will no longer be possible.

Flight crew compartment door jammed

In case of jammed flight crew compartment door, the doors panels can be removedfrom inside only. 2 quick release pins are installed on top and bottom of each doorpanels.

Right hand side:

Disconnect the electric plug (1/4 of a turn) Remove the 2 quick release hinged pins Push and remove the door panel

Left hand side:

Remove the 2 quick release hinged pins Push and remove the door panel

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2.04

P 6

JAN 12

FCC Quick release hinged pin

F2.04_P6A: Flight crew compartment door emergency removal

FCC Right panel electric plug


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2.04.7 PROCEDURE TO ACCESS THE FLIGHT CREW COMPARTMENT

The flight crew compartment is an area with a very restricted access. Indeed noperson, other than a flight crew member assigned to a flight, is admitted to, or carriedin, the flight crew compartment unless that person is:

An operating crew member A representative of the Authority responsible for certification, licensing or

inspection if this is required for the performance of his/her official duties Permitted by, and carried in accordance with instructions contained in the

Operations Manual

In the interests of safety, admission to the flight crew compartment should not causedistraction and/or interfere with the flight operation; and all persons carried on theflight crew compartment should be made familiar with the relevant safety procedures.The flight crew compartment door being closed from engines start for take-off untilengines shut down at parking stand; requests to access the flight crew compartmentwill be done through interphone. It is, indeed, a necessity to make self known to theflight crew before operating the flight crew compartment door panel.

NOTE: ATR offers the possibility to equip the aeroplane with a cabin videosurveillance. This option includes the installation of 3 video cameras in the cabin.One video camera installed in the forward cargo area controls the flight crewcompartment entry door and 2 additional cameras provide with full passengerscabin view. A video display is installed on the right hand side lateral maintenance

panel allowing the pilots to get a complete view of the cabin.

1.Cargo compartment camera2.

Flight crew compartment door camera3.Cabin camera4.Circuit breaker5.Monitor

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2.04

P 7

JAN 12

F2.04_P7A: Flight crew compartment video surveillance system


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3.00 CONTENTS

3.01 CONFIGURATION AND LAYOUT

3.01.1 AEROPLANE LAYOUT AND CABIN CROSS SECTION3.01.2 PASSENGER SEAT AND ROW IDENTIFICATION3.01.3 SEAT DESCRIPTION3.01.4 HAND BAGGAGE STOWAGE3.01.5 REAR CARGO COMPARTMENT3.01.6 FORWARD CARGO COMPARTMENT

3.02 PASSENGER SERVICE UNITS (PSU)

3.03 GALLEY

3.03.1 LOCATION3.03.2 POWER

3.04 LAVATORY

3.04.1 LOCATION AND LAYOUT3.04.2 LAVATORY SERVICE UNIT (LSU)3.04.3 LAVATORY DOOR3.04.4 LAVATORY WATER AND WASTE SYSTEM

3.05 CABIN CREW SEATS

3.05.1 LOCATION3.05.2 DESCRIPTION3.05.3 EQUIPMENT3.05.4 CREW REST AREA

3.06 FLIGHT ATTENDANT PANEL / CABIN MANAGEMENT SYSTEM

3.06.1 GENERAL DESCRIPTION3.06.2 LIGHTING SYSTEM3.06.3 GROUND SERVICE BUSES

3.06.4 TWO MINUTES MINIMUM LIGHTING

3.07 TAIL PROP

3.07.1 DESCRIPTION3.07.2 INSTALLATION3.07.3 PRE-FLIGHT CHECK

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CABIN FAMILIARISATION

CONTENTS

3.00

P 1

JAN 12


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3.01.1 AEROPLANE LAYOUT AND CABIN CROSS SECTION

The ATR layout counts:

1 flight crew compartment 2 forward cargo compartments (other options may exist) 1 cabin (seating capacity varies on the aeroplane type and company request) 1 galley (with options for more) 1 lavatory 1 aft cargo compartment

C.C.O.M



CONFIGURATION AND LAYOUT

3.01

P 1

JAN 12

ATR 42: 42-50 seats

ATR 72: 64-72 seats

R1L1

L2 R2

R2L2Cabin cross section

F3.01_P1A: ATR aeroplane layout

Galley Lavatory CargoCabin crew seat Doors/Exits

45,72 cm (18 in.)

226,3 cm (89 in.)257 cm (102 in.)

286,5 cm (112,2 in.)

191 cm(75,2 in.)

R1L1


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3.01.2 PASSENGER SEATS AND ROW IDENTIFICATION

Passengers seats are identified alphabetically, rows are identified by numbers.The cabin counts 4 seats abreast and the number of rows will vary depending on theseat pitch and the furnishing present in the cabin, especially in the aft area.

The standard ATR 42 seating configuration usually consists in 48 seats at a pitch of76,2 cm (30 inches). The standard interior configuration on ATR 72 consists of 68seats, with a pitch of 78,74 cm (31 inches).

The seats fitted in the ATR 42 vary between 42 and 50 and between 64 and 72 onATR 72.

Note:

According to the type certification process, the maximum seating capacity is 60passengers for the 42 series and 74 passengers for the 72 series.

3.01.3 SEAT DESCRIPTION

Passengers seats are double type equipped with a seat belt and life vest stowage.Other features may also be present such as literature pocket mouse trap frame, traytable, adjustable headrest, handicap (lift-up) aisle armrest with positive locking.

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3.01

P 2

JAN 12

F3.01_P2A: Example of Armonia cabin seats


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Depending on the aeroplane configuration, some passengers seat could be facing

aft. This will only impact the passenger safety bracing position to adopt.

NOTE 1:

ATR offers the possibility to install external folding armrests (on any seats apart from the front rowdue to the emergency exits) in order to allow the seating of disabled passengers. The quantity ofmodified seats and their positioning in the cabin are defined according to customers requirement.

NOTE 2:

Some ATR can be delivered without window blind on each passenger window.If available, cabin crew should ensure window blinds are opened during take-off and landingphases.

NOTE 3:

ATR offers the option to install a standard fabric headrest cover on each passenger seat. Thestandard headrest cover color is white and the dimensions are 225 x 210mm.

NOTE 4:On certain models, the seat cushions can be used as flotation devices.

3.01.4OVERHEAD COMPARTMENTSThe aeroplane is equipped with overheadcompartments above each row of seats.The maximum weight that an overheadcompartment can support will be indicated ona placard inside the compartment (From 20to 40 kilograms according to models and

location).Any item too heavy to be placed in theoverhead compartment should be stowedunder the seat (if small enough to fit in) or inthe cargo compartment.

Cabin crew should never stow a passenger luggage into the lavatory.

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3.01

P 3

JAN 12

F3.01_P3B: Mid cabin overhead compartment

F3.01_P3A: Rear facing passenger seats option


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3.01.5 REAR CARGO COMPARTMENT

Rear cargo compartment baggage loading and off-loading is done through R2service door.Although the Loading and Off-loading tasks fall under ground personnelresponsibilities, and according to operators standard operating procedures, cabincrew must be aware of the weigh and height limitations as well as specialprecautions, as they could be brought to add or remove luggage themselves duringboarding.Placards placed inside the cargo compartment indicate weight (Variable according toaeroplane) and height limitations, as well as safety net hooking and tighteninginstructions.

The height limitation must be respected to allow efficient extinguisher gasdiffusion in case of fire fighting procedure. (See chapter 4.02 page 3)

It is the cabin crew responsibility to check that the safety net is properly hooked and

tightened for the flight.

Note: ATR offers the option to install an anti smoke curtain in addition of thestandard safety net, or a rigid door to close the rear cargo compartment. This doorcan be locked with a key. If installed, it the cabin crew responsibility to close thecurtain or door for the flight.

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3.01

P 4

JAN 12

F3.01_P4A: Rear cargo loadinginstructions and limitations placards


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3.01.6 FORWARD CARGO COMPARTMENT

Forward cargo compartmentsbaggage loading and off-loading is done through thededicated cargo door, FWD left hand side.Loading and Off-loading tasks fall under ground personnel responsibilities, andaccording to operators standard operating procedures cabin crew do not have to

intervene in this area.

The FWD cargo door is not an emergency exit.

The forward cargo area being the separation area between the cabin and the flightcrew compartment, cabin crew must ensure they always operate the cabin to cargodoor with all necessary precautions (See chapter 2.01 page 1).

C.C.O.M




3.01

P 5

JAN 12

Rear cargo Rear cargo safety net Optional rear cargo

anti-smoke curtain

F3.01_P5A: Rear cargo, safety net and anti-smoke curtain


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The Passenger Service Unit (PSU) is equipped with:

A cabin crew call button An air outlet No smoking and fasten seat belt signs A passenger reading light An oxygen outlet (ATR 300/200 series) or oxygen module (ATR 500/600

series) available in every second row

The oxygen outlet (ATR 300/200 series) is a plug where cabin crew will connect aspare oxygen mask into, if needed.The oxygen module (ATR 500/600 series) already contains one oxygen mask andopens with a manual release tool.If the aeroplane is equipped with the 100% oxygen option (ATR 500/600 series only),

each module contains two oxygen masks and opens automatically.

Note:The last generation of ATR 72.200 has been equipped with oxygen modulesinstead of outlets.

C.C.O.M



PASSENGER SERVICE UNITS

3.02

P 1

JAN 12

F3.02_P1A: PSU and Oxygen module ATR 500/600

F3.02_P1B: PSU and Oxygen outlet ATR 200/300

O2module

O2outlet


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3.03.1 LOCATION

The main galley is located on the rear right hand side of the aeroplane (next toservice door R2) and is usually equipped with:

A waste bin with a flap cover Working foldaway table Trolleys Metal containers Hot jugs (28V DC - 125 W - 7.5 litres)

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GALLEY

3.03

P 1

JAN 12

Galley ATR 42

Galley ATR 72

R1 R2

L2

L2

R2

L1

L1

R1

F3.03_P1A: Standard galley (Right hand side)

Galley circuit breakers location


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IMPORTANT: Galleys should be secured at all time.

Galleys setting will vary according to the airlines requests. Indeed, ATR providesa variety of galley configuration and equipment selection as options.One galley option consists in installing a sink with water tap. The water is suppliedfrom the lavatory potable water tank and no water shut off valve is availablefor the cabin crew.There is also a possibility to add a lateral galley in the rear left hand side of thecabin, and/or inside the rear cargo compartment.

POSSIBLE GALLEY EQUIPMENT SELECTION:

- 115V ACW Hot jugs power supply

- Water Heater (5000W - 4.2 liters + 20 litres tank)- DF 300 oven (1250W - 12 casseroles)- DF 110 oven (3750 W - 32 casseroles)- DF 115 oven (3750 W - 48 casseroles)- Hot cup (560 W - 1 litre)- Ice unit instead of standard unit- Standard unit with 2 standard drawers- Half size trolley with 6 standard drawers- Full size trolley with 12 standard drawers

IMPORTANT: ON/OFF switches for electrical equipment (Optional or not) arelocated in the galley, next to the equipment (Hot jugs, oven)Main circuit breakers are located in the flight crew compartment, and additionalbreakers in the cabin entrance aisle side, on top of the galley panel RHS (SeeF3.03_P1A).

3.03.2 POWERSee Chapter 1.09 (Electrical Power)

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GALLEY

3.03

P 2

JAN 12

F3.03_P2A: Additional optionalrear cargo compartment galley

F3.03_P2B: Hot jugs / Hot jugs ON/OFF switches


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3.04.1 LOCATION AND LAYOUT

The lavatory is located at the rear left hand side of the aeroplane.

The lavatory layout is composed of:

A toilet bowl An amenity compartment

An LSU A toilet flush button A lavatory waste bin A mirror

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LAVATORY

3.04

P 1

JAN 12

R2

F3.04_P1A: Lavatory location

L2

ATR Lavatory

Flush button

Waste bin

LSU

F3.04_P1B: Lavatory


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3.04.2 LAVATORY SERVICE UNIT (LSU)

Service unit is composed of:

An air vent outlet A cabin crew call push-button A return to seatsign Only if the aeroplane is equipped with the 100% oxygen supply option (ATR

500/600 only), an oxygen module containing two masks, located in thelavatory ceiling (See chapter 4.05 p 5)

3.04.3 LAVATORY DOOR

The lavatory door is a regular type door (Not a bi-fold type door).

The door can be locked or unlocked from inside or outside the lavatory.

In order to lock or unlock the lavatory door from outside:

1. Lift the Lavatory sign2. Slide the knob to locked or unlocked position

There is a Vacant/occupied indicator sign on the FAP that illuminates according tothe lavatory door status (locked - red or unlocked - green).

IMPORTANT:On opening the lavatory door, most of the door panel slides inside the

lavatory, with a part still protruding out in the entrance way, which could hinder anemergency evacuation. Therefore standard operating procedures include that thedoor must be closed and locked for every take off and landing.

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LAVATORY

3.04

P 2

JAN 12

LSU ATR 500/600 LSU ATR 200/300

F3.04_P2A: LSU


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3.04.4 LAVATORY WATER AND WASTE SYSTEM

The aeroplane is equipped with a potable water system and a waste disposalsystem. Only the ground staff can check the level of water.

3.04.4.1 POTABLE WATER SYSTEM

Although called potable, it is not recommended to drink water from this system. Thepotable water system supplies fresh water for the lavatory sink (and for the optionalgalley sink).Fresh water for the toilet is stored in a tank located in the pressurized section of thefuselage. The water tank is filled from fresh water service panel located at the bottomof the rear fuselage. The water system is easily and completely drainable by gravity.

3.04.4.2 WASTE DISPOSAL SYSTEM

The toilet flushing system is obtained from a motorized pump filter unit. The flushingcycle is automatically controlled by electrical timer. Draining, flushing and filling of thetank are accomplished at the toilet service panel, located underneath the rearfuselage.

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LAVATORY

3.04

P 3

JAN 12

F3.04_P3A: Water system servicing location


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The ATR 42 aeroplane has 1 cabin crew station and the ATR 72 has 2 cabin crew

stations.

The seat belt must be stowed correctly in the cavity located at the rear of thebackrest in order to avoid a damage of the belt after retraction of the seat pan.

3.05.1 LOCATION

Cabin crew seats are normally located near the emergency exits so that cabin crewcan quickly open the exit door in case of an emergency evacuation.

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CABIN CREW SEATS

3.05

P 1

JAN 12

Cabin Crew station

Cabin Crew station

Cabin crew station ATR 42

Cabin crew stations ATR 72

Senior Cabin Crew statio

F3.05_P1A: Cabin crew stations location


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3.05.2 DESCRIPTION

The cabin crew seats are used by the cabin crew during take-off and landing. Theyusually fold back of the way when not in use to keep the aisles, workspaces andemergency exits clear.

The cabin crew seats consist of:

A headrest with cushion A backrest with cushion A seat pan with cushion Seat belt and shoulder harness with a 4points center buckle A safety equipment stowage

3.05.2.1 MAIN CABIN CREW SEAT (REAR)

The rear cabin crew seat is installed in the entrance area and is a fixed seat.This is a forward facing seat equipped with harness and seat belt.

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CABIN CREW SEATS

3.05

P 2

JAN 12

Rear cabin crew seat ATR200/300/500

Seat harness ATR200/300/500

F3.05_P2A: Rear cabin crew seat

Rear cabin crew seat ATR 600

Seat harness ATR 600


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3.05.2.2 ADDITIONAL CABIN CREW SEAT ATR 72 (FWD)

A second cabin crew seat is mandatory on ATR 72 which should be operated with aminimum of 2 cabin crew complement. The additional cabin crew seat is located infront of the passenger cabin (Rearward-facing) and is equipped with harness andseat belt.

On ATR 72-200 and 72-500 the seat slides inside a dedicated stowage.A knob lever controls release and locking of the seat

On ATR 72-600 the seat folds against the side panel before the cabin/cargodoor (Left hand side). A pull-lever located under the seat pan controls releaseand locking of the seat

All other features are similar to the rear cabin crew seat.

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CABIN CREW SEATS

3.05

P 3

JAN 12

F3.05_P3A: FWD cabin crew seat ATR 72

FWD cabin crew seatATR 72.200/500

FWD cabin crew seatATR 72.600

Release/locking lever


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3.05.3 EQUIPMENT

Each cabin crew seat Safety Equipment Stowage contains:

1 life jacket 1 torch 1 oxygen bottle with appropriate mask in a sterile pouch 2 manual release tools (MRT)

3.05.4 CREW REST AREA

The ATR aeroplane does not have any specific crew rest area.

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CABIN CREW SEATS

3.05

P 4

JAN 12

F3.05_P4A: Cabin crew seat safety equipment


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3.06.1 GENERAL DESCRIPTION

The FAP/CMS is located above the main cabin crew seat, at the rear of theaeroplane.

All FAP/CMS models control: The lighting in the Galley / Lavatory / Cargo / Cabin The emergency lighting The BMG and pre-recorded audio announcement system

All FAP/CMS models indicate:

A call from the captain, cabin or lavatory The detection of smoke in the aft cargo or lavatory DC and ACW power availability The non smoking and seat belt sign ON/OFF status Lavatory occupancy status

On ATR 600 CMS, additional indications are available:

No electronic device status Cabin temperature FAP customization

Maintenance

Note:An older FAP version is still available on few not retrofitted aeroplane.

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FLIGHT ATTENDANT PANEL/CABIN MANAGEMENT SYSTEM

3.06

P 1

JAN 12

F3.06_P1B: ATR 500FAP

F3.06_P1C: ATR 200/300 FAP

F3.06_P1A: ATR 600 CMS


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ATR 600 CMS

The system is operational as soon as 28VDC power is present. No ON/OFFswitch has to be manipulated.

The FAP is a complex system based on a computer machine running anoperating system. There are two computers, one for the CMS, and one for theVIDEO. The GUI (Graphical User Interface) is managed by the CMS computer.The system initialization is done in 45-50seconds.

The navigation bar is dedicated to the navigation between pages. Each page canbe considered as a tab, and only one tab can be displayed at a time. Theselection of a page is simply done by pressing the corresponding icon in thenavigation bar. If allowed, the icon becomes white and the corresponding page isshown. Only one icon can be white at a time in the navigation bar.

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3.06

P 2

JAN 12

F3.06_P2A: ATR 600 CMS

Calls display

Cabin signs

Brightness adjustment

GND Service Bus

Navigation bar

F3.06_P2B: CMS Navigation bar


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ScreensaverThis page shows a picture freely selectable and loadable. Usually theairline logo is shown on this page.

WelcomeThis page shows a message (For example welcome on board); theflight number; the destination

Cabin LightingThis page allows managing the cabin lighting

TemperatureThis page allows showing the cabin temperature in degrees Celsiusand Fahrenheit

AudioThis page allows managing the audio (cabin announcements,music)First select the audio file from the list, then play / pause / stop.

Video (optional)This page allows managing the video (See IFE chapter for operation)

ParametersThis icon must be pressed for 3 seconds to validate the selection.8 types of parameters are available:

Airline logo Welcome message Flight number Destination Screen saver Music

Pre-recorded Announcements Video

The data can be chosen either from the CMS or can be importedfrom a memory stick (USB key).

MaintenanceThis icon must be pressed for 3 seconds to validate the selection.It allows having some information regarding the CMS configuration.

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3.06

P 3

JAN 12


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3.06.2 LIGHTING SYSTEM

Normal cabin lighting is operated from the FAP/CMS.

LATERAL/CEILING: 4 lighting levels are available offering 100%, 50%,25%, 10% of intensity. To increase the level light,press "+"; to decrease the level light, press "-"; Toturn off the lights, press - until the four (4)indicators lights are turned off.

GALLEY: Monitor the galley lighting

LAV: When selected, the lavatory light will come onautomatically when the lavatory door is locked

ENTRANCE: Monitor the rear entrance lighting

CARGO: Monitor the cargo lighting.Note: A separate lighting is also installed into the rear cargocompartment

READING:Allows passenger lights to become operational

On ATR 600 CMS two (2) additional lightings are available: PSU ambient white PSU ambient blue

Either one or the other can be selected.

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3.06

P 4

JAN 12

F3.06_P4B: FAP lighting control ATR 500F3.06_P4A: CMS lighting control ATR 600


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3.06.3 GROUND SERVICE BUSES

The power in the cabin is fed with 2 main types of electricity: DC 28V and AC115V. (See chapter 1.08 Electrical power)

When arriving on board the aeroplane, both Ground Service Bus commands (DCand AC) should be turned on.

3.06.4 TWO MINUTES MINIMUM LIGHTING

On ground, if the aeroplane is not connected to any power source, it is possibleto obtain 2 minutes of minimum cabin and flight crew compartment lighting.

A light in the flight crew compartment (above the observer seat) together with theforward and aft cabin EXIT SIGNS (in between LR1 and LR2) will illuminate.The 2 minutes lights push button switch is located on the panel at the right handside of the entrance door.

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3.06

P 5

JAN 12

2 minutes lights switch

Exit signs

F3.06_P3A: 2 minutes lighting locations


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On ATR 72 only, a tail prop is available and must be installed on the tail skid to

avoid a possible pulling-up of the aeroplane during passenger boarding anddisembarking.

3.07.1 DESCRIPTION

The tail prop is a metallic cylinder installed below the tail in order to avoid theaeroplane to tip up on the tail in case of persons (above 7) moving around duringoff loading.

3.07.2 INSTALLATION

Remove the tail prop from its location Insert the tail prop metal pin into the aeroplane tail skid connector

3.07.3 PRE-FLIGHT CHECK

Availability at correct location. The tail prop is stored in the rear unpressurisedarea of the aeroplane, beyond the aft bulkhead, or as an optionnext to the rearcabin crew seat.

IMPORTANT: Pre-flight check and installation of the tail prop is usually a ground

personnel duty, however cabin crew should be familiar with its operation asground assistance might not always be available.

The cabin crew must always ensure in all case that the tail prop has beeninstalled before boarding and disembarking passengers.

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TAIL PROP ATR 72

3.07

P 1

JAN 12

F3.07_P1A: ATR 72 tail prop

Tail skid

Tail prop


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4.00 CONTENTS

4.01 AIR CONDITIONING SYSTEM AND TEMPERATURE CONTROL

4.01.1 AIR CONDITIONING SYSTEM4.01.2 TEMPERATURE CONTROL

4.02 SMOKE WARNING SYSTEM

4.02.1 DESCRIPTION AND LOCATION4.02.2 ACTIVATION

4.03 LAVATORY AUTOMATIC FIRE EXTINGUISHER

4.03.1 DESCRIPTION AND LOCATION4.03.2 ACTIVATION

4.04 EMERGENCY LIGHTING SYSTEM

4.04.1 DESCRIPTION4.04.2 LOCATION4.04.3 ACTIVATION4.04.4 PRE-FLIGHT CHECK

4.05 OXYGEN SYSTEM

4.05.1 DESCRIPTION4.05.2 ACTIVATION

4.06 INFLIGHT ENTERTAINMENT SYSTEM (IFE)

4.06.1 AUDIO AND OPTIONAL VIDEO ON ATR 600 CMS4.06.2 OPTIONAL IFE SYSTEM ON ATR 500

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AEROPLANE SYSTEMS

CONTENTS

4.00

P 1

JAN 12


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4.01.1 AIR CONDITIONING SYSTEM

The air conditioning system is supplied by air processed through 2 packs whichregulate air flow and temperature as required.

The 2 packs are installed in the main landing gear fairings and operate automaticallyand independently.

The left pack supplies the cabin and the flight crew compartment, the right packsupplies only the cabin.

Note: If one pack is inoperative, the other one supplies both compartments throughthe mixing chamber.

Air ventilation:

Conditioned air is blown into the cabin by outlets ramps located under the overheadlockers. It is then evacuated through guides along the cabin side walls at floor level.A part of it is re-circulated by the fans, the other part being evacuated overboardthrough the outflow valves installed in the rear under floor.

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AEROPLANE SYSTEMS

AIR CONDITIONING SYSTEM/TEMPERATURE CONTROL

4.01

P 1

JAN 12

PACK

1PACK

2

GENERAL AIR INLET

OUTFLOW VALVESPACK

LAVATORY VENT LINE

AIROUTLET

F4.01_P1A: AC packs view

F4.01_P1B: Air circuit


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4.01.2TEMPERATURE CONTROL

The system is designed to regulate and limit the temperature of the air dischargedfrom the packs. The temperature is controlled either automatically or manually onlyby the flight crewby setting the compartment temperature selectors on the COMPTTEMP PANEL (compartment temperature panel).

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AEROPLANE SYSTEMS


4.01

P 2

JAN 12

F4.01_P2C: Flight crew compartmentoverhead panel COMPT TEMP PANEL

F4.01_P2A: Air conditioning pack left hand side F4.01_P2B: Air conditioningpack right hand side


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The cabin crew has no possibility to control the cabin temperature. However on ATR 600 the

cabin temperature can be display on the CMS by pressing the temperature icon on thenavigation bar. The temperature shows in degrees Celsius and Fahrenheit.

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AEROPLANE SYSTEMS


4.01

P 3

JAN 12

F4.01_P3A: Cabin Temperature icon on CMS navigation bar .

F4.01_P3B: Cabin Temperature display on CMS.


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4.02.1 DESCRIPTION AND LOCATION

Four smoke detectors are located on board the aeroplane:

One in the FWD cargo compartment ceiling(For detection in the FWD cargo compartment)

One under the FWD cargo compartment floor - not visible to the crew(For detection in the electric/electronic systems)

One in the AFT cargo compartment ceiling(For detection in the AFT cargo compartment)

One in the AFT cargo compartment ceiling panel - not visible to the crew(For detection in the lavatory)

The whole system can be tested from the flight crew compartment only.

As part of the pre-flight checks, the cabin crew will visually inspect:

The AFT cargo compartment smoke detector The lavatory smoke detector duct (Duct leading to the smoke detector)

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AEROPLANE SYSTEMS

SMOKE WARNING SYSTEM

4.02

P 1

JAN 12

F4.02_P1B: Lavatory smoke detector ductF4.02_P1A: AFT cargo compartmentsmoke detector


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4.02.2 ACTIVATION

If smoke is detected in any area, the system provides Continuous Repetitive Chime(CRC) warning and visual indications on the alerting window of the central instrumentpanel in the flight crew compartment. The pilots can silence the aural indications bypressing the Master Caution button, however the visual warnings will onlyextinguish when smoke is no longer detected in the area.

4.02.2.1 FWD CARGO COMPARTMENT SMOKE DETECTORS

If smoke is detected in the forward cargo compartment or electric/electronic bay, thesystem gives CRC and visual warning to the flight crew members only.

4.02.2.2 AFT CARGO COMPARTMENT AND LAVATORY SMOKE DETECTORS

If smoke is detected in the AFT cargo compartment or the lavatory, the system givesCRC and visual warning to the flight crew members and visual warning onlyon theFAP/CMS to the cabin crew members.

The affected area light will illuminate STEADY red on the FAP/CMS.

C.C.O.M


AEROPLANE SYSTEMS


4.02

P 2

JAN 12

F4.02_P2B: Flight crew compartmentsmoke alerting window ATR 200/300/500

F4.02_P2C: Aft cargo smoke detector light on FAP

F4.02_P2A: Flight crew compartmentsmoke alerting window ATR 600

ONON

F4.02_P2D: Lavatory smoke detector light on FAP


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C.C.O.M


AEROPLANE SYSTEMS


4.02

P 3

JAN 12

F4.02_P3A: smoke detector light on CMS


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4.02.2.3 AFT CARGO COMPARTMENT EXTINGUISHER CONNECTOR

The aft cargo area of the aeroplane being difficult to access, an extinguisherconnector located near the FAP has been installed. By discharging the halonextinguisher completely through this connector, the halon gas flows from the twodiffusers, located in the ceiling of the AFT cargo compartment (See also Chapter10.03 page 6)

The warning light on the FAP will only extinguish when smoke is no longer detectedin the area.

C.C.O.M


AEROPLANE SYSTEMS


4.02

P 4

JAN 12

F4.02_P4A: Aft cargo compartmentextinguisherconnector

F4.02_P4B: Aft cargo compartment extinguisherdiffuser


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4.03.1 DESCRIPTION AND LOCATION

The lavatory waste bin is equipped with an automatic fire extinguisher that contains120g of chemical product Bromotrifluoromethane (Halon 1301 - CF3 Br)

4.03.2 ACTIVATION

If there is a fire in the waste bin, the fire extinguisher operates automatically.

When the temperature reaches approximately 78C (17 4F) the plug installed in theend of the discharge tubes melts and lets the agent flow into the waste bin.

IMPORTANT: Due to the difficulty to access the lavatory automatic fire extinguisher adaily check is normally done by engineering.According to operator standard procedures, the cabin crew could be asked toperform the pre-flight check as well (checking that the plugs on the extinguishernozzles are still in place).In all cases cabin crew must always check that the waste bin flap cover is properlyclosed.

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AEROPLANE SYSTEMS

LAVATORY AUTOMATIC FIRE EXTINGUISHER

4.03

P 1

JAN 12

F4.03_P1B: Lavatory waste bin flap cover

F4.03_P1A: Lavatory waste bin automatic fire extinguisher


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The emergency lighting system has the purpose to guide the aeroplane occupants to

the exits in case of essential power failure. In case of activation, the system has a 10minutes capacity.

4.04.1 DESCRIPTION

The emergency lighting is composed of the following equipment:

EXIT SIGNS located in the aisle in the overhead position.They show the direction to the next exit.

EXIT LIGHTS located beside the emergency exit doors.They show the position of the exit.

EMERGENCY CEILING LIGHT to illuminate the aisle.

PHOTOLUMININESCENT FLOOR PROXIMITY EMERGENCYESCAPE PATH MARKING based on the use of a material which isable to store natural or electrical light energy and to restore thisenergy gradually in the form of light in the dark. The minimumrechargeable time recommended before each flight is 15 minutesin order to obtain full lighting in case of an emergency evacuation.

EXTERNAL EMERGENCY LIGHTS located on the fuselageadjacent to each exit, and at the bottom of the entrance door

stairs.

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AEROPLANE SYSTEMS

EMERGENCY LIGHTING SYSTEM

4.04

P 1

JAN 12

F4.04_P1A: Emergency lights description


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4.04.2 LOCATION

Note: The emergency light location may vary according to aeroplane versions.

4.04.3 ACTIVATION

The emergency lighting system will activate automatically in case of power failure, ifthe toggle switch in the flight crew compartment overhead panel is on the ARM

position.The emergency light can also be activated by the flight crew by setting the switch toON or by the cabin crew by pressing the EMER. LIGHT guarded push on the FAP.The emergency lights activation from the FAP/CMS is possible regardless of th

Documents

ATR 42 - Cabin Crew Operating Manual