A330 Cabin Crew Procedure Manual

8/20/2019 A330 Cabin Crew Procedure Manual

1/202

AIRBUS 330

CABIN CREW PROCEDURES MANUAL

PART B – AEROPLANE OPERATING MATTERS


2/202

INTENTIONAL BLANK PAGE


3/202


4/202


5/202

AIRBUS 330 CABIN CREW PROCEDURES MANUAL

This AIRBUS 330 CABIN CREW PROCEDURES MANUAL is publishedby Vietnam Airlines Cabin Crew Department under the authorisation of theVietnam Airlines, Vice President Operations. Any questions with respect tothe use of this manual or information contained herein should be

addressed to:

Cabin Crew Department115 Hong Ha Street, Ward 2, Tan Binh DistrictHO CHI MINH CITYVIETNAM

Fax: +84 8 3844 6333Tel: +84 8 3848 5334 Ext 8513

Attn: Safety/Service Quality Section


6/202




7/202

LONR 1

AIRBUS 330 CABIN CREW

PROCEDURES MANUAL

LIST OF NORMAL REVISIONSRev 02

10 Dec 07

REVNO

ISSUEDDATE

EFFECTIVEDATE

APPROVAL

00 01 Aug 06

01 01 Jun 07

02 10 Dec 07 01 Feb 08

03

26 Oct 06

15 Jul 07


8/202

LONR 2


PROCEDURES MANUAL

LIST OF NORMAL REVISIONSRev 02

10 Dec 07



9/202


TABLE OF MANUAL DISTRIBUTION

NO HOLDER QUANTITY

1. Civil Aviation Administration of Vietnam 01

2. President & CEO 01

3. Vice President & CEO 05

4. Flight Operation Department 04

5. Safety & Security Department 02

6. Quality Assurance Department 02

7. Training Department 01

8. Flight Crew 919 05

9. Flight Training Center 10

10. Noibai Operation Control Center 01

11. Tansonnhat Operation Control Center 01

12. Cabin Crew Department 20

13. Each Cabin Crew Member 01


10/202




11/202

LOEP 1

AIRBUS 330 CABIN CREWPROCEDURES MANUAL

LIST OF EFFECTIVE PAGESRev 02

10 Dec 07

Page Rev Issued Date Effective Date

AUTHORISATION PAGE LIST OF NORMAL REVISIONS

LONR 1-2 02 10 Dec 07 01 Feb 08


LIST OF EFFECTIVE PAGES

LOEP 1-2 02 10 Dec 07 01 Feb 08

TABLE OF CONTENTS

TOC/P1-2 00 01 Aug 06 26 Oct 06

RECORD OF REVISIONS

ROR 1-2 00 01 Aug 06 26 Oct 06

RECORD OF BULLETINS

ROB 1-2 00 01 Aug 06 26 Oct 06

SECTION 0INTRODUCTION

TOC/P1-2 00 01 Aug 06 26 Oct 06

0.1/P1-2 01 01 Jun 07 15 Jul 07

0.2/P1-2 00 01 Aug 06 26 Oct 06

SECTION 1

AIRCRAFT EQUIPMENT

TOC/P1-2 00 01 Aug 06 26 Oct 06

1.1/P1-10 00 01 Aug 06 26 Oct 06

1.2/P1-32 00 01 Aug 06 26 Oct 06

1.3/P1-8 00 01 Aug 06 26 Oct 06


12/202

LOEP 2


LIST OF EFFECTIVE PAGESRev 02

10 Dec 07

Page Rev Issued Date Effective Date1.4/P1-14 00 01 Aug 06 26 Oct 06

1.5/P1-10 00 01 Aug 06 26 Oct 06

1.6/P1-2 00 01 Aug 06 26 Oct 06

1.7/P1-32 00 01 Aug 06 26 Oct 06

1.8/P1-2 00 01 Aug 06 26 Oct 06

1.8/P3-4 02 10 Dec 07 01 Feb 08

1.8/P5 00 01 Aug 06 26 Oct 06

1.8/P6 02 10 Dec 07 01 Feb 08

1.8/P7-14 00 01 Aug 06 26 Oct 06

SECTION 2

AIRCRAFT PROCEDURES

TOC/P1-2 00 01 Aug 06 26 Oct 06

2.1/P1-6 00 01 Aug 06 26 Oct 06

SECTION 3

EMERGENCY PROCEDURES

TOC/P1-2 00 01 Aug 06 26 Oct 06

3.1/P1-2 00 01 Aug 06 26 Oct 06

3.2/P1-4 00 01 Aug 06 26 Oct 06

3.3/P1-6 00 01 Aug 06 26 Oct 06

3.4/P1-2 00 01 Aug 06 26 Oct 06

3.5/P1-2 00 01 Aug 06 26 Oct 06

3.6/P1-4 00 01 Aug 06 26 Oct 063.7/P1-6 00 01 Aug 06 26 Oct 06

3.8/P1-2 00 01 Aug 06 26 Oct 06

3.9/P1-8 00 01 Aug 06 26 Oct 06


13/202

TOC/P1

AIRBUS A330 CABIN CREW

PROCEDURES MANUAL

TABLE OF CONTENTSRev 00

01 Aug 06

AUTHORISATION PAGE


LIST OF EFFECTIVE PAGES

TABLE OF CONTENTS

RECORD OF REVISIONS

RECORD OF BULLETINS

SECTION 0 – INTRODUCTION

0.1 GENERAL

0.2 AMENDMENT AND REVISIONSECTION 1 – AIRCRAFT EQUIPMENT

1.1 AIRCRAFT DESCRIPTION

1.2 CONTROL PANELS

1.3 LIGHTING

1.4 COMMUNICATIONS

1.5 LAVATORIES

1.6 GALLEYS1.7 DOORS, SLIDES AND EMERGENCY EXITS

1.8 EMERGENCY EQUIPMENT

SECTION 2 – AIRCRAFT PROCEDURES

2.1 GENERAL

SECTION 3 – EMERGENCY PROCEDURES

3.1 INTRODUCTION

3.2 PREPARED EMERGENCY LANDING3.3 PREPARED EMERGENCY LANDING CHECKLIST

3.4 UNPREPARED EMERGENCY LANDING

3.5 REJECTED TAKEOFF OR A LANDING THAT DOES NOT APPEARNORMAL

3.6 EVACUATION PROCEDURES

3.7 FIRE AND SMOKE PROCEDURES

3.8 DECOMPRESSION PROCEDURES

3.9 MISCELLANEOUS PROCEDURES


14/202

TOC/P2

AIRBUS A330 CABIN CREW

PROCEDURES MANUAL

TABLE OF CONTENTSRev 00

01 Aug 06



15/202

ROR 1


PROCEDURES MANUAL

RECORD OF REVISIONSRev 00

01 Aug 06

REVISIONNUMBER

ISSUEDDATE

DATEINSERTED

SIGNATURE

01 01 Jun 07 15 Jul 07

02 10 Dec 07 01 Feb 08


16/202

ROR 2


PROCEDURES MANUAL

RECORD OF REVISIONSRev 00

01 Aug 06



17/202

ROB 1


PROCEDURES MANUAL

RECORD OF BULLETINSRev 00

01 Aug 06

BULLETINNUMBER

DATEINSERTED

SIGNATURE DATEREMOVED

SIGNATURE


18/202

ROB 2


PROCEDURES MANUAL

RECORD OF BULLETINSRev 00

01 Aug 06



19/202


SECTION 0

INTRODUCTION


20/202




21/202

TOC/P1


PROCEDURES MANUAL

INTRODUCTIONRev 00

01 Aug 06

TABLE OF CONTENTS

0.1 GENERAL 0.1/P1

0.2 AMENDMENT AND REVISION 0.2/P1


22/202

TOC/P2


PROCEDURES MANUAL

INTRODUCTIONRev 00

01 Aug 06



23/202

0.1/P1


PROCEDURES MANUAL

INTRODUCTIONRev 01

01 Jun 07

0.1 GENERAL

0.1.1 This Airbus 330 Cabin Crew Procedures Manual contains proceduresand information specific to the Airbus 330 aircraft and should be read inconjunction with the Cabin Crew Safety Manual. This manual is stowedin document library in the cockpit of the Airbus 330 aircraft.

Some essential information of this manual are extracted to compose theCabin Crew Quick Reference Manual. Cabin crew are required to carrytheir personal copy of the Cabin Crew Quick Reference Manual withthem when they are working as operating crew on this aircraft type.

R


24/202

0.1/P2


PROCEDURES MANUAL

INTRODUCTIONRev 01

01 Jun 07


0 2/P1


25/202

0.2/P1


PROCEDURES MANUAL

INTRODUCTIONRev 00

01 Aug 06

0.2 AMENDMENT AND REVISION

0.2.1 The Airbus 330 Cabin Crew Procedures Manual is issued on theauthority of the Vice President Operations who will authorise allamendments to it, as required by the Company. All amendments will bein the form of printed, replacement pages; manuscript amendments arenot permitted. Revision pages will be annotated to show the date ofissue (and date of effect if different); the amendment list number, and theportion of the text which has been revised, as indicated by verticalmarginal lines adjacent to the changes. Each amendment will beaccompanied by a revised list of effective pages, with their dates ofissue, and by a certificate of receipt/incorporation. An amendment list

record (Record of Revisions) will be maintained at the front of eachmanual.

0.2.2 The Company will ensure that a copy of the Airbus 330 Cabin CrewProcedures Manual is provided for each appointed cabin crew memberand for the CAAV. The Company will maintain an up-to-date list ofmanuals together with their copy numbers and the name/appointment ofeach copy holder as appropriate. Amendments will be issued to all suchholders, who will be required to amend their copies and return theircertificates of incorporation to the Company as soon as possible afterthe amendment has been completed.

0.2.3 Details of revisions which may be urgently required in the interests offlight safety, or which are supplementary to the Airbus 330 Cabin CrewProcedures Manual, will be promulgated as bulletins and issued on bluepaper. Those of a temporary nature will be cancelled as soon as theyare no longer relevant. Those of long-term application will beincorporated into the manual when it is next amended, or within sixmonths of their effective date, whichever is the sooner.

0.2.4 When the amendment/revision concerns any part of Airbus 330 CabinCrew Procedures Manual which must be approved by the CAAV, this

appoval must be obtained before amendment or revision are required inthe interest of safety, they may be published and applied immediately,provided that application for approval has been made.

0 2/P2


26/202

0.2/P2


PROCEDURES MANUAL

INTRODUCTIONRev 00

01 Aug 06



27/202


SECTION 1

AIRCRAFT EQUIPMENT


28/202



TOC/P1


29/202


PROCEDURES MANUAL

AIRCRAFT EQUIPMENTRev 00

01 Aug 06

TABLE OF CONTENTS

1.1 AIRCRAFT DESCRIPTION 1.1/P1

1.1.1 Introduction 1.1/P1

1.1.2 Aircraft Description 1.1/P1

1.1.3 Principal Dimensions 1.1/P2

1.1.4 Aircraft Systems – General 1.1/P3

1.1.5 Passenger Cabin – Systems 1.1/P4

1.1.6 Cabin Configuration 1.1/P81.1.7 Flight Deck Door 1.1/P9

1.2 CONTROL PANELS 1.2/P1

1.2.1 General 1.2/P1

1.2.2 CIDS Installation 1.2/P2

1.2.3 Forward Attendant Panel (FAP) 1.2/P3

1.2.4 Additional Attendant Panel (AAP) 1.2/P6

1.2.5 Programming and Indication Module (PIM) 1.2/P81.2.6 Cabin Crew Handset 1.2/P25

1.2.7 Attendant Indication Panel (AIP) 1.2/P27

1.2.8 Area Call Panel (ACP) 1.2/P32

1.3 LIGHTING 1.3/P1


1.3.2 Cabin Lighting Panel 1.3/P1

1.3.3 Lavatory Lighting 1.3/P3

1.3.4 Cabin Crew Station Work Light 1.3/P4

1.3.5 Passenger Reading Light 1.3/P5

1.3.6 Cabin Signs 1.3/P6

1.3.7 Emergency Lighting System 1.3/P7

1.4 COMMUNICATIONS 1.4/P1


1.4.2 Passenger Address System (PAS) 1.4/P1

1.4.3 Cabin Interphone System 1.4/P7

TOC/P2


30/202



01 Aug 06

TABLE OF CONTENTS (CONT)

1.4.4 Passenger Call System 1.4/P10

1.4.5 Evacuation Signaling System 1.4/P12

1.5 LAVATORIES 1.5/P1


1.5.2 System Components 1.5/P2

1.5.3 Controls 1.5/P7

1.5.4 Lavatory Fire Protection System 1.5/P7

1.5.5 Lavatory Door Emergency Unlocking Mechanism 1.5/P10

1.6 GALLEYS 1.6/P1

1.6.1 Galley System Overview 1.6/P1

1.6.2 Galley Non-Normal Operations 1.6/P2

1.7 DOORS, SLIDES AND EMERGENCY EXITS 1.7/P1

1.7.1 Introduction 1.7/P1

1.7.2 Warning System 1.7/P4

1.7.3 Operations of Doors from Inside 1.7/P5

1.7.4 Operations of Doors from Outside 1.7/P8

1.7.5 Slide Arming System 1.7/P10

1.7.6 Emergency Opening 1.7/P13

1.7.7 Evacuation Slides - General 1.7/P15

1.7.8 Slide/Raft 1.7/P16

1.7.9 Raft Canopy 1.7/P27

1.7.10 Survival Kits 1.7/P28

1.7.11 Transportation of raft to another Door 1.7/P28

1.8 EMERGENCY EQUIPMENT 1.8/P1


1.8.2 Oxygen Systems 1.8/P9

1.1/P1

AIRCRAFT EQUIPMENT


31/202



01 Aug 06

1.1 AIRCRAFT DESCRIPTION

1.1.1 IntroductionThis chapter provides a general description of the aircraft, principaldimensions and passenger cabin.

1.1.2 Aircraft Description

The AIRBUS A330-300 is a medium to long-range, twin aisle subsonictransport aircraft, powered by two turbo-fan engines.

(a) The fuselage has a circular cross section and is entirely pressurizedwith the exception of the nose and tail cone, the landing gear and

air conditioning compartments.

(b) The cockpit is arranged to allow a two crew member operation. Accommodation is provided for 2 observers.

Aircraft Model Airbus 330 - 300

Engines: General Electric GE CF6-80E1A2

Crew Captain and First Officer

Maximum takeoff weight: 217 000 kg (478 398 Ib)

Fuel capacity 97,171 litresCruising altitude 41,000 feet

Range 5,650 nautical miles

( 10,500 kilometres)

Business Class 36

Economy Class 284

Passenger capacity:

VN-A368

Total 320

Business Class 24Economy Class 242

Passenger capacity:VN-A369/370

Total 266

1.1/P2

AIRCRAFT EQUIPMENT


32/202



01 Aug 06

1.1.3 Principal Dimensions

1.1.3.1 A330 - 300

1.1/P3

AIRCRAFT EQUIPMENT


33/202



01 Aug 06

1.1.4 Aircraft Systems - General

1.1.4.1 Auxiliary Power Unit (APU)

An APU is a self-contained unit which makes the aircraft independent ofextenal pneumatic and electrical power supply. On ground, it suppliesbleed air for starting the engines and for the air conditioning system; andsupplies electrical power to the electrical supply. During take-off, itsupplies bleed air for air conditioning, thus avoiding a reduction in enginethrust caused by the use of engine bleed air for this purpose whenoptimum aircraft performance is required. In flight, it backs up theElectrical system and the Air conditioning, it can be used to start theengines.

1.1.4.2 Aircraft Electrical Power

The electrical power system consists of a three phase 115/200 volt 400Hertz constant frequency AC system and a 28 volt DC system.

Electrical transients are acceptable for equipment.

Commercial supply has secondary priority.

Normally, the system produces alternating current, some of which thentransform into direct current for certain applications.

Each of the aircraft’s three generators can supply the whole network.

If all normal AC generation is lost, an emergency generator can supply AC power.

If all AC generation is lost, the system can transform DC power frombatteries into AC power.

1.1.4.3 Air Conditioning and Pressurization

Normally, bleed air for air conditioning and pressurization is supplied bythe engines. The APU can also be used to supply bleed air.

Temperature is controlled separately for the flight deck and for theforward cabin, middle cabin, after cabin. Cabin crew can control cabintemperature through the control panel on the forward attendant panel. Itcan modify each cabin zone temperature demand from the cockpit,during cruise, with a limited authority of ±2.5

oC.

The cabin pressure is controlled automatically to provide a programmedcabin altitude.

1.1/P4

AIRCRAFT EQUIPMENT


34/202



01 Aug 06

1.1.5 Passenger Cabin - Systems

1.1.5.1 Cabin Systems Electrical Power

Electrical power to the cabin In-flight Entertainment Equipment (IFE) andgalley power systems is primarily controlled from the flight deck.

Additional control of the IFE system is available to the cabin crewthrough the IFE Master Power switch located in the Video Control Center(VCC). Galley power may be turned off by moving the appropriate galleyEmergency Power switch to the OFF position.

1.1.5.2 Cabin Doors

Refer Chapter 1.7, Doors, Slides and Emergency Exits, for detailed

information.

1.1.5.3 Galleys

The galleys have provisions for storing and preparing food andbeverages. Removable containers, which insert and latch into the galleywalls, are used for replenishment of supplies, food, beverages, andwaste storage. The galleys are equipped with electrical power and waterservices.

Refer Chapter 1.6, Galleys, for detailed information.

1.1.5.4 Lavatories

Each lavatory contains a toilet, wash basin, mirror, and all the necessaryvanity items and disposal units. Some of the lavatories have baby carestations and handicap provisions. The lavatories contain two oxygenmasks which deploy automatically during cabin depressurization.Ventilation is provided for each lavatory and air exhausts throughoverboard vents.

Refer Chapter 1.5, Lavatories, for detailed information.

1.1.5.5 Closets and Partitions Closets are installed in the forward half of the aircraft. Partitions,lavatories, and galleys are used to separate class seating. Somepartitions have literature pockets.

1.1.5.6 Overhead Stowage Bins

There are storage bins located in the ceiling over doors 1L, 1R, 4L, and4R.

Overhead passenger storage bins are installed over both the outboard

and center seats to accommodate blankets, pillows, and carry-on items.

1.1/P5

AIRCRAFT EQUIPMENT


35/202



01 Aug 06

Emergency equipment may also be stored in the bins. Each bin has aplacard stating its maximum weight capacity.

1.1.5.7 Passenger and Cabin Crew Seating

(a) Passenger Seating

Accommodations are provided for each passenger class. Apassenger control unit (PCU) is provided in each seat arm rest.Passengers may use the PCU to make entertainment selections,turn the reading light on or off, or call for passenger service.

(b) Cabin Crew Seating

The cabin crew seats automatically return to the stowed positionwhen unoccupied. A combination seat belt/shoulder harness anda padded head rest are installed in the seat. The harnessfunctions as an inertia restraint device and retracts into a stowedposition when not in use. The buckle has a release plate thatmust be moved through 90 degrees for release to occur.

Note: Designated cabin crew direct view seats must beoccupied by cabin crew during taxi, takeoff and landing.

Cabin crew service units each containing an oxygen mask foreach cabin crew position are installed at each location.

1.1.5.8 Cabin Crew Stations

Cabin crew stations are located at each door and include an attendantswitch panel, service unit, attendant work lights, handset, seats, andcabin area control panels.

Designated emergency equipment and a service unit containing oxygenmasks are located at each cabin crew station.

The Forward Attendant Panel (FAP) is installed at the Forward Attendant

Station and the Additional Attendant Panels (AAP) are located at CAStation 2L and 4L.

1.1/P6

AIRCRAFT EQUIPMENTR 00


36/202


Rev 00

01 Aug 06

1.1/P7



37/202


Rev 00

01 Aug 06

1.1.5.9 Passenger Service Units

The passenger service units are located immediately below the

overhead stowage bins. Each unit has reading lights, controlled by aswitch in the passenger seat arm rest, an attendant call light, and a seatlocator sign.

1.1.5.10 Emergency Oxygen

Passenger oxygen masks are located in overhead modularcompartments. One mask is supplied for each passenger seat and twofor each lavatory. An extra mask is located in both the center andoutboard passenger seat units. Oxygen is available for approximately 15minutes.

Refer Chapter 1.8, Emergency Equipment, for detailed information.

1.1/P8



38/202


Rev 00

01 Aug 06

1.1.6 Cabin Configuration

1.1/P9



39/202


Rev 00

01 Aug 06

1.1.7 Flight Deck Door

1.1.7.1 General

A forward opening hinge door separates the flight deck from thepassenger cabin. It has an electric locking latch controlled by the flightdeck crew.

In normal conditions, when the door is closed, it remains locked. Uponflight deck entry request the flight crew can authorize entry by unlockingthe door which remains closed until it is pushed open.

When the flight deck crew does not respond to requests for entry thedoor can be unlocked by the cabin crew by entering a two (2) to seven

(7) digit code (programmed by VAC) on the keypad installed on the doorpost.

The door is bullet proof and fully compliant with decompressionrequirements.

A mechanical override enables the pilots to open the door from theinside.

1.1.7.2 Flight Deck Emergency Access Panel

The flight deck door locking system provides a means of electrically

locking and unlocking the flight deck door.

The keypad enables cabin crew to request entry to the flight deck. Thereare two different request types:

(a) Routine Access:

Press the “#” key on the keypad and wait for the flight deck doorto be opened by the flight deck crew.

(b) Emergency Access:

The emergency access code is only to be used in the case offlight deck crew incapacitation.

A toggle switch allows the flight deck crew to lock or unlock the flightdeck door following an access request thereby allowing or denying entryto the flight deck.

1.1/P10




40/202

AIRBUS 330 CABIN CREWPROCEDURES MANUAL 01 Aug 06

1.1.7.3 Keypad

The keypad is used by cabin crew to request the flight deck crew to open

the flight deck door.

(1) LOCKED/UNLOCKED INDICATOR:

GREEN light ON

The door has been unlocked either by a flight crew action, orautomatically (during 5 seconds) when no flight crew action isperformed during the delay following an emergency accessrequest. The door can be pushed open.

GREEN light flashes

An emergency request to enter the flight deck has been made.The buzzer in the flight deck will sound continuously in the flightdeck but the flight crew have taken no action.

RED light ON:

The flight crew has denied access.

(2) Digital Keypad:

The keypad is used to sound a buzzer in the flight deck for one(1) to nine (9) seconds by entering a zero to seven digit code asprogrammed by VAC, follows by the “#” key.

It is also used to enter the two to seven digit emergency codefollowed by the “#” key when the flight deck crew does not

respond.

1.2/P1




41/202


1.2 CONTROL PANELS

1.2.1 General

The Cabin Intercommunication Data System (CIDS) is a microprocessor-based system. It is used to do functional control, testing and monitoringof the cabin systems. The CIDS integrates most of the cabin systems forcommunications, calls and indications:

(a) Passenger address;

(b) Cabin and flight deck interphone;

(c) Cabin illumination;

(d) Evacuation signalling;

(e) Lavatory smoke indication;

(f) Passenger lighted signs;

(g) Passenger call;

(h) Service interphone;

(i) Emergency lighting test;

(j) Passenger reading lights;

(k) Pre-recorded announcement and boarding music controls;

(l) Passenger entertainment music control;

(m) Passenger entertainment video control;

(n) Doors/slides related indication;

(o) Water/Waste related indication;

(p) Air Conditioning (temperature indication and control).

1.2/P2




42/202


1.2.2 CIDS Installation

1.2/P3



01 A 06


43/202

US 330 C CPROCEDURES MANUAL 01 Aug 06

1.2.3 Forward Attendant Panel (FAP)

Location:

The FAP is installed at the Forward Attendant Station. It controls thecabin systems and indicates the status of the systems.

1.2/P4



01 Aug 06


44/202

PROCEDURES MANUAL 01 Aug 06

Description:

On the FAP, the attendants can control the different cabin systems andthe CIDS. It shows the attendants the status of the systems and they can

do the programming.

(a) Cabin Light Panel

(i) The cabin lighting section of the basic FAP consists ofdifferent pushbuttons, which control the passenger cabinlights, aisle, windows, centre ceiling. Each buttonilluminates when selected.

(ii) The “ENTRY” section controls the lights in the entranceareas.

(iii) The “LAV MAINT” switch is provided for the lavatorycontrol the lighting service function.

(b) Miscellaneous

(i) The “EMER” pushbutton is used for the manualillumination of the emergency lights.

(ii) The “SMOKE LAV” indication lamp flashes when smoke isdetected in any lavatory.

(iii) The “EVAC CMD” pushbutton activates the evacuationsystem warnings.

1.2/P5



01 Aug 06


45/202

PROCEDURES MANUAL 01 Aug 06

(iv) The “EVAC/RESET” pushbutton cancels some of thewarnings.

(v) The “CHIME INHIB” switch is provided for inhibited thecentralized calls from PAX.

(vi) The “CALL RESET” pushbutton is used to cancel allilluminated passenger call signs.

(c) The BGM (Back Ground Music) panel comprises the “ON/OFF”switch, a “SEL” pushbutton to set the music channel, a “+” and “-“pushbutton to increase or decrease the volume and a volumemanometer.

(d) The Programming and Indication Module (PIM) of the FAPconsists of a Liquid Cristal Display (LCD).

(e) These pushbuttons allow the page handling of the systemindications and programming features of the PIM.

(f) The numerical keypad (0 to 9) is used to select the number of arecorded announcement or a passnumber. The “ENTER” and“CLEAR“ pushbuttons set or cancel a selected announcement.

(g) The “CIDS CAUT” pushbutton illuminates whenever a failure of aCIDS or a connected system occured. The “PNL LIGHT TEST”

checks the LCD and the integrated light in the FAP pushbuttons.

1.2/P6



01 Aug 06


46/202

PROCEDURES MANUAL 0 ug 06

1.2.4 Addi tional Attendant Panel (AAP)

The intensity of the lights of the different Entry Areas (mid/aft) and cabin

sections can also be controlled from the Additional Attendant Panels.The operation is the same as the operation from the forward panel.

1.2.4.1 Location

Additional Attendant Panels (AAP) are located at C/A Station 2L and 4L.

1.2/P7



01 Aug 06


47/202

PROCEDURES MANUAL g

1.2.4.2 Description

The AAP can include optional pushbuttons for the cabin lights control theillumination intensity of the entry areas and the different cabin sections.

(a) The “EVAC CMD” button activates the EVAC signals.

(b) The “EVAC RESET” pushbutton cancels the audio signals.

(c) The “CALL RESET” pushbutton is used to cancel all illuminatedpassenger call signs.

(d) The “SMOKE LAV” indication lamp flashes when smoke isdetected in a lavatory.

(e) The “CHIME INHIB” silences the passengers call sound.

(f) The “CABIN-DIM 1-DIM 2” pushbuttons control the light intensityof the rear cabin.

(g) The “ENTRY-DIM 1-DIM 2” pushbuttons control the light intensity

of the rear entry area.

1.2/P8



01 Aug 06


48/202

1.2.5 Programming and Indication Module (PIM)

1.2.5.1 General

Failure annunciations in the cabin are provided on the PIM(Programming and lndcation Module) which is part of the Forward Attendant Panel.

The PIM has no system test facilities, it is only used for systemindications and programming operations.

1.2/P9



01 Aug 06


49/202

1.2.5.2 Description

The PIM is equipped with a coloured full graphic Liquid Cristal Display.

Twelve softkeys are attached to this display for menu guided operations.

The hardkeys provide direct access to the respective menus.

To allow numeric inputs to the system the PIM is provided with astandard keyboard with twelve pushbuttons.

The Panel light test pushbutton enables all the lights integrated in theFAP to be tested.

The CIDS CAUTION light is automatically activated in case of a systemfailure, when the light is on, the Cabin Crew must have a look at the PIM

display.

1.2.5.3 Operation

NORMAL MODE

When power is connected to the aircraft, a power up test page appearson the PIM. This page disappears after end of test.

The PIM display is normally blank, if no page is selected manually orautomatically displayed.

In general the PIM has a time out of 10 minutes after a page wasmanually selected.

1.2/P10



01 Aug 06


50/202

If a function is selected via a hardkey, the PIM displays the relevant pageimmediately. If this key is pressed a second time or when another page isselected, this page disappears.

AUTOMATIC MODE

If a failure occurs the CIDS CAUTION light comes on. Now two differentconditions can occur:

(a) A page was manually selected and is displayed on the screen:

A message appears in amber in the information row to inform thecrew of a required action.

(b) No page is displayed on the screen, then either

(i) The DOORS/SLIDES page comes on with an indication of thefailure or

(ii) The SYSTEM CHECK menu comes on and the symbol in front ofthe system which failed, flashes.

1.2/P11



01 Aug 06


51/202

The CIDS CAUTION light can be reset inflight by pushing it.

It comes on again in case of another failure or automatically after landingif the failure still exists.

The reset has no consequences for the PIM messages.

1.2.5.4 System Check

NORMAL MODE

On pressing the “SYS CHECK” hardkey, the SYSTEM CHECK page isdisplayed.

1.2/P12



01 Aug 06


52/202

It may be called up for preflight checks.

AUTOMATIC MODE

If a failure is detected on one of the cabin systems, the” SYSTEMCHECK “ page or the information “ SELECT SYSTEM CHECK” isautomatically displayed.

1.2.5.5 Layout selection

The layout information is recorded in the Cabin Assignement Module(CAM) fitted in the FAR The cabin LAYOUT pages on the PIM allowmodifications. The access to the LAYOUT page is protected by a codenumber and only accessible on ground.

1.2/P13



01 Aug 06


53/202

CABIN ZONES PROGRAMMING

Normal mode (NO AUTOMATIC MODE)

On pressing “ZONE PROG” hardkey, the zones programming page isdisplayed.

These pages provide the menus for the cabin zones and for the nosmoking zones programming.

Cabin zones are defined by passenger classes and attendant workingareas. Cabin functions like passenger address, general illumination,passenger call, video tone or chimes for interphone and signs arerelated to these zones according to customer requests.

1.2/P14



01 Aug 06


54/202

By means of the CABIN ZONES PROGRAMMING the user can easilymodify the length of the cabin zones.

These modifications are stored in the CAM.

The maximum number of zones is 5.

Only the zone ends are programmable (except the last seat row which isfixed).

A zone can not be deleted. The smallest zone could consist of 1seatrow.

When all changes have been performed on the PIM, the new datas aresaved by pressing the “ SAVING “and SAVING CONFIRMATION”

softkey. The modified layout is saved in the respective CAM memory.If an increase (“ + “) or decrease (“ — “) at the end of a zone is notpossible the respective symbol (“ < —“ or” > + “) disappears and thesoftkey looses in function.

Note: The NO SMOKING ZONE handling is identical to the CABINZONES PROGRAMMING with the exception that a NO SMOKINGZONE can be deleted.

1.2/P15



01 Aug 06


55/202

CABIN TEMPERATURE

Normal mode (NO AUTOMATIC MODE)

On pressing the “CABIN TEMP” hardkey, the CABIN TEMPERATUREpage is displayed.

The page consists of three temperature bar graphs for temperaturepreselection. On both ends of the upper bar graph, the limits of thecontrol range are displayed (18-30 degrees).

On the right hand side, the actual target temperature is indicated (FWD,MID, AFT).

Cabin temperature control

On pressing the “+“ or “—“ key, the preselected value changes. Thetemperature correction is limited to plus or minus 2.5°C (4°5F).

If the upper or lower limit is reached, the ± symbol disappears.

If the” COCKPIT SELECTED TEMP “softkey is pressed all preselected

temperatures switch back to the cockpit selected temperatures.

1.2/P16



01 Aug 06


56/202

SYSTEM FAILURE MESSAGES

The possible failure messages in the “CIDS INTERNAL” page could be

CHECK PA/I NTPH/SIGNS/PAX CALL/LIGHTS

CHECK PA/SIGNS/PAX CALL/LIGHTS

CHECK PA/INTPH/PAX CALL

ONLY BASIC FUNCTIONS AVAILABLE

CHECK PA/INTPH/SIGNS/PAX CALL/LIGHTS

CABIN ATTENDANT ACTION

No direct cabin attendant action, for information only!

Be aware during the rest of the flight!

On ground call maintenance !

1.2/P17



01 Aug 06


57/202

SYSTEM FAILURE MESSAGES (cont’d)

The possible messages in the “WATER ICE PROTECTION“ page couldbe:

CABIN ATTENDANT ACTION:

No direct cabin attendant action, but keep a close look on the affectedgalley or lavatory !

1.2/P18



01 Aug 06


58/202


POSSIBLE MESSAGES:


In flight:

Ignore the message

On ground:

Flush one toilet on indicated side.

(a) If no flush, check if cabin panel door and balancing lever are closed.

(b) If still no flush, lock indicated lavatories.

Note: Toilets are operative when message is no longer displayed.


59/202

1.2/P20



01 Aug 06



60/202

SYSTEM FAILURE MESSAGES (cont d)

POSSIBLE MESSAGES:


Open access door in toilet shroud, near the floor.The door can be on theleft or right side of the toilet, depending on the aircraft configuration.

Flush the toilet:

(a) permanent vacuum noise:

(i) close flush valve by manual override

(ii) lock the lavatory

(b) water constantly running into the bowl

(i) close manual water supply

(ii) lock the lavatory.

Note: The WATER shut off valve is located at the side of the wash-handbasin.

1.2/P21



01 Aug 06



61/202


POSSIBLE MESSAGES


Flush indicated lavatory. It is functional if flush cycle runs successfully.Should the flush cycle not occur, the lavatory must be locked.

1.2/P22



01 Aug 06



62/202


POSSIBLE MESSAGES:


Lock all lavatories on indicated side.


WASTE BALANCING must be performed.

1.2/P23



01 Aug 06



63/202

( )


No action required.

1.2/P24



01 Aug 06



64/202

POSSIBLE MESSAGES:

CABIN ATTENDANT ACTION

(a) If a lavatory smoke detector is inoperative, the correspondinglavatory must be permanently watched over.

(b) If a crew rest smoke detector is inoperative, the crew rest must beunoccupied and closed during the entire flight.

1.2/P25



01 Aug 06

1.2.6 Cabin Crew Handset


65/202

Each main cabin attendant station is equipped with an attendant handset(in total 8) with PA and interphone capabilities and the associated Attendant Indication Panel (AlP).

The handsets are accessible to attendants while strapped in their seats.

1.2/P26



01 Aug 06

The interphone handset has integrated keys for PA and calls.


66/202

CABIN OPERATION

Handset is hooked off.

The keyboard is located in the inner face of the handset.

By dialing “PA”, “ALL”, PA announcement is performed through the cabinas soon as PU flap is pressed.

A message “PA ALL” is displayed on the nearest AlP and the message“PA ALL IN USE” on all other AlPs.

When the announcement is finished, press RESET or hook on thehandset.

The messages disappear on the AlPs.

1.2/P27



01 Aug 06

1.2.7 Attendant Indication Panel (AIP)


67/202

1.2.7.1 General

One Attendant Indication Panel (AlP) is mounted near each AttendantStation which is equipped with an handset.

1.2/P28



01 Aug 06

AlP features include a two row alphanumeric display and two indicatorlights The upper row displays communication information such as


68/202

lights. The upper row displays communication information, such asinterphone calls and the lower row displays system information. The

indicator lights serve as attention getters. Green for communicationinformation, pink for system and emergency information.

1.2/P29



01 Aug 06

1.2.7.2 Handset operation related messages


69/202

EXAMPLE A : THE PA ALL function is initiated.

By hooking off the handset, a symbol appears and flashes at calling AIPthe system awaits a dial procedure

The “PA” push button on the handset is pressed, a second symbolflashes, the system awaits now the second dial procedure.

The “ALL” push button is pressed, the indication “PA ALL” appears on the

calling AIP. As soon as the announcement starts, the symbol ”>” is displayed on thecalling AIR On all the other AlP’s the message “PA ALL IN USE” is shownon the lower line.

1.2/P30



01 Aug 06

EXAMPLE B : ATTENDANT AT DOOR 1LH CALLS ATTENDANT ATDOOR 3.


70/202

The handset at door 1LH is hooked off.

The “INTERPHONE” push button is pressed, a second symbol flashes,the system awaits the second dial procedure.

The “3” push-button is pressed, the indication “3 ATTENDANT” appearson calling AIR On the AlP’s at doors 3LH and 3RH the message “CALL1L ATTENDANT” is displayed and the green indicator comes on.

1.2/P31



01 Aug 06

As soon as the attendant at door 3LH hooks off the handset, the symbol“>“ appears on AlP’s at door 1 LH and 3LH, which means that the


71/202

communication is established.

On the AlP at door 3RH the indication disappear.

During handset operation following messages could appear on the AIP’s:

1.2/P32



01 Aug 06

1.2.8 Area Call Panel (ACP)

The Area Call Panel consists of five individually controlled illuminated


72/202

The Area Call Panel consists of five individually controlled illuminatedcolored fields. Each color corresponds to a specific call. The fields are

used in steady and in flashing mode.

The indications are:

(a) CREW Call Pink (steady or flashing)

(b) PAX Cabin Call Blue (steady)

(c) PAX Lavatory Call Amber (steady)

(d) Lavatory smoke Amber (flashing)

(e) Evac Signalling Pink (flashing)

1.3/P1



01 Aug 06

1.3 LIGHTING

1 3 1 General


73/202

1.3.1 General

The cabin light system provides illumination to the cabin, the lavatories,the galleys and the attendant work areas.

This system is part of the Cabin Intercommunication Data System(CIDS).

1.3.1.1 Cabin area

(a) The general illumination has fluorescent tubes installed in theoverhead stowage compartments and the ceiling panels. Theyshape five lighting strips.

(b) The entrance area illumination has fluorescent tubes installed on theentrance area ceiling panels.

(c) For the night lighting, the fluorescent tubes are located in the ceilingpanels (switched on to 10 % i llumination level).

The lighting strips are divided into 3 groups:

(i) Lighting strips on the outer side of the lateral overhead stowagecompartment.

(ii) Lighting strips in the ceiling panels.

(iii) Lighting strips under the center overhead stowagecompartment.

1.3.1.2 Entrance areas

Fluorescent tubes are installed in the ceiling panels illuminate theentrance areas. Two fluorescent tubes are installed in the left hand sideand right hand side ceiling panels at each entrance.

The operation is identical to that of the cabin area lighting.

1.3.1.3 Galley Area

General galley area lighting is provided by the entrance area lighting.

1.3.2 Cabin Ligh ting Panel

The cabin lighting panel is located on the Forward Attendant Panel(FAP). It controls all illumination in the cabin.

1.3/P2



01 Aug 06


74/202

The separate switches on the lighting control panel at the Purser stationcontrol each of the lighting strips. The switches “DIM 1”, “DIM 2” and“NIGHT” control the brightness of the lighting strips in each zone and thelights in the entrance area. (100 %, 50 % and 10 %)

(a) “ENTRY” pushbutton causes the fluorescent lamps at forward,mid and aft entrance areas to come on with 100 % illuminationintensity.

Note: The lights in the forward entrance area decrease in

intensity automatically when the cockpit door is opened and theengines are running

(b) The cabin lighting is divided into a first class (FC) a businessclass (BC) and a tourist class (YC) area.

The lighting strip can be switched separately in the 3 areas.

Examples:

When “CABIN FC” pushbutton is pressed the illumination of the1st class zone comes on 100 %

When “CABIN FC”“DIM 1” pushed the illumination of the FC areacomes on to 50 %

When “CABIN BC”“DIM 2” pushed the illumination of the BC areacomes on to 10 %.

“NIGHT” for the night lighting, selected fluorescent in the ceilingpanels are switched on to 10 % illumination level.

(c) The integral light of “WDO”, “CTR” and “AISLE” pushbuttonscomes on automatically when any “CABIN” pushbutton isselected on. When pressed:

1.3/P3



01 Aug 06

(i) “WDO” : the illumination of the window areas goes off.

(ii) “CTR” the illumination of the center overhead stowage


75/202

compartment areas goes off “AISLE” : the illumination of

the aisle area goes off.

(iii) When pushed again, the illumination of the selected areacomes on to the intensity level previously selected.

1.3.3 Lavatory Lighting

The lavatory lights are installed above the door of each lavatory. Amicroswitch installed at each lavatory door, controls the illumination level.

The fluorescent lamps are on 50 % intensity, when the lavatory door isclosed and unlocked. The spot lights are switched off. The fluorescentlamps are on 100 % intensity and the spot lights come on, when thelavatory door is closed and locked.

1.3/P4



01 Aug 06

1.3.4 Cabin Crew Station Work Ligh t

Cabin attendant work lights are installed at each attendant station and


76/202

can be controlled individually by an integrated pushbutton.

1.3/P5



01 Aug 06

1.3.5 Passenger Reading Ligh ts

The passenger reading lights are high intensity lights. Each passengert l hi di li ht i di id ll


77/202

can control his reading light individually.

The control switch is installed in the seat armrest (in the PCU).

1.3/P6



01 Aug 06

1.3.6 Cabin Signs

Pictogram signs to advise the passengers of required actions, areprovided in the cabin and lavatories


78/202

provided in the cabin and lavatories.

The passenger information signs are monitored from the signs panel in thecockpit.

(a) Fasten seat belts

ON Fasten seat belt signs in cabin and return to cabin signin lavatories illuminate associated with a low chime.

AUTO The signs in the cabin and in the lavatories illuminateautomatically together with a low chime, when the slatsare extended . They extinguish after the slats areretracted.

1.3/P7



01 Aug 06

OFF When switched to OFF the signs extinguish and the lowchime sounds.

(b) No smoking


79/202

(b) No smoking

ON The no smoking signs and the EXIT signs illuminate anda low chime sounds.

AUTO The no smoking signs and EXIT signs illuminate whenthe landing gear extends and extinguish when the gearsare retracted, together with a low chime.

On ground when the aircraft is on the gears the signsremain on.

OFF Signs are switched off. Low chime sounds when

switched to off.

1.3.7 Emergency Lighting System

1.3.7.1 General

The emergency lighting system is installed to provide:

(a) illumination of the cabin and the exit areas in the event of afailure of normal lighting system

(b) illumination of exit location and exit marking signs at each

passenger/crew door and emergency exit;

(c) illumination of the marking system of the emergency path

(d) illumination of lavatories, independent of the main lavatorylighting system

(e) in addition, the escape slides have their own emergencylighting.

1.3.7.2 System Components

The emergency lighting system consists of the following:

(a) 8 EXIT lights located over each EXIT door frame

(b) 8 EXIT signs located in the exit areas ceiling

(c) 24 emergency ceiling lights over the aisles

(d) floor escape path marking system which includes EXIT markersand low intensity lights located close to each exit at floor leveland below passengers seats.

1.3/P8



01 Aug 06

Eight Emergency Power Supply Units (EPSU) energize all the EXIT lightsigns, and floor proximity light. They installed in the ceiling at each exitarea.


80/202

The escape slides are equipped with an integral lighting system. Theescape slide lights automatically illuminate when the escape slidedeploys. They have the same supply as the cabin emergency lights,from the power supply units.

1.4/P1



01 Aug 06

1.4 COMMUNICATIONS

1.4.1 General


81/202

The communication system includes:

(a) Passenger address, including boarding music and the passengerentertainment system;

(b) Interphone system;

(c) Passenger call system;

(d) Evacuation signaling including the evacuation command system.

All systems are controlled by the Cabin Intercommunication Data

System (CIDS).1.4.2 Passenger Address System (PAS)

1.4.2.1 General

The PAS allows cabin announcements to passengers throughloudspeakers. In addition, one loudspeaker is installed in each lavatoryand galley.

PAS volume increases automatically as soon as an engine is runningand in the case of a depressurization.

The PAS can be operated from the cockpit (handset or Audio ControlPanel with audio equipment) or from the cabin (handset).

The PAS is designed such that cabin crew PA announcements can bemade to the whole cabin or separately to the business class cabin oreconomy class cabin, as required.

1.4.2.2 PAS Priority Levels

PAS priority levels are in accordance with the following:

Priority Position

1st Flight deck station

2nd

Purser station

3rd

Other cabin crew stations

4th

Pre-recorded announcements

5th

Video/entertainment sound

6th

Boarding music

1.4/P2



01 Aug 06

1.4.2.3 PA Announcement from any Cabin Crew Station

To make a normal PA announcement throughout the aircraft from anycabin crew station, proceed as follows:


82/202

(1) Press PA ALL switch:

Message “PA ALL” is displayed on the nearest AIP.

Message “PA ALL IN USE” is displayed at other AIP’s.

Press PUSH TO TALK (PTT) switch and make PAannouncement.

(2) Press RESET when finished, or hang up handset.

1.4/P3



01 Aug 06

1.4.2.4 Pre-recorded Announcement and Boarding Music(PRAM)

The function of the PRAM is to play pre-recorded announcements andmusic programs. These are transmitted to the passengers, through the


83/202

passenger address system which is a part of the CabinIntercommunication Data System (CIDS).

The announcements are also transmitted to the passengers through theheadsets from the Passenger Entertainment System (PES).

The PRAM reproducer is installed in the avionics compartment. It canstore up to 256 pre-recorded announcements. In addition, four differentboarding music programs are selectable.

These functions are controlled from the Programming and Indication

Module (PIM) in the Forward Attendant Panel (FAP).When the announcement system operates, a “PA IN USE” message isshown at all Attendant Indication Panels.The PRAM transmits manuallyselected announcements, automatic announcements (FASTEN SEATBELT and NO SMOKING) and an emergency announcement when arapid cabin decompression occurs.

(a) Pre-recorded Announcement

The announcement control equipment is as follows:

(i) a PRE ANN pushbutton switch to set the pre-recordedannouncement mode.

(ii) a numerical keypad (0 to 9), to set the announcementnumbers.

(iii) a CLEAR pushbutton, to cancel all stored announcements inthe memory.

(iv) an ENTER pushbutton, to set the selected announcement inthe next free memory.

(v) a LCD (Liquid Cristal Display) monitor, with 12 soft keys, 6on the left, 6 on the right.

The soft keys can have these functions:

(i) START ALL : starts all stored announcements in thememory.

(ii) START NEXT : starts the next announcement in thememory.

(iii) STOP : stops the transmission of announcements.

1.4/P4



01 Aug 06

(iv) MEMO 1 to MEMO 5 : to set the selected announcementnumber in the related memory.


84/202

By pressing the “PRE ANN” hardkey, the PRERECORDED ANNOUNCEMENT page is displayed.

1.4/P5



01 Aug 06


85/202

The numerical keyboard is used to set coded messages.

(i) Each keyboard entry must be closed with ENTER or bypressing any MEMO field softkey.

(ii) Corrections on the selected MEMO field can be performedby pressing CLEAR on the keyboard or by overwriting therespective MEMO field.

(iii) The system will accept a number range between 0 t0 256.Numbers out of this range will lead to an ERROR messageat the respective MEMO field.

(iv) An annoucement which cannot be found by the PRAM, willbe indicated by a MISSING message (only for MEMO 1 andMEMO 2 announcements).

(v) By pressing the STOP softkey all messages can be stopped.ON ANNOUNCE field will be cleared.

1.4/P6



01 Aug 06


86/202

To start the playback of the announcement “START ALL” or “STARTNEXT” must be pressed.

If a message is found and on announcement, the display will scroll theMEMO fields. Additional message(s) can be entered in the field with thearrow.

If the announcements are started via START ALL, it is possible to selectSTART NEXT, which leads to a change in the announcement mode. Thatmeans, only the next message will be announced then.

If the announcements are started via START NEXT, it is possible to selectSTART ALL, which leads to a change in the announcement mode. Thatmeans, all the messages will be announced then.

The initial page is displayed again after playback of the lastannouncement.

(b) Boarding music

A row of ten LEDs, to indicate thevolume level

An ON/OFF pusbutton switch

A digit display, to indicate themusic channel

A SEL pushbutton, to set the musicchannel

A (+) pushbutton, to increase thevolume level

A (-) pushbutton, to decrease the volume level.

1.4/P7



01 Aug 06

1.4.3 Cabin Interphone System

The cabin interphone system provides two way communication andalerting facilities between the cabin crew and cabin crew and between

bi d fli ht d k


87/202

cabin crew and flight deck crew.

1.4.3.1 Normal Call from One Cabin Crew Station to another Cabin Crew Station

To make a normal call from one cabin crew station to another cabin crewstation, proceed as follows (Example: Purser calls aft attendant station):

(1) Press INTPH switch;

(2) Press 4 on keyboard

AIP at forward left attendant handset displays all dial and systeminformation, after dialing: “4 ATTND”

ACP at aft attnd stations L/R steady PINK. Hi-Lo chime via aft attndstation loudspeakers.

On AIPs at aft attnd stations steady text: “CALL 1L ATTND” and steadyGREEN indicator.

When finished, hang up handset.

1.4/P8



01 Aug 06

1.4.3.2 One Cabin Crew Station calls all Cabin Crew Stations

To make a normal call from one cabin crew station to all other cabincrew stations, proceed as follows:


88/202

(1) Press INTPH switch;

(2) Press ALL switch;

AIP at forward left attendant handset displays all dial and system

information, after dialing: “ALL ATTND”

ACP at all attnd stations steady PINK.

Hi-Lo chime via all attendant station loudspeakers.

On AIPs at all attendant stations steady text: “CALL ALL ATTND” andsteady GREEN indicator.


1.4/P9



01 Aug 06

1.4.3.3 Emergency Call from the Cabin Crew Station to Flight Deck

To make a call from a cabin crew station to the flight deck, proceed asfollows:


89/202

(1) Press PRIOR CAPT switch;

AIP at attendant handset displays all dial and system information, after

dialing: “PRIOR CAPT”

CALL panel in cockpit: Legend flashing on EMER pushbutton switch

AUDIO CONTROL PANEL in cockpit: flashing light on call indicator.

Crew call buzzer is activated 3 x 1 sec.


1.4/P10



01 Aug 06

1.4.4 Passenger Call System

A call system provides the possibility to passengers to call the cabincrew from:

(a) passenger seats


90/202

(a) passenger seats

(b) lavatories

1.4.4.1 Call from a passenger seat

Pressing the cabin attendant call button on the Passenger Service Unit(PSU) results in:

To RESET the call lights, the cabin attendant call button on the PSUmust be pushed again.

Note: In case of a passenger call during boarding when all the seat rownumbering lights are illuminated in steady mode, the respective seat rownumbering light will flash. As soon as all doors are closed seat rownumbering lights are off and will illuminate in steady mode whenactivated.

1.4/P11



01 Aug 06

1.4.4.2 Call from lavatory

Pressing the cabin attendant call button on the Lavatory Service Unit(LSU) results in:


91/202

To Reset the call, the call button must be pushed again.

1.4/P12



01 Aug 06

1.4.5 Evacuation Signalli ng System

An emergency evacuation signalling system (integrated in the CIDS) isinstalled. It provides visual and aural alert in the event of impending

emergency evacuation of the aircraft.


92/202

g yLocation: Panels provided with warning lights are installed

(a) One in the cockpit

(b) One at the purser station (1)

(c) One at the attendant station door 2 (opt) (2)

(d) One at the aft attendant station (3)

(1): At Purser station

1.4/P13



01 Aug 06

(2) and (3): at CA 2L and 4L


93/202

Description:

(a) Forward Attendant Panel

(1) “EVAC CMD”

Located only at the purser station and is used to activate the system.

(2) “EVAC/RESET”

Button flashes red when the system is activated. When the pushbutton ispressed the audio warning at this respective station is silenced.


94/202

1.5/P1



01 Aug 06

1.5 LAVATORIES

1.5.1 General

The lavatories are installed in the cabin for comfort of passengers andcrew. Each lavatory has a washroom function. Cold, hot and waste water


95/202

connections, air outlet connections and fans are provided.

The lavatories can be installed in various of configurations to satisfycustomer request:

(a) forward lavatories (La-Lc) (L11-L12)

(b) mid lavatories (Lk-Lh) (L34-L33)

(c) aft lavatories (Lu-Lv, Ly, Lz) (L73-L81 - L74-L82)

1.5/P2



01 Aug 06

1.5.2 System Components

1.5.2.1 Toilet manual shut off

A manual shut off valve in each lavatory permits to shut off the water

supply for the faucet and toilet. It is located at floor level behind anaccess door next to the toilet bowl on the side towards the faucet


96/202

access door, next to the toilet bowl, on the side towards the faucet.

A shut off lever, located below the toilet bowl on the left or right handside, permits to close the flush valve manually.

1.5/P3



01 Aug 06

1.5.2.2 Rinse Valve Failure

To avoid toilet overflow in case of a rinse valve failure, a warning signalis transmitted to the CIDS.

A triple LO chime sounds throughout the cabin attendant loudspeakers,and the ACP amber light flashes at the relevant attendant stations zone


97/202

and the ACP amber light flashes at the relevant attendant stations zonewise.

On the AlP the affected lavatory is shown in clear wording and the redindicator light comes on.

The amber call light is flashing at the relevant lavatory.

Audio warning and visual indications can be cancelled by pressing theCIDS caution light pushbutton (1) on the PIM. The PIM message willdisappear if the relevant manual override valve is closed.


98/202

1.5/P5



01 Aug 06

1.5.2.4 Waste System

The toilet waste quantity can be checked by pressing the waste key onthe Programming and Indication Module (PIM).


99/202

If the waste service panel is open, the waste page is automaticallydisplayed and the indication “WASTE SVCE DOOR OPEN” appears onthe screen.

Vacuum lavatories system failure messages:

If a vacuum lavatories system failure is detected by the CIDS, thesystem check page will be automatically displayed on the PIM.

1.5/P6



01 Aug 06

The softkey corresponding to the vacuum lavatories must be pressed.

On the lavatory system check page different messages could appear.

The following short indicates these messages and their required cabin

attendant action.


100/202

1.5/P7



01 Aug 06

1.5.3 Controls

1.5.3.1 Lavatory Service Unit


101/202

(1) Return to seat sign

(2) Cabin Attendant call button

(3) Plug

The return to seat sign comes on when the FASTEN SEAT BELTS signsare switched on.

The Cabin Attendant call button pressed operates the pax call soundand lights in the cabin.

1.5.4 Lavatory Fire Protection System

1.5.4.1 Smoke Detector

One smoke detector is installed in each lavatory extraction duct.

If smoke enters into the measuring chamber of the detector, a warningsignal is transmitted to the CIDS.

On all the AlPs the affected lavatory is shown in clear wording and thered indicator light flashes.

A triple chime is broadcast via all Loudspeakers.

The amber light of the respective ACP and the outside smoke indicatorof the affected lavatory are flashing.

The corresponding LAV SMOKE button on the FAP or the AAPilluminates.

1.5/P8



01 Aug 06

The RESET operations from attendant panels also affect the indicationsin the respective area except for the chime distribution which is resetentirely.


102/202

1.5/P9



01 Aug 06

1.5.4.2 Extinguisher

A small extinguisher bottle which contains 120 g of halon and freon isinstalled in each waste bin.

The lavatory fire extinguishing system is completely automatic and self-contained.


103/202

A fire or overheat condition opens the release mechanism.

A temperature increase from approx 71°C to 140°C (300°F) operates thelavatory fire extinguisher, within 60 s.

1.5/P10



01 Aug 06

1.5.5 Lavatory Door Emergency Unlocking Mechanism

It is possible to unlock the doors from the passenger compartment sidein the event of emergency without using a special tool.

For this, lift the LAVATORY cover plate above the VACANT/OCCUPIEDindicator and push the unlocking pin from right to left.


104/202

1.6/P1



01 Aug 06

1.6 GALLEYS

1.6.1 Galley System Overview

1.6.1.1 General

Individual galley modules may contain ovens, waste containers, coffeemakers, refrigeration units, storage/servicing carts, sinks and stowage


105/202

g g g gspace to aid in food preparation and dispensing. Galleys are equippedwith electrical power and water systems. Lighting controls are located onthe galley electric panel. A galley vent system keeps the air fresh.

Service carts are restrained for takeoff and landing. There are stowageareas for extra carts located at various galleys. The number of food cartsshall not exceed the number of in-flight cart restraints available.

1.6.1.2 Galley Locations

Galleys are installed at the front and the rear of the aircraft.

1.6.1.3 Galley Electrical Power

Electrical power is supplied through a control panel in each galley. Ifpower is unavailable to one or more galleys the flight deck should benotified.

1.6.1.4 Galley Water System

Each galley that has running water is equipped with a water shutoffvalve. Positioning the water shutoff valve to the OFF position turns offwater to that galley.

Potable water contents are available on the water and waste module onthe FAP, as follows:

1.6/P2



01 Aug 06


106/202

(1) IND ON pressed and held:

Water and waste quantities are indicated in percentage of total

tanks capacities.Released:

The indications of water and waste quantities are darkened.

1.6.1.5 Galley Waste System

Galley sink waste water is drained overboard through heated drainmasts.

To prevent sink drain blockages cabin crew should not put solid waste(coffee grounds, tea bags, fruit pulp, and so on) in the sink drain. Putsolid waste in the galley waste bins. Mixtures, which can curdle andcreate a drain blockage, should be diluted with an equal amount ofwater.

The sink drain strainer should not be removed.

1.6.2 Galley Non-Normal Operations

1.6.2.1 Galley Sink Drain Blockages

If a sink drain is blocked, or drainage is slow, no more fluids should be

poured into the sink. Dispose of fluids in another galley sink.

1.7/P1



01 Aug 06

1.7 DOORS, SLIDES AND EMERGENCY EXITS

1.7.1 Introduction

The aircraft is equipped with six type “A” doors and two type “I”

emergency exits except A330 (VN-A368) with eight type “A” doors.

They have an inward initial opening movement and then open upwardsd f d Th b it i f


107/202

and forwards. They become emergency exits in case of emergencyevacuation and are all provided with an emergency evacuation facilitystowed in a container hinged on the lower part of the door.

1.7/P2



01 Aug 06


108/202

1.7/P3



01 Aug 06


109/202

1.7/P4



01 Aug 06

1.7.2 Warning System

Each door has an observation window equipped with a sunshade. Closeto that window, there are two electrical lights.

(a) One indicator light which illuminates white when the slide is armedand the door handle moved up.

(b) One warning light which flashes red in case of cabin differential


110/202

( ) g gpressure above 2.5 MBAR (0.0362 PSI) when all engines are shutdown and the arming system is disarmed.

The lights are visible also from outside.

1.7/P5



01 Aug 06

1.7.3 Operations of Doors from inside

1.7.3.1 Type “A” Door Operations

Opening:

(a) The slide arming lever must be in DISARMED position and theSAFETY PIN installed.

(b) If the RED CABIN PRESSURE warning light close to the


111/202

(b) If the RED CABIN PRESSURE warning light close to theOBSERVER WINDOW flashes, DO NOT OPEN THE DOOR andREPORT TO the COCKPIT CREW.

(c) Grasp one ASSIST HANDLE “A”

(d) Lift the door control handle fully up.

(e) (The two upper latches disengage and door unlocks)(f) Push the door outwards then move it forwards, by using the ASSIST

HANDLE “B”, until it locks in its fully open position.

(An integrated damper limits the speed of the door).

1.7/P6



01 Aug 06

Closing: To unlock a door from its fully open position:

(a) Press the GUST LOCK located on the support arm of the door

(b) Grasp the ASSIST HANDLE “A”

(c) Using the ASSIST HANDLE “B”, move the door rearwards

(d) When the door is in front of its frame, pull the door in and lower thedoor control handle


112/202

door control handle

(e) Check that the door locks correctly, the door locking indicators,located on the upper part of the door indicate locked.

1.7/P7



01 Aug 06

1.7.3.2 Type “I” Door Operations

Opening: Type “I” door opens the same way as the type “A” door.

(a) The slide arming lever must be in DISARMED position and the

SAFETY PIN installed.(b) If the RED CABIN PRESSURE warning light close to the

OBSERVER WINDOW flashes, DO NOT OPEN THE DOOR andREPORT TO the COCKPIT CREW


113/202

REPORT TO the COCKPIT CREW.

(c) Grasp one ASSIST HANDLE “A”.

(d) Remove plastic cover over control handle.

(e) Lift the control handle fully up.

(f) Push the door outwards, then move it forwards, by using the ASSIST HANDLE “B”, until it locks in its fully open position.

1.7/P8



01 Aug 06

Closing: Closing is the same as type “A” door.

To unlock a door from its fully open position.

(a) Press the GUST LOCK located on the support arm of the door

(b) Grasp the ASSIST HANDLE “A”

(c) Using the ASSIST HANDLE “B”, move the door rearwards

(d) When the door is in front of its frame pull the door in and lower the


114/202

(d) When the door is in front of its frame, pull the door in and lower thedoor control handle

(e) Check that the door locks correctly, the door locking indicator, onthe upper part of the door must indicate locked.

1.7.4 Operations of Doors from Outside

1.7.4.1 Opening

Labels next to the exterior control handle indicate how to open the doorfrom the outside.

(a) CHECK through the observation window that the RED CABINPRESSURE INDICATOR DOES NOT FLASH

(b) PUSH the flap and grasp the handle, lift it fully up (to the horizontalgreen line)

(c) PULL the door outwards and forwards until it locks in the fully openposition.

1.7/P9



01 Aug 06


115/202

1.7.4.2 Closing

PUSH the gust lock to unlock the door, move the door towards theframe, push it in and lower the control handle. The door is locked whenthe handle is flush with the fuselage.

1.7/P10



01 Aug 06

1.7.5 Slide Arming System

1.7.5.1 “DISARMED” position

When the ARMING LEVER is in the DISARMED position a safety pin

with a red flag must be installed to• Indicate that the door is in the DISARMED mode

• Prevent inadvertent movement of the arming lever.


116/202

(1) Type “A” door:

1.7/P11



01 Aug 06

a. Type “I” door:


117/202

1.7/P12



01 Aug 06

1.7.5.2 ARMING procedure:

In order to arm the door:

(a) the safety pin has to be removed and stowed in the hole provided

for that purpose, on the support arm for the type A door, on thebutton of the door frame for the type I door.

(b) then the arming lever must be moved to the ARMED position

THE DOOR IS NOW READY FOR FLIGHT


118/202

THE DOOR IS NOW READY FOR FLIGHT

(1) Type “A” door

(2) Type “I” door

When the arming lever is in the ARMED position a flap moves under thedisarmed hole which avoids reinstalling of the safety pin.

1.7/P13



01 Aug 06

Note: If the SLIDE ARMING lever is in the “ARMED” position and thedoor is opened from the outside the lever will move automatically andmechanically to the “DISARMED” position

1.7.6 Emergency Opening

1.7.6.1 Type “A” Doors:

(a) Check that the evacuation system is armed

(b) Hold on to the frame assist handle


119/202


(c) Lift door control handle rapidly fully up and release

The door opens automatically and locks in the open position.

Should the pneumatic assistance of the door fail, PUSH door openMANUALLY

1.7/P14



01 Aug 06

1.7.6.2 Type “I” Doors

(a) Check that the evacuation system is armed


(c) Uncover control handle

Lift door control handle rapidly fully up and release The door opensautomatically and locks in the open position.

Sh ld th ti i t f th d f il PUSH d


120/202

Should the pneumatic assistance of the door fail, PUSH door openMANUALLY

1.7/P15



01 Aug 06

1.7.7 Evacuation Slides - General

A slide raft is installed in each passenger/crew door (type A door).

For doors 1 and 4 these slide rafts deploy straight down. For doors 2L and

2R the slide raft is canted in order to deploy in acceptable clearance awayof the engines.

An escape slide is installed in each emergency exit (type I door).

They permit quick evacuation for the passengers and the crew in an


121/202

y gemergency.

1.7/P16



01 Aug 06

1.7.8 Slide/Raft

1.7.8.1 Type “A” doors

They are of the DUAL-LANE type and have two functions:

(a) as an escape slide

(b) as an inflatable raft.

Normal Operation


122/202

The deployment and inflation of the unit is automatically initiated when thedoor is opened in “armed” mode. As the door opens, the girt tensions andpulls the packboard off the door. It falls below the door sill, the speedlacing releases and the unit falls from the packboard. A firing lanyardactuates the regulator valve, primary gas is supplied to the aspirators and

the inflation is initiated.

1.7/P17



01 Aug 06

Manual Inflation

If the automatic inflation is not initiated, the red manual inflation handle,located on the girt extension of the SLIDE-RAFT, has to be pulled.

This handle is always located at the right hand side of the girt extension.


123/202

1.7/P18



01 Aug 06

Restraint Devices

An intermediate tie device restrains the SLIDE/RAFT to approximativelyone third of its extended length, to prevent slide-raft from inflatingunderneath the fuselage.

When the SLIDE/RAFT becomes sufficiently pressurized, the intermediatetie releases and the slide-raft is projected outwards and downwards tocontact the ground.

The slide rafts inflate and deploy within 4 seconds.


124/202

The inflation reservoir sensors are connected to the CIDS and thepressure of the inflation cylinder is indicated on the PIM.

1.7/P19



01 Aug 06

Slide/Raft Features


125/202

1.7/P20



01 Aug 06


126/202

1.7/P21



01 Aug 06

1.7.8.2 Type “I” door

The escape slides are of SINGLE LANE type and are installed on the leftand right emergency exit door in the cabin.


127/202

Normal Operation

The slide inflation is automatic if you open the emergency exit door andthe emergency control handle is in the ARMED position.

During the door opening, the escape slide drops down and the automaticinflation is initiated. The slide can also be inflated manually after the door

is opened by pulling the manual inflation handle. To avoid wind effect tillthe slide is fully inflated, a restraint device keeps it folded as long as theinflation is not sufficient to break it.

It takes about 6 seconds for the escape-slide to be ready for evacuation.

1.7/P22



01 Aug 06

Manual Inflation

If the slide automatic inflation does not occur, pull the manual inflationhandle which is located on the right hand side of the slide.


128/202

1.7/P23



01 Aug 06

Slide/Raft Features

8/20/2019 A330 Cabin Crew Procedur

Documents

A330 Cabin Crew Procedure Manual