ATA 44 Cabin Systems.pdf

A380 TECHNICAL TRAINING MANUAL MANUAL RAMP & SERVICING COURSE - M02 (RR Trent 900) ATA 44 Cabin Systems Syste ms

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A380 TECHNICAL TRAINING MANUAL

ATA 44 CABIN SYSTEMS Cabin Systems Introduction (1) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 Cabin Intercommunication Data System Presentation (1) . . . . . . . . . . 4 In-Flight Entertainment System Presentation (1) . . . . . . . . . . . . . . . . 12 Cabin Monitoring System Presentation (1) . . . . . . . . . . . . . . . . . . . . 20

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RAMP & SERVICING COURSE - M02 (RR Trent 900) ATA 44 Cabin Systems

TABLE OF CONTENTS

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CABIN SYSTEMS INTRODUCTION (1) General The Cabin systems are composed of: - the Cabin Intercommunication Data System (CIDS) - the In Flight Entertainment System (IFE), - and the Cabin Monitoring System.

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CABIN SYSTEMS INTRODUCTION (1)

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CABIN SYSTEMS INTRODUCTION (1)

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CABIN INTERCOMMUNICATION DATA SYSTEM PRESENTATION (1) General The CIDS (Cabin Intercommunication Data System) is the cabin core system. It fulfills an easy interface with some aircraft and cabin support systems for the cabin crew, the passengers, the maintenance personnel and the cockpit crew. The CIDS lets them accomplish the functional control, the testing and the monitoring of these systems through the following four functions: - Communication, - Indicating, - Control, - Others.

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CABIN IN TERCOMMUNI CATION DATA SYSTEM PRESENTATION (1)

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CABIN INTERCOMMUNICATION DATA SYSTEM PRESENTATION (1) System Architecture The main components of the Cabin Intercommunication Data System (CIDS) are: - three directors, - Decoder/Encoder Units (DEUs) type A dedicated to passenger related functions, - DEUs type B dedicated to cabin support sys tems and cabin crew related functions, - Flight Attendant Panels (FAPs), mini-FAPs, Attendant Indication Panels (AIPs), Area Call Panels (ACPs), Additional Attendant Panels (AAPs) for controls and indicating, - communication devices like handsets and loudspeakers.

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CABIN INTERCOMMUNICATION DATA SYSTEM PRESENTATION (1) Crew Signalling And Alerting

Communication Functions The CIDS has several communication functions, which are: - Passenger Address - Cabin interphone - Service interphone - Crew signalling and alerting

PA The Passenger Address (PA) is one of t he main functions of the CIDS. It supplies one way voice communication to do announcements from the cockpit or from a cabin crew station to the passengers. These announcements are initiated from the cockpit using either a handset or acoustic devices and from the cabin using cabin crew stations handsets. They are then broadcasted to the passengers either through passengers headsets via In Flight entertainment (IFE) and throug h all cabin loudspeakers. A PA announcement can be direct or prerecorded voice information and it can also be used to supply prerecorded music.

There are different kinds of cockpit and cabin crew signaling and alerting functions depending on the situation. The "area ready" function lets the cabin crew inform the purser that a dedicated cabin area is ready for takeoff/landing. This function is activated thanks to the FAPs and the optional MINI-FAPs. The "cabin ready" signaling function lets the purser inform the cockpit crew that all the cabin areas are ready for takeoff/landing. This function is activated thanks to the FAPs. The optional "sterile cockpit" lets the cockpit crew inform the purser that they do not want to be disturbed. This function is activated by the cockpit crew through a sterile cockpit P/B. The optional Emergency Crew Alerting System (ECAS) is used to indicate an unusual behaviour in cabin or cockpit. This function is activated from the cabin thanks to a cabin alert P/B and from the cockpit via a cockpit alert P/B.

Cabin Interphone

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The cabin interphone system is used for communication between all cabin crew stations or between the cockpit and the cabin crew stations. From the cockpit the communication is established via the cockpit handset or via acoustic device. From the cabin the communication is established via any cabin crew station handset.

Service Interphone M

The service interphone system is used, on ground only, for communications between the service interphone jacks o r between the service interphone jacks, the cockpit and the cabin crew stations. The service interphone jacks are located within the major service areas. 1

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COMMUNICATION FUNCTIONS - PA ... CREW SIGNALLING AND ALERTING A

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CABIN INTERCOMMUNICATION DATA SYSTEM PRESENTATION (1) Indicating Functions The CIDS fulfills several indicating functions like : - Smoke Detection Function (SDF), - Emergency lighting power supply , - Ice protection and control (e.g. freezing of potable water system) - Trolley lift, - Electrical load management, - Galley cooling, - IFE and seat power, - Doors/slides status, - Vacuum System Control Function (VSCF) (e.g.: potable water/waste tank filling level)

Control Functions

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The CIDS fulfills several control functions related to: - Cabin lighting and passenger reading lights, - EVAC, - Lighted signs (e.g.: FSB, NS signs) - PAX call, - IFE, - Air conditioning (e.g.: cabin zones temperature adjustment), - VSCF (e.g.: auto flush, water depressurisation of water system) - Optional Electrical Window Shade (EWS). P

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The CIDS fulfills several other functions related to: - Software loading - Layout selection - Cabin programming - Loudspeakers level adjustment - Fap Set-Up RAMP & SERVICING COURSE - M02 (RR Trent 900) ATA 44 Cabin Systems


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IN-FLIGHT ENTERTAINMENT SYSTEM PRESENTATION (1) General The In-Flight Entertainment (IFE) system is an optional system, installed within the cabin on customer request. The IFE system gives mainly to the passenger entertainment supported by the audio, the optional video, the optional interactive functions ('such as games, shopping, and internet) and the optional telephone. These functions are controlled by the cabin crew, the passengers, and/or aut omatically according to A/C system d ata. The PAX service system lets the p assengers control from their seat so me functions of other A/C systems such as CIDS PAX call or PAX reading lights.

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IN-FLIGHT ENTERTAINMENT SYSTEM PRESENTATION (1)

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IN-FLIGHT ENTERTAINMENT SYSTEM PRESENTATION (1) Note: The Human Machine Interface (HMI) of a control console is made of a touch screen.

System Architecture Overview The IFE system architecture is based on a modul ar concept, which gives a platform for various entertainment systems from different vendors in an add-on principle. It offers flexibility and adaptability for customized configuration. This system is basically composed of three main parts: the IFE Center (IFEC), an IFE control panel and a cabin network.

IFEC The IFEC is located in the u pper avionic bay. It is made of one or two racks (IFEC rack 2 is optional) which contains the IFE system head end equipment. It is composed of computers, video/audio sources, files servers and third party equipment. The IFEC manages the whole IFE system and is the interface with the cabin network, the A/C systems, the CIDS, and the optional cabin workstation.

IFE control panel, cabin workstation and RCC

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The IFE control panel supplies a centralized control and monitoring of the whole IFE system for the cabin attendants. It is an application, which may run either as one of the FAP application or hosted in an optional and specific device called cont rol console. Note that th e FAP may be located within an optional cabin workstatio n while the control console is located either within the optional cabin workstation or within an optional Remote Control Center (RCC). The IFE control panel controls other optional equipment such as additional audio/vid eo sources (except in RCC), fax unit, data loader, credit card reader, etc... The cabin workstation when install ed is the main working area of the purser and offers the centralized operation for IFE, CIDS, cabin logbook, email, PAX profile and electronic documentation. In addition to or instead of the cabin workstation, the RCC when installed offers an additional limited IFE control through an other control console.

Cabin Network The cabin network supplies audio, video, data, telephone and up loadable software to the passenger seats equipment. It supplies also video data to the overhead or wall mounted video equipment. It comprises: - The cabin distribution network, which is composed of Area Distribution Boxes (ADBs) (a maximum of 12 can be installed). They facilitate the distribution of the cabin network data to and from the passengers seats via the seat network and to the overhead video equipment via the overhead network. Moreover the ADBs give the connection of RCC to the cabin distribution enabling the cabin staff to control the IFE system from locations other than the cabin workstation : - The overhead network, which is composed of Tapping Units (TUs). Each one is able to supply video and power to 3 overheads or wall mounted DUs - The seat network, which is composed of Floor Disconnect Boxes (FDBs) and Seat Electronic Boxes (SEBs). It exchanges data between the cabin distribution network and the seat equipment.

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SYSTEM ARCHITECTURE OVERVIEW - IFEC ... CABIN NETWORK A

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IN-FLIGHT ENTERTAINMENT SYSTEM PRESENTATION (1) Pax Service System In baseline configuration the PAX service system functions give reading light and attendant call control to the passengers. Each Passenger Service Unit (PSU) reading light and attendant call light is controlled from the related PCU. This control is done via the cabin network, the IFEC and the CIDS.

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IN-FLIGHT ENTERTAINMENT SYSTEM PRESENTATION (1) Telephone (Optional) In seat telephone The In-Seat Telephone function supplies the cabin internal seat-to-seat communication, and air to ground communication (voice and data). The telephone handset is integrated in the passenger seat but it can also be integrated in the optional crew rest compartments. The telephone handset is connected to the IFEC via the seat and cabin distribution networks. The air to ground communication is then established via the telephone function in the IFEC and via the SATCOM system. As an airline option, the seats may be equipped with a credit card reader (e.g.: payment of telephone communications).

Wall mounted telephone The wall mounted telephone function supplies telephone communication for wall-mounted telephones and fax. The telephone or fax station are connected to the IFEC via a seat network and the cabin distribution network. The air to ground communication is then established via the telephone function and via the SATCOM system.

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CABIN MONITORING SYSTEM PRESENTATION (1) General The cabin monitoring system is composed of the optional Cockpit Door Surveillance System (CDSS) and of the optional Cabin Video Monitoring System (CVMS). The CDSS is designed to help the cockpit crew to identify a person requesting entrance to the cockpit and to survey the doors 1 hidden cross section via video camera observation. The CVMS is mainly designed to help the cabin and cockpit crew in video surveillance of the whole cabin (main and upper deck) and of some other areas like the staircases, the crew rest areas and the lower deck facilities. The CVMS is installed to detect unruly passeng ers, suspicious behaviors or other potential threats occurring in these areas.

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AIRBUS S.A.S. 31707 BLAGNAC cedex, FRANCE STM REFERENCE LAY08521 JANUARY 2009 PRINTED IN FRANCE AIRBUS S.A.S. 2009 ALL RIGHTS RESERVED AN EADS COMPANY

ATA 44 Cabin Systems.pdf

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