AIRBUS M35 INDICATING RECORDING SYSTEMS SINGLE AISLE TECHNICAL TRAINING MANUAL MAINTENANCE COURSE M35 LINE MECHANICS (V2500A5.ME)

 SINGLE AISLE   TECHNICAL TRAINING MANUAL   MAINTENANCE COURSE - M35 LINE MECHANICS (V2500-A5/ME)   INDICATING/RECORDING SYSTEMS  This document must be used for training purposes only Under no circumstances should this document be used as a reference It will not be updated All rights reserved No part of this manual may be reproduced in any form, by photostat, microfilm, retrieval system, or any other means, without the prior written permission of AIRBUS S.A.S SINGLE AISLE TECHNICAL TRAINING MANUAL INDICATING/RECORDING SYSTEMS ELECTRONIC INSTRUMENT SYSTEM (EIS) (Classic) UP & DOWN DATA LOADING SYSTEM EIS Architecture (1)  2 Engine/Warning Display Presentation (1)  4 ECAM Advisory & Failure Related Modes (3)  12 ECAM Warnings Presentation (1)  20 EIS Abnormal Operation (3)  28 EIS Warnings (3)  50 Up & Down Data Loading System Presentation (1)  180 Up & Down Data Loading System Utilization (2)  184 ELECTRONIC INSTRUMENT SYSTEM (EIS) (Enhanced) AIRCRAFT INTEGRATED DATA SYSTEM (AIDS-SFIM) EIS Architecture (1)  52 Engine/Warning Display Presentation (1)  54 ECAM Advisory & Failure Related Modes (3)  62 ECAM Warnings Presentation (1)  70 EIS Abnormal Operation (3)  78 EIS Warnings (3)  110 Print Report STD Header Description (3)  194 Individual Print Report Description (3)  200 DIGITAL FLIGHT DATA RECORDING SYSTEM (DFDRS) DFDRS Description/Operation (3)  188 DFDRS Warnings (3)  192 A/C INTEGRATED DATA SYS (AIDS-TELEDYNE) (option) CLOCK Print Report STD Header Description (3)  228 Individual Print Report Description (3)  234 Electrical Clock D/O (2)  112 MAINTENANCE PRACTICE CENTRALIZED FAULT DISPLAY SYSTEM (CFDS) Computer Removal and Installation (3)  264 Pushbutton Removal and Installation (3)  266 U3U06191 - U0O35M0 CFDS Fault Processing (3)  118 CFDS Aircraft System Types (1)  124 CFDS Failure Classification (1)  126 CFDS Reports (1)  134 CFDS Phases (2)  160 Trouble Shooting Procedure with CFDS (3)  162 PRINTER Printer Presentation (1)  172 Printer Paper Loading (2)  174 MAINTENANCE COURSE - M35 LINE MECHANICS (V2500-A5/ME)  31 - INDICATING/RECORDING SYSTEMS TABLE OF CONTENTS May 11, 2006 Page SINGLE AISLE TECHNICAL TRAINING MANUAL EIS ARCHITECTURE (1) EFIS-ECAM The Electronic Instrument System (EIS) is shown on identical Cathode Ray Tubes (CRTs) The Electronic Flight Instrument System (EFIS) are displayed on identical Display Units (DUs) and controlled through the EFIS control panels and the lighting/loudspeaker control panels The Electronic Centralized Aircraft Monitoring (ECAM) pages are displayed on identical DUs and controlled through the ECAM Control Panel (ECP) and which are not related to warning, are directly sent to the DMCs The inputs received by the SDACs are used to elaborate amber warnings These signals will then be sent to the FWC to generate warnings DMC The Display Management Computers (DMCs) process data in order to generate codes and graphic instructions related to the image to display Note the particular role of DMC is to be switched instead of DMC or DMC Each DMC can process three displays: Primary Flight Display (PFD), Navigation Display (ND) and upper or lower ECAM display FWC U3U06191 - U0O35M0 - UM31P2000000002 The Flight Warning Computers (FWCs) monitor the aircraft systems These computers are the heart of the ECAM system Each FWC generates all warning messages to display and supplies the attention getters It also computes the flight phases and supplies aural warnings SDAC The System Data Acquisition Concentrators (SDACs) receive various signals from the aircraft systems and send them to the FWCs and DMCs The SDACs acquire most of the signals used to display system pages and used by the FWCs to generate amber warnings INPUTS The inputs received by the FWC are used to elaborate red warnings Various items of information for systems like engines, fuel, navigation MAINTENANCE COURSE - M35 LINE MECHANICS (V2500-A5/ME)  31 - INDICATING/RECORDING SYSTEMS EIS ARCHITECTURE (1) May 10, 2006 Page U3U06191 - U0O35M0 - UM31P2000000002 SINGLE AISLE TECHNICAL TRAINING MANUAL EFIS-ECAM INPUTS MAINTENANCE COURSE - M35 LINE MECHANICS (V2500-A5/ME)  31 - INDICATING/RECORDING SYSTEMS EIS ARCHITECTURE (1) May 10, 2006 Page SINGLE AISLE TECHNICAL TRAINING MANUAL ENGINE/WARNING DISPLAY PRESENTATION (1) GENERAL OVERVIEW U3U06191 - U0O35M0 - UM31P4000000003 The Engine/Warning Display (EWD) is normally on the upper Electronic Centralized Aircraft Monitoring (ECAM) Display Unit (DU) It is divided into two areas: the upper area and the lower area The upper area displays: - engine primary parameters, - Fuel On Board (FOB), - slats and flaps position The lower area is used for: - warning and caution messages, - memo messages MAINTENANCE COURSE - M35 LINE MECHANICS (V2500-A5/ME)  31 - INDICATING/RECORDING SYSTEMS ENGINE/WARNING DISPLAY PRESENTATION (1) May 10, 2006 Page U3U06191 - U0O35M0 - UM31P4000000003 SINGLE AISLE TECHNICAL TRAINING MANUAL GENERAL OVERVIEW MAINTENANCE COURSE - M35 LINE MECHANICS (V2500-A5/ME)  31 - INDICATING/RECORDING SYSTEMS ENGINE/WARNING DISPLAY PRESENTATION (1) May 10, 2006 Page SINGLE AISLE TECHNICAL TRAINING MANUAL ENGINE/WARNING DISPLAY PRESENTATION (1) ENGINE/WARNING DISPLAY AREAS UPPER AREA The symbols of the upper area are permanently displayed The parameters are provided in the form of analog and/or digital indications (refer to related chapter for detailed description) LEFT MEMO AREA Takeoff (TO) or landing memo, normal memo, independent failure messages, or primary failure messages and actions to are displayed in the left memo area As soon as a failure is detected, the memo messages are replaced by warning/caution messages RIGHT MEMO AREA U3U06191 - U0O35M0 - UM31P4000000003 Normal memo and secondary failure messages are displayed in the right memo area For example when an ENGine ANTI ICE P/B is set to ON, ENG A.ICE appears on the right memo area During TO and landing, most of the warnings are inhibited to avoid distraction of the crew For example, at TO, when the second engine is set to TO power and until the aircraft has reached 1.500 ft, TO INHIB is displayed MAINTENANCE COURSE - M35 LINE MECHANICS (V2500-A5/ME)  31 - INDICATING/RECORDING SYSTEMS ENGINE/WARNING DISPLAY PRESENTATION (1) May 10, 2006 Page SINGLE AISLE TECHNICAL TRAINING MANUAL INDIVIDUAL PRINT REPORT DESCRIPTION (3) APU MES/IDLE REPORT This report is generated when the engine is started with the APU It presents APU parameters during and after engine start, and at APU idle It also presents the last APU start parameters U3U06191 - U0O35M0 - UM31DF000000002 NOTE: MES means Main Engine Start MAINTENANCE COURSE - M35 LINE MECHANICS (V2500-A5/ME)  31 - INDICATING/RECORDING SYSTEMS INDIVIDUAL PRINT REPORT DESCRIPTION (3) May 10, 2006 Page 254 U3U06191 - U0O35M0 - UM31DF000000002 SINGLE AISLE TECHNICAL TRAINING MANUAL APU MES/IDLE REPORT MAINTENANCE COURSE - M35 LINE MECHANICS (V2500-A5/ME)  31 - INDICATING/RECORDING SYSTEMS INDIVIDUAL PRINT REPORT DESCRIPTION (3) May 10, 2006 Page 255 SINGLE AISLE TECHNICAL TRAINING MANUAL INDIVIDUAL PRINT REPORT DESCRIPTION (3) APU SHUTDOWN REPORT U3U06191 - U0O35M0 - UM31DF000000002 This report is generated when there is an APU auto shutdown due to a detected failure data sets are recorded at s intervals before the event MAINTENANCE COURSE - M35 LINE MECHANICS (V2500-A5/ME)  31 - INDICATING/RECORDING SYSTEMS INDIVIDUAL PRINT REPORT DESCRIPTION (3) May 10, 2006 Page 256 U3U06191 - U0O35M0 - UM31DF000000002 SINGLE AISLE TECHNICAL TRAINING MANUAL APU SHUTDOWN REPORT MAINTENANCE COURSE - M35 LINE MECHANICS (V2500-A5/ME)  31 - INDICATING/RECORDING SYSTEMS INDIVIDUAL PRINT REPORT DESCRIPTION (3) May 10, 2006 Page 257 SINGLE AISLE TECHNICAL TRAINING MANUAL INDIVIDUAL PRINT REPORT DESCRIPTION (3) LOAD REPORT U3U06191 - U0O35M0 - UM31DF000000002 This report is generated if excessive loads have been applied to the airframe during landing An aircraft bounce can also be detected It records aircraft aerodynamics parameter sets before, at and after a hard landing MAINTENANCE COURSE - M35 LINE MECHANICS (V2500-A5/ME)  31 - INDICATING/RECORDING SYSTEMS INDIVIDUAL PRINT REPORT DESCRIPTION (3) May 10, 2006 Page 258 U3U06191 - U0O35M0 - UM31DF000000002 SINGLE AISLE TECHNICAL TRAINING MANUAL LOAD REPORT MAINTENANCE COURSE - M35 LINE MECHANICS (V2500-A5/ME)  31 - INDICATING/RECORDING SYSTEMS INDIVIDUAL PRINT REPORT DESCRIPTION (3) May 10, 2006 Page 259 SINGLE AISLE TECHNICAL TRAINING MANUAL INDIVIDUAL PRINT REPORT DESCRIPTION (3) FREE PROGRAMMABLE REPORTS U3U06191 - U0O35M0 - UM31DF000000002 These reports are generated when specific conditions programmed by the airline are met Each data set contains up to 12 parameters chosen by the airline The report does not exceed 54 sets of data The sampling intervals, the average intervals and the history time of parameter recording are chosen by the airline MAINTENANCE COURSE - M35 LINE MECHANICS (V2500-A5/ME)  31 - INDICATING/RECORDING SYSTEMS INDIVIDUAL PRINT REPORT DESCRIPTION (3) May 10, 2006 Page 260 U3U06191 - U0O35M0 - UM31DF000000002 SINGLE AISLE TECHNICAL TRAINING MANUAL FREE PROGRAMMABLE REPORTS MAINTENANCE COURSE - M35 LINE MECHANICS (V2500-A5/ME)  31 - INDICATING/RECORDING SYSTEMS INDIVIDUAL PRINT REPORT DESCRIPTION (3) May 10, 2006 Page 261 SINGLE AISLE TECHNICAL TRAINING MANUAL INDIVIDUAL PRINT REPORT DESCRIPTION (3) ECS REPORT This report is generated when there is a malfunction in the air conditioning or pressurization system It records engine, aircraft and environmental data at and minutes before the event with 15 s intervals U3U06191 - U0O35M0 - UM31DF000000002 NOTE: ECS means Environmental Control System MAINTENANCE COURSE - M35 LINE MECHANICS (V2500-A5/ME)  31 - INDICATING/RECORDING SYSTEMS INDIVIDUAL PRINT REPORT DESCRIPTION (3) May 10, 2006 Page 262 U3U06191 - U0O35M0 - UM31DF000000002 SINGLE AISLE TECHNICAL TRAINING MANUAL ECS REPORT MAINTENANCE COURSE - M35 LINE MECHANICS (V2500-A5/ME)  31 - INDICATING/RECORDING SYSTEMS INDIVIDUAL PRINT REPORT DESCRIPTION (3) May 10, 2006 Page 263 SINGLE AISLE TECHNICAL TRAINING MANUAL COMPUTER REMOVAL AND INSTALLATION (3) COMPUTER REMOVAL/INSTALLATION U3U06191 - U0O35M0 - UM01D2000000001 Before starting a computer removal/installation procedure, the A/C has to be set-up for maintenance The first task is to make sure that the ground service network is energized and the access door is open and accessible Then make sure that the C/Bs listed in the removal of the computer procedure of Aircraft Maintenance Manual (AMM) is open The first action is to loosen the nut and then to lower the nut When the nut is lowered, pull the computer on its rack to disconnect the electrical connectors and remove the computer from its rack Before starting a computer installation procedure, clean and a visual inspection of the component interface and of the adjacent area First remove the blanking caps from the electrical connectors and make sure that the electrical connectors are clean and in the correct condition Then install the computer on its rack and push it on its rack to connect the electrical connectors Now you can engage the nuts on the studs and tighten them The installation is finished You can close the C/B The last actions of the computer installation are to a test through the MCDU and to close the access Make sure that the work area is clean and clear of tools and other items, close the access door and remove the access platform MAINTENANCE COURSE - M35 LINE MECHANICS (V2500-A5/ME)  31 - INDICATING/RECORDING SYSTEMS COMPUTER REMOVAL AND INSTALLATION (3) May 10, 2006 Page 264 U3U06191 - U0O35M0 - UM01D2000000001 SINGLE AISLE TECHNICAL TRAINING MANUAL COMPUTER REMOVAL/INSTALLATION MAINTENANCE COURSE - M35 LINE MECHANICS (V2500-A5/ME)  31 - INDICATING/RECORDING SYSTEMS COMPUTER REMOVAL AND INSTALLATION (3) May 10, 2006 Page 265 SINGLE AISLE TECHNICAL TRAINING MANUAL PUSHBUTTON REMOVAL AND INSTALLATION (3) PUSHBUTTON REMOVAL AND INSTALLATION U3U06191 - U0O35M0 - UM31Y2000000001 Before starting a P/B removal installation procedure, make sure that the lamp capsule is in the delatched (up) position when you remove it from an alternate action switch If the lamp capsule is not delached (up) when you remove it the switch cannot operate Then open the C/B of the circuit related to the P/BSW Put the removal tool lamp capsule extractor in the notches on the side of the head of the P/BSW Carefully pull the tool to remove the head of the P/BSW The head stays attached to the body of the P/BSW by the rods that turn Now you have to remove the body of the P/BSW First, fully loosen the two screws of the body but not lock them After, pull the head to remove the body Before starting the installation of a P/BSW, clean and make an inspection of the component interface and of the adjacent area Now, put the TOP mark in the up position and push the body of the P/BSW fully into its housing Torque the two screws of the body of the P/BSW Now, install the head in the body of the P/BSW To this, push the head until it touches the stop To finish the installation task close the C/B of the circuit related to the P/BSW After that, make sure that the work area is clean and clear of tools and other items MAINTENANCE COURSE - M35 LINE MECHANICS (V2500-A5/ME)  31 - INDICATING/RECORDING SYSTEMS PUSHBUTTON REMOVAL AND INSTALLATION (3) May 10, 2006 Page 266 U3U06191 - U0O35M0 - UM31Y2000000001 SINGLE AISLE TECHNICAL TRAINING MANUAL PUSHBUTTON REMOVAL AND INSTALLATION MAINTENANCE COURSE - M35 LINE MECHANICS (V2500-A5/ME)  31 - INDICATING/RECORDING SYSTEMS PUSHBUTTON REMOVAL AND INSTALLATION (3) May 10, 2006 Page 267 AIRBUS S.A.S 31707 BLAGNAC cedex, FRANCE STM REFERENCE U3U06191 MAY 2006 PRINTED IN FRANCE AIRBUS S.A.S 2006 ALL RIGHTS RESERVED AN EADS JOINT COMPANY WITH BAE SYSTEMS ... UM31P2000000002 SINGLE AISLE TECHNICAL TRAINING MANUAL EFIS-ECAM INPUTS MAINTENANCE COURSE - M35 LINE MECHANICS (V2500-A5/ME)  31 - INDICATING/ RECORDING SYSTEMS EIS ARCHITECTURE (1) May 10, 2006 Page SINGLE. ..  174 MAINTENANCE COURSE - M35 LINE MECHANICS (V2500-A5/ME)  31 - INDICATING/ RECORDING SYSTEMS TABLE OF CONTENTS May 11, 2006 Page SINGLE AISLE TECHNICAL TRAINING MANUAL EIS ARCHITECTURE... UM31D3000000001 SINGLE AISLE TECHNICAL TRAINING MANUAL ALERT CLASSIFICATION - GENERAL STATUS MAINTENANCE COURSE - M35 LINE MECHANICS (V2500-A5/ME)  31 - INDICATING/ RECORDING SYSTEMS ECAM ADVISORY