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Airbus A318 A319 A320 A321 Chapter 31 Indicating and Recording Systems Maintenance Manual AES Rev 40 2012
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Comprehensive Airbus A318, A319, A320 and A321 Aircraft Maintenance Manual Chapter 31 covering indicating and recording systems. This AES Revision 40 manual includes CFDS/CFDIU, digital flight-data recording, AIDS, ECAM and central warning systems, EIS, PFD and ND displays, display management, system pages, component removal/installation, servicing, operational tests, BITE functions and detailed system diagrams.
SKU: HD-AIRBUS-ATA31-AES40-2012
Category: Aircraft Maintenance Manuals
Tags: Airbus A318 A319 A320 A321 Chapter 31 Manual, Airbus A320 Chapter 31 Aircraft Maintenance Manual, Airbus AES Rev 40 2012 Maintenance Manual, Airbus Indicating Recording Systems Maintenance Manual
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Description
Airbus A318 / A319 / A320 / A321 Chapter 31 Indicating and Recording Systems Maintenance Manual – AES Rev 40 (2012)
The Airbus A318 A319 A320 A321 Chapter 31 Indicating and Recording Systems Maintenance Manual AES Rev 40 2012 is a detailed aircraft maintenance reference devoted to ATA Chapter 31 systems across the A318, A319, A320 and A321 family. At 2061 PDF pages, it brings together system descriptions, component architecture, maintenance practices, servicing instructions, removal and installation tasks, operational tests, BITE procedures and extensive technical illustrations for the aircraft’s indicating, warning, display, fault-reporting and data-recording equipment.
Coverage extends from the electrical clock and cockpit indicating panels through the Centralized Fault Display System, digital flight-data recording, Aircraft Integrated Data System functions, ECAM warning and system displays, the Electronic Instrument System, Primary Flight Display, Navigation Display and associated display-management equipment. The document also contains numerous aircraft-configuration applicability statements, making it important to follow the applicability shown with each individual task or figure.
Chapter 31 Maintenance and Diagnostic Scope
This Airbus Chapter 31 manual combines descriptive material with practical maintenance procedures. System architecture sections explain how computers, display units, acquisition concentrators, recorders, data interfaces and cockpit controls communicate. Maintenance sections then provide the task structure needed for component access, removal, installation, servicing, testing and system checks.
Centralized maintenance functions receive especially extensive treatment. The CFDS and CFDIU material covers architecture, system BITE communication, fault storage, maintenance phases, report generation, MCDU menu access, post-flight reporting, avionics status, ground scanning, system report/test functions, back-up mode operation and maintenance-filter handling. Procedures are included for reading Class 3 faults, accessing individual SYSTEM REPORT/TEST pages and carrying out CFDIU operational or BITE tests.
The recording-system material follows the Digital Flight Data Recording System through its interconnections, Flight Data Interface Unit or Flight Data Interface and Management Unit arrangements, Digital Flight Data Recorder, accelerometer and related interfaces. The manual includes DFDR readout procedures, coding-plug information, operational checks, recorder and accelerometer tests, and component removal and installation procedures. Detailed figures show recorders, system block diagrams, interconnection schematics and data-source relationships.
Flight Warning, ECAM and Electronic Instrument Systems
A large portion of the Airbus A318 A319 A320 A321 Chapter 31 Indicating and Recording Systems Maintenance Manual AES Rev 40 2012 is dedicated to the aircraft’s warning and electronic display architecture. Central Warning Systems coverage includes the Flight Warning Computers, System Data Acquisition Concentrators, ECAM control panel, warning and caution interfaces, ECAM display behavior, power supply relationships and system fault presentation.
Adjustment and test tasks address Flight Warning Computer operation, SDAC operation, ECAM control-panel testing, circuit-breaker monitoring and programming-data functions. Separate removal and installation sections cover equipment such as the Flight Warning Computer, SDAC, ECAM control panel and loudspeakers.
The Electronic Instrument System material develops the relationship between Display Management Computers, display units, EFIS controls, ECAM controls, PFDs and Navigation Displays. It includes system start and stop procedures, EIS operational testing, EFIS/ECAM switching tests, display-unit brightness functions, input tests and overall system testing. Wiring and interface illustrations show the relationships between display units, brightness controls, DMCs and transfer-selector functions.
Display and Recording References
Primary Flight Display and Navigation Display chapters contain extensive illustrated presentation material. PFD subjects include flight-director presentation, flight-path information, attitude-related displays and display parameters. Navigation Display coverage includes multiple operating presentations and navigation symbology together with TCAS indications, terrain display information and other display modes represented in the manual.
ECAM coverage extends beyond the warning display to system/status pages for aircraft functions including air conditioning and cabin pressure, electrical, flight controls, fuel, hydraulic, wheels, oxygen, bleed, APU, doors/oxygen and engine displays. These sections document the presentation and acquisition/interface relationships used to produce the information shown to the crew.
Complete PDF Bookmark Tree
Complete Bookmarks
The complete bookmarks in the “Airbus A318 A319 A320 A321 Chapter 31 Indicating and Recording Systems Maintenance Manual AES Rev 40 2012” are as follows:
Manual Front Matter
Chapter 05 – TIME LIMITS – MAINTENANCE CHECKS
Chapter 06 – DIMENSIONS AND AREAS
Chapter 07 – LIFTING AND SHORING
Chapter 08 – LEVELING AND WEIGHING
Chapter 09 – TOWING AND TAXIING
Chapter 10 – PARKING, MOORING, STORAGE & RETURN TO SERVICE
Chapter 11 – PLACARDS AND MARKINGS
Chapter 12 – SERVICING
Chapter 20 – STANDARD PRACTICES – AIRFRAME
Chapter 21 – AIR CONDITIONING
Chapter 22 – AUTO FLIGHT
Chapter 23 – COMMUNICATIONS
Chapter 24 – ELECTRICAL POWER
Chapter 25 – EQUIPMENT/FURNISHINGS
Chapter 26 – FIRE PROTECTION
Chapter 27 – FLIGHT CONTROLS
Chapter 28 – FUEL
Chapter 29 – HYDRAULIC POWER
Chapter 30 – ICE AND RAIN PROTECTION
+Chapter 31 – INDICATING/RECORDING SYSTEMSp. 1
Table of Contentsp. 1
+31-00 – INDICATING/RECORDING SYSTEMS – GENERALp. 27
+31-00-00 – INDICATING/RECORDING SYSTEMS – GENERALp. 27
+31-00-00 PB 001 CONF 00 – INDICATING/RECORDING SYSTEMS – GENERAL – DESCRIPTION AND OPERATIONp. 27
Generalp. 27
Description and Operationp. 28
Figure 31-00-00-12800-A – Indicating/Recording System – Electrical Clockp. 33
Figure 31-00-00-13400-A – Indicating/Recording System – CFDS Architecturep. 34
Figure 31-00-00-13900-A – Indicating/Recording System – Recording System Architecturep. 35
Figure 31-00-00-14400-A – Indicating/Recording System – FWS and EIS Components Layout in Cockpit.p. 36
Figure 31-00-00-14900-A – Indicating/Recording System – EFIS Acquisitionp. 37
Figure 31-00-00-15000-A – Indicating/Recording System – Typical PFD and NDp. 38
Figure 31-00-00-15200-A – Indicating/Recording System – ECAM Acquisitionp. 39
Figure 31-00-00-15300-A – Indicating/Recording System – Upper and Lower Display Unitsp. 40
Figure 31-00-00-15500-A – Indicating/Recording System-EIS – DUs Reconfigurationp. 41
+31-10 – INSTRUMENTS AND CONTROL PANELSp. 42
+31-10-00 – INSTRUMENTS AND CONTROL PANELSp. 42
+31-10-00 PB 201 CONF 00 – INSTRUMENTS AND CONTROL PANELS – MAINTENANCE PRACTICESp. 42
31-10-00-700-001-A – Test Program after Removal/Installation of a VU panelp. 42
+31-14 – OVERHEAD PANELp. 57
+31-14-25 – OVERHEAD CONTROL AND INDICATING PANELp. 57
+31-14-25 PB 201 CONF 00 – OVERHEAD CONTROL AND INDICATING PANEL – MAINTENANCE PRACTICESp. 57
+31-14-25-860-002-A – Floor Path Emergency-Lighting Inhibition With Removal of the Overhead Panel 25VUp. 57
Figure 31-14-25-991-00100-A – Panel 25VU – Location in the Cockpit and Rear Facep. 58
31-14-25-400-001-A – Installation of the 25VUp. 59
+31-21 – ELECTRICAL CLOCKp. 61
+31-21-00 – ELECTRICAL CLOCKp. 61
+31-21-00 PB 001 CONF 00 – ELECTRICAL CLOCK – DESCRIPTION AND OPERATIONp. 61
Generalp. 61
Component Locationp. 62
System Descriptionp. 63
Interfacep. 65
Operationp. 66
Figure 31-21-00-11200-B – Clock – Block Diagramp. 67
Figure 31-21-00-12800-B – Clock – Component Locationp. 68
Figure 31-21-00-14300-B – Clock – UTC/Elapsed Time Displayp. 69
Figure 31-21-00-15200-B – Clock – UTC/Chronometer Displayp. 70
Figure 31-21-00-15900-B – Clock – Date Displayp. 71
Figure 31-21-00-17000-B – Clock – Internal Block Diagramp. 72
Figure 31-21-00-19000-A – ARINC Word Structurep. 73
+31-21-00 PB 501 CONF 00 – ELECTRICAL CLOCK – ADJUSTMENT/TESTp. 74
+31-21-00-750-002-A – Procedure to set the Clockp. 74
Figure 31-21-00-991-00100-B – Clockp. 77
31-21-00-710-002-A – Operational Test of the Clockp. 78
+31-21-21 – CLOCKp. 80
+31-21-21 PB 401 CONF 00 – CLOCK – REMOVAL/INSTALLATIONp. 80
+31-21-21-000-001-A – Removal of the Clockp. 80
Figure 31-21-21-991-00100-A – Clockp. 82
Figure 31-21-21-991-00100-B – Clockp. 83
31-21-21-400-001-A – Installation of the Clockp. 84
+31-30 – CENTRALIZED FAULT DISPLAY SYSTEM (CFDS) AND DATA RECORDING SYSTEMp. 87
+31-30-00 – CENTRALIZED FAULT DISPLAY SYSTEM (CFDS) AND DATA RECORDING SYSTEMp. 87
+31-30-00 PB 001 CONF 00 – CENTRALIZED FAULT DISPLAY SYSTEM (CFDS) AND DATA RECORDING SYSTEM – DESCRIPTION AND OPERATIONp. 87
Generalp. 87
System Descriptionp. 88
Operationp. 89
Figure 31-30-00-13200-A – CFDS – Architecturep. 90
Figure 31-30-00-13600-A – CFDS – Maintenance and Data Recording Systemp. 91
Figure 31-30-00-13600-B – CFDS – Maintenance and Data Recording Systemp. 92
+31-32 – CENTRALIZED FAULT DISPLAY INTERFACE (CFDIU)p. 93
+31-32-00 – CENTRALIZED FAULT DISPLAY INTERFACE (CFDIU)p. 93
+31-32-00 PB 001 CONF 00 – CENTRALIZED FAULT DISPLAY INTERFACE (CFDIU) – DESCRIPTION AND OPERATIONp. 93
Generalp. 93
Component Locationp. 94
System Descriptionp. 95
Power Supplyp. 122
Interfacesp. 124
Component Descriptionp. 157
Operationp. 159
CFDS BITEp. 184
Figure 31-32-00-11500-H – CFDS – Component Locationp. 195
Figure 31-32-00-13200-A – CFDS – CFDIU Locationp. 196
Figure 31-32-00-13200-B – CFDS – CFDIU Locationp. 197
Figure 31-32-00-14700-C – CFDS – Block Diagramp. 198
Figure 31-32-00-14700-E – CFDS – Block Diagramp. 199
Figure 31-32-00-15000-A – CFDS – Multipurpose Control and Display Unit (MCDU)p. 200
Figure 31-32-00-15000-B – CFDS – Multipurpose Control and Display Unit (MCDU)p. 201
Figure 31-32-00-15100-D – CFDS – Interconnection with the MCDUsp. 202
Figure 31-32-00-15100-I – CFDS – Interconnection with the MCDUsp. 203
Figure 31-32-00-16000-A – CFDIU – Connection With Different System Typesp. 204
Figure 31-32-00-17100-A – CFDIU – Fault Storage "at the latest" in System BITE and Transmission to the CFDIU : Normal Mode/Type 1 Systemsp. 205
Figure 31-32-00-17100-C – CFDIU – Fault Storage "at the latest" in System BITE and Transmission to the CFDIU: Normal Mode/Type 1 Systemsp. 206
Figure 31-32-00-17200-A – CFDIU – Fault Storage "at the soonest" in System BITE and Transmission to the CFDIU : Normal Mode/Type 1 Systemsp. 207
Figure 31-32-00-17200-C – CFDIU – Fault Storage "at the soonest" in System BITE and transmission to the CFDIU: Normal Mode/Type 1 Systemsp. 208
Figure 31-32-00-17600-B – CFDIU – Fault Storage in System BITE and Transmission to the CFDIU : Normal Mode/Type 2 Systemsp. 209
Figure 31-32-00-17600-D – CFDIU – Fault Storage in System BITE and Transmission to the CFDIU: Normal Mode/Type 2 Systemsp. 210
Figure 31-32-00-17900-A – CFDIU – Faults Storage "at the soonest" in CFDIU : Normal Modep. 211
Figure 31-32-00-17900-C – CFDIU – Faults Storage "at the soonest" in CFDIU: Normal Modep. 212
Figure 31-32-00-18000-A – CFDIU – Faults Storage "at the latest" in CFDIU : Normal Modep. 213
Figure 31-32-00-18000-C – CFDIU – Faults Storage "at the latest" in CFDIU: Normal Modep. 214
Figure 31-32-00-18100-A – CFDIU – Example of CFDIU Operation – Type 3 Systemp. 215
Figure 31-32-00-18200-A – CFDIU – Description of the Fault Correlation Processingp. 216
Figure 31-32-00-19400-A – CFDIU – Maintenance Phase Logic (Nominal Case)p. 217
Figure 31-32-00-19500-B – Maintenance Phases – Logic Diagram (transition to flight "at the soonest". FLT N°. parameter entered prior to engine)p. 218
Figure 31-32-00-19600-B – Maintenance Phases – Logic Diagram (transition to flight "at the latest". FLT N° . parameter not entered)p. 219
Figure 31-32-00-19700-A – CFDIU – Computation of Maintenance Phases (Downgraded Case – Loss of Both FWCs)p. 220
Figure 31-32-00-19800-C – CFDIU – CFDIU Transmission to BITE – Normal Mode (Label 227)p. 221
Figure 31-32-00-19800-E – CFDIU – CFDIU Transmission to BITE – Normal Mode (Label 227)p. 222
Figure 31-32-00-22300-A – CFDIU – Power Supplyp. 223
Figure 31-32-00-22300-B – CFDIU – Power Supplyp. 224
Figure 31-32-00-23800-D – CFDIU – Inputs/Outputs Architecturep. 225
Figure 31-32-00-23800-E – CFDIU – Inputs/Outputs Architecturep. 226
Figure 31-32-00-27000-C – CFDIU – Input/Output Labels Listp. 227
Figure 31-32-00-27000-D – CFDIU – Input/Output Labels Listp. 228
Figure 31-32-00-28500-A – CFDIU – Printer Interface Architecturep. 229
Figure 31-32-00-28600-A – CFDIU – Process for Printing a Pagep. 230
Figure 31-32-00-31600-A – CFDIU – Internal Architecturep. 231
Figure 31-32-00-31700-A – CFDIU – Exploded Viewp. 232
Figure 31-32-00-34400-C – CFDIU – CFDS Menu on Groundp. 233
Figure 31-32-00-34400-F – CFDIU – CFDS Menu on Groundp. 234
Figure 31-32-00-34400-G – CFDIU – CFDS Menu on Groundp. 235
Figure 31-32-00-34600-C – CFDIU – CFDS Menu in Flightp. 236
Figure 31-32-00-34600-F – CFDIU – CFDS Menu in Flightp. 237
Figure 31-32-00-34600-G – CFDIU – CFDS Menu in Flightp. 238
Figure 31-32-00-35000-C – CFDIU – LAST (or CURRENT) LEG REPORTp. 239
Figure 31-32-00-35200-C – CFDIU – LAST (or CURRENT) LEG ECAM REPORTp. 240
Figure 31-32-00-35400-C – CFDIU – PREVIOUS LEGS REPORTp. 241
Figure 31-32-00-35600-C – CFDIU – AVIONICS STATUSp. 242
Figure 31-32-00-35800-C – CFDIU – POST FLIGHT REPORTp. 243
Figure 31-32-00-35800-D – CFDIU – POST FLIGHT REPORTp. 244
Figure 31-32-00-36100-A – PFR/FILTER PROGRAM – Sheet 1/4p. 245
Figure 31-32-00-36100-I – PFR/FILTER PROGRAM – Sheet 1/4p. 246
Figure 31-32-00-36100-J – PFR/FILTER PROGRAM – Sheet 1/4p. 247
Figure 31-32-00-36200-B – CFDIU – GMT/DATE INITIALIZATIONp. 248
Figure 31-32-00-36300-A – CFDIU – Current Flight Reportp. 249
Figure 31-32-00-36500-B – CFDIU – POST FLIGHT REPORT (Not Filtered) – Sheet 2/4p. 250
Figure 31-32-00-36500-C – CFDIU – POST FLIGHT REPORT (Not Filtered) – Sheet 2/4p. 251
Figure 31-32-00-36600-B – CFDIU – Printing of Memorized Filter – Sheet 3/4p. 252
Figure 31-32-00-36600-C – CFDIU – Pinting of Memorized Filter – Sheet 3/4p. 253
Figure 31-32-00-36700-B – CFDIU – POST FLIGHT REPORT (Filtered) – Sheet 4/4p. 254
Figure 31-32-00-36700-C – CFDIU – POST FLIGHT REPORT (Filtered) – Sheet 4/4p. 255
Figure 31-32-00-36900-C – CFDIU – PASSWORD CHANGEp. 256
Figure 31-32-00-36900-D – CFDIU – PASSWORD CHANGEp. 257
Figure 31-32-00-37100-B – CFDIU – SYSTEM REPORT/TESTp. 258
Figure 31-32-00-38100-C – CFDIU – Establishment and Availability of the Reports Listed in the CFDS menu by the MCDU – Sheet 1/2p. 259
Figure 31-32-00-38100-E – CFDIU – Establishment and Availability of the Reports Listed in the CFDS menu by the MCDU – Sheet 1/2p. 260
Figure 31-32-00-38200-C – CFDIU – Establishment and Availability of the Reports Listed in the CFDS menu by the MCDU – Sheet 2/2p. 261
Figure 31-32-00-38200-E – CFDIU – Establishment and Availability of the Reports Listed in the CFDS menu by the MCDU – Sheet 2/2p. 262
Figure 31-32-00-38700-B – CFDIU – Type 1 System Reportp. 263
Figure 31-32-00-38800-C – CFDIU – Type 1 System Report – Descriptionp. 264
Figure 31-32-00-38900-A – CFDIU – LRU IDENTIFICATIONp. 265
Figure 31-32-00-38900-B – CFDIU – LRU IDENTIFICATIONp. 266
Figure 31-32-00-39000-B – CFDIU – Type 1 System Report – TROUBLE SHOOTING DATA DESCRIPTIONp. 267
Figure 31-32-00-39100-B – CFDIU – Establishment and Availability of the Reports – Type 1 and 2 Systemsp. 268
Figure 31-32-00-39100-D – CFDIU – Establishment and Availability of the Reports – Type 1 and 2 systemsp. 269
Figure 31-32-00-39300-B – CFDIU – Type 2 System Reportp. 270
Figure 31-32-00-39400-B – CFDIU – Type 2 System Report – Descriptionp. 271
Figure 31-32-00-39600-B – CFDIU – Type 3 System Reportp. 272
Figure 31-32-00-40600-G – CFDIU – Modification of Main Menu for Transmission to the Groundp. 273
Figure 31-32-00-40600-O – CFDIU – Modification of Main Menu for Transmission to the Groundp. 274
Figure 31-32-00-41000-A – CFDIU – AVIONICS DATAp. 275
Figure 31-32-00-41200-D – CFDIU – Manual Message Transmissionp. 276
Figure 31-32-00-42300-C – CFDIU – BACKUP MODE Through MCDU – On Groundp. 277
Figure 31-32-00-42500-A – CFDIU – Test Plug Power Supplyp. 278
Figure 31-32-00-46500-B – Indicating/Recording Systems – SYSTEM REPORT/TESTp. 279
Figure 31-32-00-46700-B – CFDIU – SYSTEM REPORT/TESTp. 280
Figure 31-32-00-46800-B – CFDIU – GROUND SCANNINGp. 281
+31-32-00 PB 201 CONF 00 – CENTRALIZED FAULT DISPLAY INTERFACE (CFDIU) – MAINTENANCE PRACTICESp. 282
31-32-00-869-001-A – Procedure for CFDS Switching to Back-up Modep. 282
31-32-00-869-002-A – Procedure for Class 3 Faults Readingp. 284
31-32-00-869-003-A – Procedure to use CFDS, the aircraft being in the jacking configuration .p. 287
+31-32-00-860-001-A – Procedure to Get Access to the SYSTEM REPORT/TEST Menu Pagep. 290
Figure 31-32-00-991-00100-A – CFDS – SYSTEM REPORT/TEST – Menu Pagep. 292
+31-32-00-860-002-A – Procedure to Get Access to the SYSTEM REPORT/TEST/AIR COND Pagep. 293
Figure 31-32-00-991-00200-E – CFDS – SYSTEM REPORT/TEST/AIR COND Pagep. 295
+31-32-00-860-003-A – Procedure to Get Access to the SYSTEM REPORT/TEST/COM Pagep. 296
Figure 31-32-00-991-00300-A – CFDS – SYSTEM REPORT/TEST/COM Pagep. 299
+31-32-00-860-004-A – Procedure to Get Access to the SYSTEM REPORT/TEST/ELEC Pagep. 300
Figure 31-32-00-991-00400-B – CFDS – SYSTEM REPORT/TEST/ELEC Pagep. 302
+31-32-00-860-005-A – Procedure to Get Access to the SYSTEM REPORT/TEST FIRE PROT Pagep. 303
Figure 31-32-00-991-00500-B – CFDS – SYSTEM REPORT/TEST – FIRE PROT pagep. 305
+31-32-00-860-006-A – Procedure to Get Access to the SYSTEM REPORT/TEST F/CTL Pagep. 306
Figure 31-32-00-991-00600-B – CFDS – SYSTEM REPORT/TEST/F/CTL Pagep. 308
+31-32-00-860-007-A – Procedure to Get Access to the SYSTEM REPORT/TEST/ICE & RAIN Pagep. 309
Figure 31-32-00-991-00700-D – CFDS – SYSTEM REPORT/TEST/ICE & RAIN Pagep. 311
+31-32-00-860-008-A – Procedure to Get Access to the SYSTEM REPORT/TEST/INST Pagep. 312
Figure 31-32-00-991-00800-B – CFDS – SYSTEM REPORT/TEST/INST Pagep. 314
+31-32-00-860-009-A – Procedure to Get Access to the SYSTEM REPORT/TEST/L/G Pagep. 315
Figure 31-32-00-991-00900-C – CFDS – SYSTEM REPORT/TEST/L/G Pagep. 317
+31-32-00-860-010-A – Procedure to Get Access to the SYSTEM REPORT/TEST NAV Pagep. 318
Figure 31-32-00-991-01000-B – CFDS – SYSTEM REPORT/TEST/NAV Pagep. 321
+31-32-00-860-011-A – Procedure to Get Access to the SYSTEM REPORT/TEST/PNEU Pagep. 322
Figure 31-32-00-991-01100-A – CFDS – SYSTEM REPORT/TEST/PNEU Pagep. 324
+31-32-00-860-012-A – Procedure to Get Access to the SYSTEM REPORT/TEST/ENG Pagep. 325
Figure 31-32-00-991-01200-B – CFDS – SYSTEM REPORT/TEST/ENG Pagep. 327
+31-32-00-860-013-A – Procedure to Get Access to the SYSTEM REPORT/TEST/INFO SYS Pagep. 328
Figure 31-32-00-991-01400-A – CFDS – SYSTEM REPORT/TEST/INFO SYS Pagep. 330
+31-32-00-860-014-A – Procedure to Get Access to the SYSTEM REPORT/TEST/FUEL Pagep. 331
Figure 31-32-00-991-01500-A – CFDS – SYSTEM REPORT/TEST FUEL Pagep. 333
+31-32-00 PB 301 CONF 00 – CENTRALIZED FAULT DISPLAY INTERFACE (CFDIU) – SERVICINGp. 334
31-32-00-600-001-A – Uploading of the Maintenance Filter Data Base to the CFDIU with the Portable Data Loader (SFIM)p. 334
31-32-00-600-001-D – Uploading of the Maintenance Filter Data Base to the CFDIU with the Portable Data Loader (SFIM)p. 337
31-32-00-600-002-A – Activation/Deactivation of the PFR (Post Flight Report) FILTERp. 340
31-32-00-610-002-A – Activation/Deactivation of the Automatic Post Flight Report Printoutp. 343
+31-32-00 PB 501 CONF 00 – CENTRALIZED FAULT DISPLAY INTERFACE (CFDIU) – ADJUSTMENT/TESTp. 346
31-32-00-710-002-A – Operational Test of the Back-up Modep. 346
31-32-00-740-002-A – BITE Test of the Centralized Fault Display Interface Unit (CFDIU)p. 349
31-32-00-740-003-A – Ground Scanning of the CFDIUp. 351
31-32-00-740-009-A – Read the AVIONICS STATUS on the MCDUp. 353
31-32-00-750-001-A – CFDIU TIME/DATE Initializationp. 355
+31-32-34 – INTERFACE UNIT – CENTRALIZED FAULT DISPLAY (CFDIU)p. 357
+31-32-34 PB 401 CONF 00 – INTERFACE UNIT – CENTRALIZED FAULT DISPLAY (CFDIU) – REMOVAL/INSTALLATIONp. 357
+31-32-34-000-001-A – Removal of the CFDIUp. 357
Figure 31-32-34-991-00100-A – Centralized Fault Display Interface Unit (CFDIU)p. 359
31-32-34-400-001-A – Installation of the CFDIUp. 360
+31-33 – DIGITAL FLIGHT DATA RECORDING SYSTEM INTERCONNECTIONp. 363
+31-33-00 – DIGITAL FLIGHT DATA RECORDING SYSTEM INTERCONNECTIONp. 363
+31-33-00 PB 001 CONF 00 – DIGITAL FLIGHT DATA RECORDING SYSTEM INTERCONNECTION – DESCRIPTION AND OPERATIONp. 363
Generalp. 363
Component Locationp. 364
System Descriptionp. 365
System Power Supplyp. 367
Interfacep. 369
Component Descriptionp. 377
Operation/Control and Indicatingp. 385
Test BITEp. 388
Figure 31-33-00-12400-O – Component Locationp. 391
Figure 31-33-00-12400-X – Component Locationp. 393
Figure 31-33-00-14500-D – System Block Diagramp. 395
Figure 31-33-00-14500-F – System Block Diagramp. 396
Figure 31-33-00-14600-B – DFDRS Interconnection Schematic 1/2p. 397
Figure 31-33-00-14700-A – DFDRS Interconnection Schematic 2/2p. 398
Figure 31-33-00-15900-B – Power Supplyp. 399
Figure 31-33-00-15900-G – Power Supplyp. 400
Figure 31-33-00-17800-B – Block Diagram of Parameter Sourcesp. 401
Figure 31-33-00-17800-C – Block Diagram of Parameter Sourcesp. 402
Figure 31-33-00-19300-B – DFDRS – Input Schematicp. 403
Figure 31-33-00-19300-C – DFDRS – Input Schematicp. 404
Figure 31-33-00-22200-B – Flight Data Interface Unitp. 405
Figure 31-33-00-22200-D – Flight Data Interface and Management Unitp. 406
Figure 31-33-00-22300-B – Functional Block Diagramp. 407
Figure 31-33-00-22300-C – Functional Block Diagramp. 408
Figure 31-33-00-22400-B – System Internal Interfacep. 409
Figure 31-33-00-22400-C – System Internal Interfacep. 410
Figure 31-33-00-23100-D – Digital Flight Data Recorderp. 411
Figure 31-33-00-23100-G – Digital Flight Data Recorderp. 412
Figure 31-33-00-23200-G – DFDR – Functional Block Diagramp. 413
Figure 31-33-00-23200-I – DFDR – Functional Block Diagramp. 414
Figure 31-33-00-23300-C – DFDR – Interfacep. 415
Figure 31-33-00-23300-E – DFDR – Interfacep. 416
Figure 31-33-00-23300-F – DFDR – Interfacep. 417
Figure 31-33-00-23700-A – Linear Accelerometerp. 418
Figure 31-33-00-23800-A – LA – Functional Block Diagramp. 419
Figure 31-33-00-27400-B – Power Interlockp. 420
Figure 31-33-00-27400-G – Power Interlockp. 421
Figure 31-33-00-27900-A – CTL PNLp. 422
Figure 31-33-00-28000-A – Event Marker Buttonp. 423
+31-33-00 PB 201 CONF 00 – DIGITAL FLIGHT DATA RECORDING SYSTEM INTERCONNECTION – MAINTENANCE PRACTICESp. 424
31-33-00-710-013-A – DELETEDp. 424
+31-33-00-710-009-A – Readout Procedure of the Digital Flight Data Recorderp. 425
Figure 31-33-00-991-00300-CR – DFDR Ground Support Equipment Connectorp. 428
+31-33-00-710-010-A – Procedure to Use the Aircraft Coding Plug 197VC-Ap. 429
Figure 31-33-00-991-00800-A – Coding Table of the Coding Plug 197VC-Ap. 433
+31-33-00 PB 501 CONF 00 – DIGITAL FLIGHT DATA RECORDING SYSTEM INTERCONNECTION – ADJUSTMENT/TESTp. 434
+31-33-00-710-001-A – Operational Test of the Power Interlocks and Status Monitoringp. 434
Figure 31-33-00-991-00100-A – DFDR-Testp. 437
Figure 31-33-00-991-00100-B – DFDR-Testp. 439
+31-33-00-710-006-A – Operational Check of DFDR through the MCDUp. 441
Figure 31-33-00-991-00200-A – FDIU-Testp. 445
Figure 31-33-00-991-00200-B – DFDR-Testp. 447
Figure 31-33-00-991-00200-C – DFDR-Testp. 449
31-33-00-710-007-A – Operational Test of the DFDRp. 451
31-33-00-710-011-A – Functional Test of the Three-Axis-Accelerometerp. 453
31-33-00-710-016-A – Operational Test of the Three-Axis-Accelerometer thru the MCDUp. 455
31-33-00-710-015-A – Operational Check of ULBp. 457
+31-33-16 – ACCELEROMETER – THREE AXISp. 461
+31-33-16 PB 401 CONF 00 – ACCELEROMETER – THREE AXIS – REMOVAL/INSTALLATIONp. 461
+31-33-16-000-001-A – Removal of the Three-Axis-Accelerometer (LA)p. 461
Figure 31-33-16-991-00100-B – Three-Axis-Accelerometer – Removal/Installationp. 463
31-33-16-400-001-A – Installation of the Three-Axis-Accelerometer (LA)p. 464
+31-33-34 – INTERFACE UNIT – FLIGHT DATA (FDIU)p. 466
+31-33-34 PB 401 CONF 00 – INTERFACE UNIT – FLIGHT DATA (FDIU) – REMOVAL/INSTALLATIONp. 466
+31-33-34-000-001-A – Removal of the Flight Data Interface Unit (FDIU)p. 466
Figure 31-33-34-991-00100-A – Flight Data Interface Unit (FDIU)p. 468
31-33-34-400-001-A – Installation of the Flight Data Interface Unit (FDIU)p. 469
+31-33-55 – RECORDER – DIGITAL FLIGHT DATA (DFDR)p. 471
+31-33-55 PB 401 CONF 00 – RECORDER – DIGITAL FLIGHT DATA (DFDR) – REMOVAL/INSTALLATIONp. 471
+31-33-55-000-001-A – Removal of the Digital Flight Data Recorder (DFDR)p. 471
Figure 31-33-55-991-00100-H – Removal/Installation of the DFDRp. 473
31-33-55-400-002-A – Installation of the Digital Flight Data Recorder (DFDR)p. 474
+31-33-55-920-001-A – Discard Underwater Locator Beacon Batteryp. 476
Figure 31-33-55-991-00200-E – Removal/Installation – Underwater Locator Beacon Batteryp. 479
+31-35 – MULTIFUNCTION PRINTINGp. 480
+31-35-00 – MULTIFUNCTION PRINTINGp. 480
+31-35-00 PB 001 CONF 00 – MULTIFUNCTION PRINTING – DESCRIPTION AND OPERATIONp. 480
Generalp. 480
Component Locationp. 481
System Descriptionp. 482
Power Supplyp. 483
Interfacep. 484
Component Descriptionp. 486
Operationp. 487
Testp. 488
Figure 31-35-00-13500-A – Printer – Component Locationp. 489
Figure 31-35-00-15800-A – Printer – Interconnection Block Diagramp. 490
Figure 31-35-00-18400-A – Printer – Internal Block Diagramp. 491
+31-35-00 PB 501 CONF 00 – MULTIFUNCTION PRINTING – ADJUSTMENT/TESTp. 492
31-35-00-710-001-A – Operational Test of the Printerp. 492
+31-35-22 – PRINTERp. 494
+31-35-22 PB 301 CONF 00 – PRINTER – SERVICINGp. 494
+31-35-22-600-001-A – Servicing of the Printerp. 494
Figure 31-35-22-991-00200-A – Printerp. 496
+31-35-22 PB 401 CONF 00 – PRINTER – REMOVAL/INSTALLATIONp. 497
+31-35-22-000-001-A – Removal of the Printerp. 497
Figure 31-35-22-991-00100-A – Printerp. 499
31-35-22-400-001-A – Installation of the Printerp. 500
+31-36 – AIDS INTERCONNECTIONp. 502
+31-36-00 – AIDS INTERCONNECTIONp. 502
+31-36-00 PB 001 CONF 01 – AIDS INTERCONNECTION (DMU, DAR) – DESCRIPTION AND OPERATIONp. 502
Generalp. 502
Component Locationp. 503
System Descriptionp. 504
Power Supplyp. 509
Interfacep. 510
Component Descriptionp. 552
Operation/Control and Indicatingp. 587
Test BITEp. 618
Figure 31-36-00-12900-A – Component Locationp. 628
Figure 31-36-00-12900-K – Component Locationp. 630
Figure 31-36-00-14600-A – System Block Diagramp. 632
Figure 31-36-00-14600-D – System Block Diagramp. 633
Figure 31-36-00-15800-A – AIDS – Power Supplyp. 634
Figure 31-36-00-15800-C – AIDS – Power Supplyp. 635
Figure 31-36-00-26100-A – AIDS – DMUp. 636
Figure 31-36-00-26100-C – Flight Data Interface and Management Unit (FDIMU)p. 637
Figure 31-36-00-26200-A – DMU Internal Componentsp. 638
Figure 31-36-00-26200-D – FDIMU Internal Componentsp. 639
Figure 31-36-00-26300-A – DMU Internal Block Diagramp. 640
Figure 31-36-00-26300-E – FDIMU Internal Block Diagramp. 641
Figure 31-36-00-26400-A – DMU DITS Input Bus and Input Data Flowp. 642
Figure 31-36-00-26400-D – FDIMU Internal Signal Flowp. 643
Figure 31-36-00-26500-C – FDIMU Interfacep. 647
Figure 31-36-00-27200-A – AIDS Flight Phases – Table 11p. 649
Figure 31-36-00-34100-A – MCDUp. 650
Figure 31-36-00-34200-A – Several MCDU'sp. 651
Figure 31-36-00-34300-A – AIDS Main Menup. 652
Figure 31-36-00-34300-D – AIDS Main Menup. 653
Figure 31-36-00-34800-A – MCDU – Return Functionp. 654
Figure 31-36-00-34800-D – MCDU – Return Functionp. 655
Figure 31-36-00-34900-A – MCDU – Display Printp. 656
Figure 31-36-00-36000-A – Parameter Label Call-Upp. 657
Figure 31-36-00-36000-D – Parameter Label Call-Upp. 658
Figure 31-36-00-36100-A – Parameter Alpha Call-Upp. 659
Figure 31-36-00-36100-D – Parameter Alpha Call-Upp. 660
Figure 31-36-00-36200-A – Parameter Menup. 661
Figure 31-36-00-36200-D – Parameter Menup. 662
Figure 31-36-00-36300-A – AIDS DMU Programming (Sheet 1/4)p. 663
Figure 31-36-00-36300-D – AIDS DMU Programming (Sheet 1/4)p. 664
Figure 31-36-00-36400-A – AIDS DMU Programming (Sheet 2/4)p. 665
Figure 31-36-00-36500-A – AIDS DMU Programming (Sheet 3/4)p. 666
Figure 31-36-00-36600-A – AIDS DMU Programming (Sheet 4/4)p. 667
Figure 31-36-00-36700-A – SAR Recording (Sheet 1/3)p. 668
Figure 31-36-00-36700-D – SAR Recording (Sheet 1/3)p. 669
Figure 31-36-00-36800-A – SAR Recording (Sheet 2/3)p. 670
Figure 31-36-00-36900-A – SAR Recording (Sheet 3/3)p. 671
Figure 31-36-00-37000-A – Remote Print Assignmentp. 672
Figure 31-36-00-37000-D – Remote Print Assignmentp. 673
Figure 31-36-00-37100-A – AIDS Software Loadingp. 674
Figure 31-36-00-37100-D – AIDS Software Loadingp. 675
Figure 31-36-00-37200-A – AIDS Database Loadingp. 676
Figure 31-36-00-37200-D – AIDS Database Loadingp. 677
Figure 31-36-00-37300-A – AIDS Previous Reportsp. 678
Figure 31-36-00-37300-D – AIDS Previous Reportsp. 679
Figure 31-36-00-37400-A – AIDS Stored Reportsp. 680
Figure 31-36-00-37400-D – AIDS Stored Reportsp. 681
Figure 31-36-00-37500-A – AIDS – List of Stored Reportsp. 682
Figure 31-36-00-37500-B – AIDS – List of Stored Reportsp. 683
Figure 31-36-00-37600-A – Manual Request Reportsp. 684
Figure 31-36-00-37600-D – Manual Request Reportsp. 685
Figure 31-36-00-37700-B – AIDS Disk Ident Pagep. 686
Figure 31-36-00-37800-B – AIDS Disk Directory Pagep. 687
Figure 31-36-00-37900-B – AIDS Disk DAR Record Pagep. 688
Figure 31-36-00-40500-A – DMU Power-up Testp. 689
Figure 31-36-00-41000-A – Last Leg Reportp. 690
Figure 31-36-00-41200-A – Previous Legs Reportsp. 691
Figure 31-36-00-41400-A – LRU Identificationp. 692
Figure 31-36-00-41400-B – LRU Identificationp. 693
Figure 31-36-00-41600-A – Ground Scanningp. 694
Figure 31-36-00-41800-A – Trouble Shoot Datap. 695
Figure 31-36-00-41800-B – Trouble Shoot Datap. 696
Figure 31-36-00-42000-A – Class 3 Faultsp. 697
Figure 31-36-00-42200-A – Test Menup. 698
Figure 31-36-00-42400-A – Ground Reportp. 699
Figure 31-36-00-42600-A – Software Load Statusp. 700
Figure 31-36-00-42600-B – Software Load Statusp. 701
+31-36-00 PB 201 CONF 00 – AIDS INTERCONNECTION – MAINTENANCE PRACTICESp. 702
31-36-00-740-004-A – Update of the APU Hours and Cycles in the DMU after APU, ECB or DMU Replacementp. 702
31-36-00-740-013-A – Update of the APU Hours and Cycles in the FDIMU after APU, ECB or FDIMU Replacementp. 704
31-36-00-740-005-A – Update of the Engine Hours and Cycles in the DMU after Engine or DMU Replacementp. 706
31-36-00-740-014-A – Update of the Engine Hours and Cycles in the FDIMUp. 708
31-36-00-740-006-A – Printout of the APU Hours and Cyclesp. 710
31-36-00-740-007-A – Printout of the Engine Hours and Cyclesp. 712
31-36-00-740-008-A – Access to the Parameter Call-Up Menusp. 715
31-36-00-740-009-A – DMU Programming Proceduresp. 718
31-36-00-740-016-A – FDIMU Programming Proceduresp. 722
+31-36-00-740-010-A – Printout of Stored Reportsp. 726
Figure 31-36-00-991-00300-A – Example for Print Out of Stored Reports.p. 729
+31-36-00-740-011-A – Printout of Manually Requested Reportsp. 730
Figure 31-36-00-991-00500-A – Example for Print Out of Manually Requested Reportsp. 733
31-36-00-710-004-A – AIDS Software Load Procedurep. 734
31-36-00-710-013-A – FDIMU AIDS Software Load Procedurep. 739
31-36-00-710-008-A – AIDS Software Load Procedure through the PCMCIA-Card (PCMCIA = Personal Computer Memory Card International Association)p. 745
31-36-00-710-010-A – Dump Procedure to Download DMU Datap. 749
31-36-00-710-014-A – Dump Procedure to Download FDIMU Datap. 752
31-36-00-710-016-A – Downloading Procedure of FDIMU/DMU Data on a PCMCIA Cardp. 755
+31-36-00-000-001-A – Removal of the Personal Computer Memory Card (PCMCIA) of the FDIMU/DMUp. 757
Figure 31-36-00-991-00100-A – Removal / Installation of the Personal Computer Memory Card (PCMCIA)p. 759
Figure 31-36-00-991-00100-E – Removal / Installation of the Personal Computer Memory Card (PCMCIA)p. 760
31-36-00-400-001-A – Installation of the Personal Computer Memory Card (PCMCIA) of the FDIMU/DMUp. 761
+31-36-00-960-003-A – Replacement of the FDIMU Batteriesp. 764
Figure 31-36-00-991-00600-A – Replacement of the FDIMU Batteriesp. 766
+31-36-00-960-002-A – Replacement of the DMU Batteriesp. 767
Figure 31-36-00-991-00200-A – Replacement of the DMU Batteriesp. 769
+31-36-00 PB 501 CONF 00 – AIDS INTERCONNECTION – ADJUSTMENT/TESTp. 770
31-36-00-710-001-A – Test of the DMUp. 770
31-36-00-740-012-A – Test of the FDIMUp. 772
+31-36-34 – MANAGEMENT UNIT – DATA (DMU OR FDIMU)p. 776
+31-36-34 PB 401 CONF 00 – MANAGEMENT UNIT – DATA (DMU OR FDIMU) – REMOVAL/INSTALLATIONp. 776
+31-36-34-000-001-A – Removal of the Data Management Unit (DMU)p. 776
Figure 31-36-34-991-00100-A – Data Management Unit (DMU)p. 778
+31-36-34-000-002-A – Removal of the FDIU/DMU (FDIMU)p. 779
Figure 31-36-34-991-00500-A – Flight Data Interface Management Unit (FDIMU)p. 781
31-36-34-400-001-A – Installation of the Data Management Unit (DMU)p. 782
31-36-34-400-002-A – Installation of the FDIU/DMU (FDIMU)p. 785
+31-37 – AIDS INPUT INTERFACEp. 788
+31-37-00 – AIDS INPUT INTERFACEp. 788
+31-37-00 PB 001 CONF 00 – AIDS INPUT INTERFACE – DESCRIPTION AND OPERATIONp. 788
Generalp. 788
System descriptionp. 789
Figure 31-37-00-12600-D – DMU Source Block Diagram (sheet 1/2)p. 810
Figure 31-37-00-12600-H – FDIMU (DMU-Part) Source Block Diagram (sheet 1/2)p. 811
Figure 31-37-00-12700-C – DMU Source Block Diagram (sheet 2/2)p. 812
Figure 31-37-00-12700-D – FDIMU (DMU-Part) Source Block Diagram (sheet 2/2)p. 813
+31-37-00 PB 201 CONF 00 – AIDS INPUT INTERFACE – MAINTENANCE PRACTICESp. 814
+31-37-00-200-001-A – Check of the Load-Report Parameter after Hard/Overweight Landing or Excessive Turbulencep. 814
Figure 31-37-00-991-00100-C – Load-Report Print-Out – Descriptionp. 818
Figure 31-37-00-991-00200-B – Load Report – Event Sequencep. 819
Figure 31-37-00-991-00300-A – Load Report – Flow Chart (Hard/Overweight Landing)p. 820
Figure 31-37-00-991-00300-B – Load Report – Flow Chart (Hard/Overweight Landing)p. 821
Figure 31-37-00-991-00400-A – Load Report – Flow Chart (Excessive Turbulence)p. 822
+31-37-21 – AIDS – ECS REPORTSp. 823
+31-37-21 PB 001 CONF 00 – AIDS – ECS REPORTS – DESCRIPTION AND OPERATIONp. 823
Generalp. 823
Reportsp. 824
Figure 31-37-21-12800-A – ECS Reportp. 842
Figure 31-37-21-12800-B – ECS Reportp. 843
+31-37-49 – AIDS – APU REPORTSp. 844
+31-37-49 PB 001 CONF 00 – AIDS – APU REPORTS – DESCRIPTION AND OPERATIONp. 844
Generalp. 844
Reportsp. 845
Figure 31-37-49-12900-A – APU MES/IDLE Reportp. 866
Figure 31-37-49-13900-A – APU Shutdown Reportp. 867
+31-37-51 – AIDS – STRUCTURE REPORTSp. 868
+31-37-51 PB 001 CONF 00 – AIDS – STRUCTURE REPORTS – DESCRIPTION AND OPERATIONp. 868
Generalp. 868
Load Reportsp. 869
Figure 31-37-51-12800-A – Load Reportp. 895
Figure 31-37-51-12800-B – Load Reportp. 896
+31-37-73 – AIDS – ENGINE REPORTSp. 897
+31-37-73 PB 001 CONF 01 – AIDS – ENGINE REPORTS – DESCRIPTION AND OPERATIONp. 897
Generalp. 897
Reportsp. 898
Figure 31-37-73-12800-A – Engine Cruise Report (Engine Type IAE)p. 1041
Figure 31-37-73-12800-B – Engine Cruise Report (Engine Type IAE)p. 1042
Figure 31-37-73-13500-A – Cruise Performance Report (Engine Type IAE)p. 1043
Figure 31-37-73-13600-A – Take Off Delta EPR Summary (Engine Type IAE)p. 1044
Figure 31-37-73-13600-B – Take Off Delta EPR Summary (Engine Type IAE)p. 1045
Figure 31-37-73-14300-A – Engine Take-Off Report (Engine Type IAE)p. 1046
Figure 31-37-73-15000-A – Engine Report On Request (Engine Type IAE)p. 1047
Figure 31-37-73-15700-A – Engine Gas Path Advisory Report (Engine Type IAE)p. 1049
Figure 31-37-73-16400-A – Engine Mechanical Advisory Report (Engine Type IAE)p. 1051
Figure 31-37-73-17100-A – Engine Divergence Report (Engine Type IAE)p. 1052
Figure 31-37-73-17100-B – Engine Divergence Report (Engine Type IAE)p. 1053
Figure 31-37-73-17800-A – Engine Start Report (Engine Type IAE)p. 1054
Figure 31-37-73-18500-A – Engine Run Up Report (Engine Type IAE)p. 1055
+31-38 – UP AND DOWN DATA LOADING SYSTEM ACQUISITION/INTERFACE AND EQUIPMENTp. 1056
+31-38-00 – UP AND DOWN DATA LOADING SYSTEM ACQUISITION/INTERFACE AND EQUIPMENTp. 1056
+31-38-00 PB 001 CONF 00 – UP AND DOWN DATA LOADING SYSTEM ACQUISITION/INTERFACE AND EQUIPMENT – DESCRIPTION AND OPERATIONp. 1056
System Descriptionp. 1056
Interfacep. 1057
+31-50 – CENTRAL WARNING SYSTEMSp. 1058
+31-50-00 – CENTRAL WARNING SYSTEMSp. 1058
+31-50-00 PB 001 CONF 00 – CENTRAL WARNING SYSTEMS – DESCRIPTION AND OPERATIONp. 1058
Generalp. 1058
Component Locationp. 1059
System Descriptionp. 1061
ECAM Operationp. 1069
Power Supplyp. 1081
Bite Descriptionp. 1083
OEB REMINDER function descriptionp. 1089
Figure 31-50-00-11200-A – ECAM breakdownp. 1092
Figure 31-50-00-12400-A – Component Location in the Cockpitp. 1093
Figure 31-50-00-12500-A – Component Location in the Avionics Compartmentp. 1094
Figure 31-50-00-13900-A – FWS Block Diagramp. 1095
Figure 31-50-00-14000-A – Warning/Caution Interfacep. 1096
Figure 31-50-00-14100-A – Acquisition of the FWCs and SDACsp. 1097
Figure 31-50-00-14900-A – Alert in Case of a System Faultp. 1098
Figure 31-50-00-15300-A – SDAC Architecture – Sheet 1/4p. 1099
Figure 31-50-00-15400-A – SDAC Architecture – Sheet 2/4p. 1100
Figure 31-50-00-15500-A – SDAC Architecture – Sheet 3/4p. 1101
Figure 31-50-00-15600-A – SDAC Architecture – Sheet 4/4p. 1102
Figure 31-50-00-16000-A – FWC – Block Diagram – Sheet 1/3p. 1103
Figure 31-50-00-16100-A – FWC – Block Diagram – Sheet 2/3p. 1104
Figure 31-50-00-16400-A – FWC – Block Diagram – Sheet 3/3p. 1105
Figure 31-50-00-16500-A – FWC Monitorp. 1106
Figure 31-50-00-16900-A – ECAM Control Panelp. 1107
Figure 31-50-00-17600-A – EIS ECAM Inputsp. 1108
Figure 31-50-00-18000-A – Ecam Display Unitsp. 1109
Figure 31-50-00-21300-A – ECAM Display – Normal Operationp. 1110
Figure 31-50-00-21400-A – MEMO Items – Normal Check Listp. 1111
Figure 31-50-00-21800-A – ECAM Display with A/C Faultp. 1112
Figure 31-50-00-22000-A – Corrective Action Carried by the Crewp. 1113
Figure 31-50-00-22100-A – Action on Either CLR and Resultp. 1114
Figure 31-50-00-22200-A – 2nd Action on Either CLR and Resultp. 1115
Figure 31-50-00-22300-A – 3rd Action on Either CLR and Resultp. 1116
Figure 31-50-00-22400-A – Example of Message Overflowp. 1117
Figure 31-50-00-22500-A – ECAM Message – Double A/C System Failurep. 1118
Figure 31-50-00-22700-A – STATUS Page Examplep. 1119
Figure 31-50-00-23900-A – Main Electrical Power Supply of FWS Componentsp. 1120
Figure 31-50-00-25900-A – ECAM-1 Pagep. 1121
Figure 31-50-00-26100-A – ECAM-1/LAST LEG REPORTp. 1122
Figure 31-50-00-26300-A – ECAM-1/PREVIOUS LEGS REPORTp. 1123
Figure 31-50-00-26500-A – ECAM-1/LRU IDENTIFICATIONp. 1124
Figure 31-50-00-26700-A – ECAM-1/GROUND SCANNINGp. 1125
Figure 31-50-00-26900-A – ECAM-1/CLASS 3 FAULTSp. 1126
Figure 31-50-00-27100-A – ECAM-1/TROUBLE SHOOTING DATAp. 1127
Figure 31-50-00-27300-A – ECAM-1/ECAM PIN PROGRAM SOFT Pages (FWC P/N 350E053020606)p. 1128
Figure 31-50-00-27400-A – ECAM-1/ECAM PIN PROGRAM SOFT Pages (FWC P/N 350E053020707 or 350E053020808)p. 1129
Figure 31-50-00-27500-A – ECAM-1/ECAM PIN PROGRAM HARD Pages (SDACs in Basic Mode and FWC P/N 350E017271616 or 350E053020202)p. 1131
Figure 31-50-00-27600-A – ECAM-1/ECAM PIN PROGRAM HARD Pages (SDACs in Basic Mode and FWC P/N 350E018312020 or 350E053020303)p. 1132
Figure 31-50-00-27700-A – ECAM-1/ECAM PIN PROGRAM HARD Pages (SDACs in Basic Mode and FWC P/N 350E053020404)p. 1133
Figure 31-50-00-27800-A – ECAM-1/ECAM PIN PROGRAM HARD Pages (SDACs in Basic Mode and FWC P/N 350E053020606, 350E053020707 or 350E053020808)p. 1134
Figure 31-50-00-27900-A – ECAM-1/ECAM PIN PROGRAM HARD Pages (SDACs in Full Mode and FWC P/N 350E017271616 or 350E053020202)p. 1135
Figure 31-50-00-28000-A – ECAM-1/ECAM PIN PROGRAM HARD Pages (SDACs in Full Mode and FWC P/N 350E018312020 or 350E053020303)p. 1136
Figure 31-50-00-28100-A – ECAM-1/ECAM PIN PROGRAM HARD Pages (SDACs in Full Mode and FWC P/N 350E053020404)p. 1137
Figure 31-50-00-28200-A – ECAM-1/ECAM PIN PROGRAM HARD Pages (SDACs in Full Mode and FWC P/N 350E053020606)p. 1138
Figure 31-50-00-28300-A – ECAM-1/ECAM PIN PROGRAM HARD Pages (SDACs in Full Mode and FWC P/N 350E053020707, 350E053020808 or 350E053020909)p. 1139
Figure 31-50-00-30400-A – ECAM-1/OEB DATABASE/LIST FWC1 and LIST FWC2p. 1140
Figure 31-50-00-30800-A – ECAM-1/OEB DATABASE UPDATEp. 1142
Figure 31-50-00-31000-A – ECAM-1/OEB DATABASE UPDATE/CREATEp. 1143
Figure 31-50-00-31200-A – ECAM-1/OEB DATABASE UPDATE/DELETEp. 1144
Figure 31-50-00-31400-A – ECAM-1/OEB DATABASE UPDATE/VERSIONp. 1145
Figure 31-50-00-31600-A – ECAM-1/OEB DATABASE UPDATE/CROSSLOADp. 1146
+31-50-00 PB 501 CONF 00 – CENTRAL WARNING SYSTEMS – ADJUSTMENT/TESTp. 1147
31-50-00-710-001-A – Ground Scanning of the Central Warning Systemp. 1147
31-50-00-710-002-A – Operational Test of the Flight Warning Computer (FWC)p. 1149
31-50-00-710-003-A – Operational Test of the System Data Acquisition Concentrator (SDAC)p. 1152
31-50-00-710-004-A – Operational Test of the ECAM Control Panelp. 1155
31-50-00-710-005-A – Operational Test of the Circuit Breaker Monitoring Systemp. 1158
+31-50-00-740-002-A – Read and Decode the Hardware Pin Programming of the SDAC and FWCp. 1162
Figure 31-50-00-991-00500-A – ECAM-1/ECAM PIN PROGRAM HARDWARE Pages (SDACs in Basic Mode and FWC P/N: 350E017271616 or 350E053020202)p. 1183
Figure 31-50-00-991-00300-B – Table of the SDAC Hardware Pin Programming Datap. 1184
Figure 31-50-00-991-00300-A – Table of the SDAC Hardware Pin Programming Datap. 1185
Figure 31-50-00-991-00400-A – Table of the FWC Hardware Pin Programming Datap. 1186
Figure 31-50-00-991-00600-A – ECAM-1/ECAM PIN PROGRAM HARDWARE Pages (SDACs in Basic Mode and FWC P/N: 350E018312020 or 350E053020303)p. 1187
Figure 31-50-00-991-00700-A – ECAM-1/ECAM PIN PROGRAM HARDWARE Pages (SDACs in Basic Mode and FWC P/N: 350E053020404)p. 1188
Figure 31-50-00-991-00800-A – ECAM-1/ECAM PIN PROGRAM HARDWARE Pages (SDACs in Basic Mode and FWC P/N: 350E053020606, 350E053020707 or 350E053020808)p. 1189
Figure 31-50-00-991-00900-A – ECAM-1/ECAM PIN PROGRAM HARDWARE Pages (SDACs in Full Mode and FWC P/N: 350E017271616 or 350E053020202)p. 1190
Figure 31-50-00-991-01000-A – ECAM-1/ECAM PIN PROGRAM HARDWARE Pages (SDACs in Full Mode and FWC P/N: 350E018312020 or 350E053020303)p. 1191
Figure 31-50-00-991-01100-A – ECAM-1/ECAM PIN PROGRAM HARDWARE Pages (SDACs in Full Mode and FWC P/N: 350E053020404)p. 1192
Figure 31-50-00-991-01300-A – ECAM-1/ECAM PIN PROGRAM HARDWARE Pages (SDACs in Full Mode and FWC P/N: 350E053020707 or 350E053020808)p. 1193
Figure 31-50-00-991-01200-A – ECAM-1/ECAM PIN PROGRAM HARDWARE Pages (SDACs in Full Mode and FWC P/N: 350E053020606)p. 1194
+31-50-00-740-003-A – Read FWC Software Pin Programmingp. 1195
Figure 31-50-00-991-00200-B – Table of the FWC Software Pin Programming Datap. 1198
Figure 31-50-00-991-00200-A – Table of the FWC Software Pin Programming Datap. 1201
31-50-00-710-009-A – Operational Test of the Automatic Call Out with the Radio Altimeter Simulatorp. 1204
31-50-00-710-011-A – Operational Test of the MASTER CAUT and MASTER WARN lightsp. 1207
+31-51 – OPERATIONAL PRESENTATIONp. 1210
+31-51-00 – OPERATIONAL PRESENTATIONp. 1210
+31-51-00 PB 001 CONF 00 – OPERATIONAL PRESENTATION – DESCRIPTION AND OPERATIONp. 1210
Generalp. 1210
Message Presentationp. 1211
List of Maintenance Items in Statusp. 1213
Symbology Used in the Operational Presentationp. 1214
Figure 31-51-00-12900-A – Message Presentationp. 1215
Figure 31-51-00-13000-A – Upper and Lower ECAM Display Unit – Sectionsp. 1216
Figure 31-51-00-13100-A – Lower ECAM Display Unit – Sectionsp. 1217
+31-51-00 PB 301 CONF 00 – OPERATIONAL PRESENTATION – SERVICINGp. 1218
31-51-00-610-001-A – Load OEB REMINDER Data into FWCs using MCDUs.p. 1218
31-51-00-610-002-A – Delete OEB REMINDER Data from FWCs using MCDUs.p. 1224
31-51-00-610-003-A – Crossload OEB REMINDER Data into FWCs using MCDUs.p. 1231
31-51-00-210-001-A – Read OEB REMINDER Data in the FWC1 and/or the FWC2.p. 1236
+31-52 – FWC – ACQUISITION/INTERFACEp. 1239
+31-52-00 – FWC – ACQUISITION/INTERFACEp. 1239
+31-52-00 PB 001 CONF 01 – FWC – ACQUISITION/INTERFACE – DESCRIPTION AND OPERATIONp. 1239
Generalp. 1239
Signal Typesp. 1240
Interface Tablesp. 1242
+31-53 – FLIGHT WARNING COMPUTER (FWC)p. 1243
+31-53-21 – LOUD SPEAKERp. 1243
+31-53-21 PB 401 CONF 00 – LOUD SPEAKER – REMOVAL/INSTALLATIONp. 1243
+31-53-21-000-001-A – Removal of the Loudspeakersp. 1243
Figure 31-53-21-991-00100-A – Loudspeakerp. 1245
31-53-21-400-001-A – Installation of the Loudspeakersp. 1246
+31-53-34 – COMPUTER – FLIGHT WARNING (FWC)p. 1248
+31-53-34 PB 401 CONF 00 – COMPUTER – FLIGHT WARNING (FWC) – REMOVAL/INSTALLATIONp. 1248
+31-53-34-000-001-A – Removal of the Flight Warning Computer (FWC)p. 1248
Figure 31-53-34-991-00100-A – Flight Warning Computer (FWC)p. 1250
31-53-34-400-001-A – Installation of the Flight Warning Computer (FWC)p. 1251
+31-54 – SDAC – ACQUISITION/INTERFACEp. 1255
+31-54-00 – SDAC – ACQUISITION/INTERFACEp. 1255
+31-54-00 PB 001 CONF 01 – SDAC – ACQUISITION/INTERFACE – DESCRIPTION AND OPERATIONp. 1255
Generalp. 1255
Signal Typep. 1256
Interfacep. 1259
+31-55 – SYSTEM DATA ACQUISITION CONCENTRATOR (SDAC)p. 1260
+31-55-34 – CONCENTRATOR – SYSTEM DATA ACQUISITION (SDAC)p. 1260
+31-55-34 PB 401 CONF 00 – CONCENTRATOR – SYSTEM DATA ACQUISITION (SDAC) – REMOVAL/INSTALLATIONp. 1260
+31-55-34-000-001-A – Removal of the SDACp. 1260
Figure 31-55-34-991-00100-A – System Data Acquisition Concentrator (SDAC)p. 1262
31-55-34-400-001-A – Installation of the SDACp. 1263
+31-56 – ECAM CONTROL PANELp. 1266
+31-56-00 – ECAM CONTROL PANELp. 1266
+31-56-00 PB 001 CONF 00 – ECAM CONTROL PANEL – DESCRIPTION AND OPERATIONp. 1266
Generalp. 1266
Functional Descriptionp. 1267
ECP ARINCp. 1269
Figure 31-56-00-11200-A – ECAM Control Panelp. 1276
Figure 31-56-00-11300-A – ECAM Control Panel – Electrical Definitionp. 1277
Figure 31-56-00-13800-A – ECP – Power Supplyp. 1278
+31-60 – ELECTRONIC INSTRUMENT SYSTEM (EIS)p. 1279
+31-60-00 – ELECTRONIC INSTRUMENT SYSTEM (EIS)p. 1279
+31-60-00 PB 001 CONF 00 – ELECTRONIC INSTRUMENT SYSTEM (EIS) – DESCRIPTION AND OPERATIONp. 1279
Generalp. 1279
Component Locationp. 1282
Power Supplyp. 1283
Component Descriptiop. 1284
Eis Operationp. 1288
Operation in Case of Failurp. 1304
Testp. 1313
Figure 31-60-00-14800-B – Component Location in the Cockpitp. 1315
Figure 31-60-00-23600-C – PFD in Approach with FPV and PFDp. 1316
Figure 31-60-00-29900-A – WHEEL Pagep. 1317
Figure 31-60-00-36200-A – Presentation by Display Units in Normal Configurationp. 1318
Figure 31-60-00-36300-A – ND in ROSE-ILS Modep. 1319
Figure 31-60-00-36400-A – Component Location in the Cockpitp. 1320
Figure 31-60-00-36500-A – ND in ROSE-VOR Modep. 1321
Figure 31-60-00-36600-A – ND in ROSE-NAV Modep. 1322
Figure 31-60-00-36700-A – ND – Weather Radar in ARC Modep. 1323
Figure 31-60-00-36800-A – PFD and ND Imagep. 1324
Figure 31-60-00-36900-A – Avionics Compartment – EISp. 1325
Figure 31-60-00-37000-A – ND in ARC Mode – Typical En Route Flight Planp. 1326
Figure 31-60-00-37100-A – Automatic Advisory Modep. 1327
Figure 31-60-00-37200-B – Main Electrical Power Supply of the EIS Componentsp. 1328
Figure 31-60-00-37300-A – ND in ARC mode – AP/FD in TRACK mode – A/C off the Flight Planp. 1329
Figure 31-60-00-37400-A – Automatic Mode Related to the Flight Phasep. 1330
Figure 31-60-00-37600-B – ENGINE Page – Running Modep. 1331
Figure 31-60-00-37700-C – Display Unit – Typical Imagep. 1332
Figure 31-60-00-37800-A – ND in ARC Mode – Takeoff Examplep. 1333
Figure 31-60-00-37900-A – ND in ARC Mode – VOR/FMGC Discrepancy Messagep. 1334
Figure 31-60-00-38000-B – DMC Output Bus – Attitude Comparisonp. 1335
Figure 31-60-00-38200-A – ND in Plan Modep. 1336
Figure 31-60-00-38300-B – FCU – AFS & EFIS Controlp. 1337
Figure 31-60-00-38500-A – ND – Weather Radar Image in ARC and ROSE Modep. 1338
Figure 31-60-00-38600-A – EFIS Control Sectionp. 1339
Figure 31-60-00-38800-C – Engine Parameters Displayp. 1340
Figure 31-60-00-39000-D – FUEL Pagep. 1341
Figure 31-60-00-39100-A – ECAM CP – EIS DMC SWITCHING Panelp. 1342
Figure 31-60-00-39200-A – HYD Pagep. 1343
Figure 31-60-00-39300-A – EFIS – ECAM Reconfiguration Capabilityp. 1344
Figure 31-60-00-39400-A – ECAM Reconfiguration Between DMC's and Between DUsp. 1345
Figure 31-60-00-39500-A – AIR BLEED Pagep. 1346
Figure 31-60-00-39600-A – CFDIU to EFIS/ECAM Interfacep. 1347
Figure 31-60-00-39700-D – DOOR/OXY Pagep. 1348
Figure 31-60-00-39800-A – CFDS Menu Access to BITEp. 1349
Figure 31-60-00-40000-B – ECAM / EFIS Acquisitionp. 1350
Figure 31-60-00-40100-C – PFD/ND Brightness – ON/OFF Control PFD/ND Transferp. 1351
Figure 31-60-00-40200-A – APU Pagep. 1352
Figure 31-60-00-40500-B – PFD – Typical Displayp. 1353
Figure 31-60-00-40600-A – ELEC Pagep. 1354
Figure 31-60-00-40800-Z – Ecam Display Unitsp. 1355
Figure 31-60-00-40900-B – TCAS Indicationsp. 1356
Figure 31-60-00-41000-A – TCAS Messagep. 1357
Figure 31-60-00-41100-A – AIR COND Pagep. 1358
Figure 31-60-00-41200-B – TCAS Indicationsp. 1359
Figure 31-60-00-41300-A – TCAS Messagesp. 1360
Figure 31-60-00-41400-A – CAB PRESS Pagep. 1361
Figure 31-60-00-41500-C – ND – TERRAIN Displayp. 1362
Figure 31-60-00-41700-C – CRUISE Pagep. 1363
Figure 31-60-00-41800-A – EIS Block Diagramp. 1364
Figure 31-60-00-42000-B – AIR COND Pagep. 1365
Figure 31-60-00-42100-A – F/CTL Pagep. 1366
+31-60-00 PB 201 CONF 00 – ELECTRONIC INSTRUMENT SYSTEM (EIS) – MAINTENANCE PRACTICESp. 1367
31-60-00-860-001-A – EIS Start Procedurep. 1367
31-60-00-860-002-A – EIS Stop Procedurep. 1370
+31-60-00 PB 501 CONF 00 – ELECTRONIC INSTRUMENT SYSTEM (EIS) – ADJUSTMENT/TESTp. 1371
31-60-00-710-001-A – Operational Test of the EISp. 1371
31-60-00-710-002-A – Operational Test of EFIS/ECAM Switching Functionsp. 1374
31-60-00-710-003-A – PFD/ND/Upper and Lower ECAM Display Units (DU) – Brightnessp. 1379
31-60-00-740-002-A – Perform Electronic Instrument System (EIS) Input Testp. 1382
31-60-00-740-004-A – EIS System Testp. 1386
+31-61 – EIS – CONTROLp. 1389
+31-61-00 – EIS – CONTROLp. 1389
+31-61-00 PB 001 CONF 00 – EIS – CONTROL – DESCRIPTION AND OPERATIONp. 1389
Generalp. 1389
EIS Component Locationp. 1390
EIS Controlsp. 1392
Figure 31-61-00-12600-E – EIS – Component Location in the Cockpit – Sheet 1/2p. 1395
Figure 31-61-00-12800-A – EIS – Component Location in the Cockpit – Sheet 2/2p. 1396
Figure 31-61-00-13000-A – EIS – Component Location in the Avionics Compartmentp. 1397
Figure 31-61-00-13100-A – EIS – Location of CAPT and F/O PFD-ND XFR Relay Boxesp. 1398
Figure 31-61-00-15100-A – Wiring Diagram Between DUs and Brightness ON/OFF Potentiometersp. 1399
Figure 31-61-00-15500-A – ECAM CTL PNL and SWITCHING Panelp. 1400
Figure 31-61-00-15600-A – Wiring Diagram for the DMCs and Transfer Selector Switch Interfacep. 1401
Figure 31-61-00-16300-B – FCU – Auto Flight and EFIS Controlp. 1402
Figure 31-61-00-16400-A – PFD Control Partp. 1403
Figure 31-61-00-16500-A – ND Control Partp. 1404
Figure 31-61-00-17700-A – Wiring Diagram for the DUs – Activation of Warning Flag Pattern on the Groundp. 1405
Figure 31-61-00-17800-A – Warning, Flag Patterns During Cockpit Light Test on the Ground (EFIS part)p. 1406
Figure 31-61-00-18000-B – Warning, Flag Patterns During Cockpit Light Test on the Ground (ECAM part)p. 1407
+31-61-12 – CONTROL PANEL – ECAMp. 1408
+31-61-12 PB 401 CONF 00 – CONTROL PANEL – ECAM – REMOVAL/INSTALLATIONp. 1408
+31-61-12-000-001-A – Removal of the ECAM Control Panelp. 1408
Figure 31-61-12-991-00100-A – ECAM Control Panelp. 1409
31-61-12-400-001-A – Installation of the ECAM Control Panelp. 1410
+31-62 – DMC – ACQUISITION/INTERFACEp. 1412
+31-62-00 – DMC – ACQUISITION/INTERFACEp. 1412
+31-62-00 PB 001 CONF 00 – DMC – ACQUISITION/INTERFACE – DESCRIPTION AND OPERATIONp. 1412
Generalp. 1412
System Descriptionp. 1413
Interfacep. 1417
Figure 31-62-00-12500-A – Signal Flow from A/C Systems to the EISp. 1467
Figure 31-62-00-13400-B – DMCs Output Busesp. 1468
+31-63 – DISPLAY MANAGEMENT COMPUTER (DMC)p. 1469
+31-63-00 – DISPLAY MANAGEMENT COMPUTER (DMC)p. 1469
+31-63-00 PB 001 CONF 00 – DISPLAY MANAGEMENT COMPUTER (DMC) – DESCRIPTION AND OPERATIONp. 1469
Generalp. 1469
Component locationp. 1470
System Descriptionp. 1471
Interfacep. 1472
Component Descriptionp. 1473
Figure 31-63-00-11200-A – Overall Architecturep. 1496
Figure 31-63-00-12400-A – DMC – Component Locationp. 1497
Figure 31-63-00-14200-A – CRT – Block Diagramp. 1498
Figure 31-63-00-16800-A – EIS Configurationp. 1499
Figure 31-63-00-16900-A – DMC – Data Flowp. 1500
Figure 31-63-00-17000-A – DMC – Block Diagramp. 1501
Figure 31-63-00-17200-A – DPU Board – Block Diagramp. 1502
Figure 31-63-00-17300-A – I/O Interface Board – Block Diagramp. 1503
Figure 31-63-00-17400-A – Weather Radar Serial Input Wordp. 1504
Figure 31-63-00-17500-A – WXR Board – Block Diagramp. 1505
Figure 31-63-00-17600-A – Conversion of Manchester Bits to TTL-Levelsp. 1506
Figure 31-63-00-17700-A – Manchester Decoderp. 1507
Figure 31-63-00-17800-A – Conversion of Manchester Bits to NRZ Bitsp. 1508
Figure 31-63-00-17900-A – Examples of Valid and Invalid NRZ Bitsp. 1509
Figure 31-63-00-18000-A – Writing Maskp. 1510
Figure 31-63-00-18100-A – Master Beam and Slave Beamp. 1511
Figure 31-63-00-18200-A – Timing Diagram for Beam Processingp. 1512
Figure 31-63-00-18300-A – Switching Power Supply – Basic Configurationp. 1513
Figure 31-63-00-18900-A – CRT – Analog Board – Block Diagramp. 1514
Figure 31-63-00-19100-A – Symbol Generator – Block Diagramp. 1515
Figure 31-63-00-19200-A – Mask Circuit – Block Diagramp. 1516
Figure 31-63-00-19300-A – Color Circuit Block Diagramp. 1517
Figure 31-63-00-19400-A – WXR Link Receiver – Block Diagramp. 1518
Figure 31-63-00-19700-A – Low Voltage Power Supply – Block Diagramp. 1519
+31-63-00 PB 401 CONF 00 – DISPLAY MANAGEMENT COMPUTER (DMC) – DEACTIVATION/REACTIVATIONp. 1520
31-63-00-040-001-A – Deactivation of the DMCp. 1520
31-63-00-440-001-A – Reactivation of the DMC (Installation of the DMC3 in its initial position)p. 1522
+31-63-22 – DISPLAY UNITp. 1524
+31-63-22 PB 401 CONF 00 – DISPLAY UNIT – REMOVAL/INSTALLATIONp. 1524
+31-63-22-000-001-A – Removal of the Display Unitp. 1524
Figure 31-63-22-991-00100-A – Display Unit.p. 1526
31-63-22-400-001-A – Installation of the Display Unitp. 1527
31-63-22-400-002-A – Display Units Swapping procedurep. 1530
+31-63-22 PB 601 CONF 00 – DISPLAY UNIT – INSPECTION/CHECKp. 1537
+31-63-22-200-001-A – Measurement of the Display Unit Brightnessp. 1537
Figure 31-63-22-991-00200-A – Brightness Measurement Chartp. 1542
+31-63-22 PB 701 CONF 00 – DISPLAY UNIT – CLEANING/PAINTINGp. 1543
31-63-22-100-001-A – Cleaning of the Display Unitp. 1543
+31-63-34 – COMPUTER – DISPLAY MANAGEMENT (DMC)p. 1545
+31-63-34 PB 401 CONF 00 – COMPUTER – DISPLAY MANAGEMENT (DMC) – REMOVAL/INSTALLATIONp. 1545
+31-63-34-000-001-A – Removal of the DMCp. 1545
Figure 31-63-34-991-00100-A – DMCp. 1547
31-63-34-400-001-A – Installation of the DMCp. 1548
+31-64 – PRIMARY FLIGHT DISPLAY (PFD)p. 1550
+31-64-00 – PRIMARY FLIGHT DISPLAY (PFD)p. 1550
+31-64-00 PB 001 CONF 00 – PRIMARY FLIGHT DISPLAY (PFD) – DESCRIPTION AND OPERATIONp. 1550
Generalp. 1550
Component Locationp. 1551
System Descriptionp. 1552
EIS Acquisition and Wiringp. 1588
Figure 31-64-00-14800-A – PFD – Zonesp. 1591
Figure 31-64-00-15000-A – PFD – Aircraft Attitude Displayp. 1592
Figure 31-64-00-15100-A – PFD – Pitch Scalep. 1593
Figure 31-64-00-15300-A – PFD – Sectorsp. 1594
Figure 31-64-00-15500-A – PFD – Rising Runway,Lateral Acceleration and FD Bars Parametersp. 1595
Figure 31-64-00-15900-A – PFD – Attitude Failure Displayp. 1597
Figure 31-64-00-16200-A – PFD – Slip Indicationp. 1598
Figure 31-64-00-16500-B – PFD – Guidance Selectionp. 1599
Figure 31-64-00-16800-A – PFD – FD Displayp. 1600
Figure 31-64-00-17200-A – PFD – Flight Path Presentation and Parametersp. 1601
Figure 31-64-00-17400-A – PFD – FD and FPV Failure Displayp. 1603
Figure 31-64-00-18000-A – PFD – Yaw, FD, Radio Alt, Roll and Pitch Angle Parametersp. 1604
Figure 31-64-00-18300-A – PFD – Excessive Attitude Displayp. 1606
Figure 31-64-00-18700-A – PFD – Attitude Discrepancyp. 1607
Figure 31-64-00-18900-B – PFD – Reactive windshear alertp. 1608
Figure 31-64-00-20400-A – PFD – Radio Altitude Indicationp. 1609
Figure 31-64-00-21100-A – PFD – Heading Presentationp. 1611
Figure 31-64-00-21300-B – PFD – Selections and Figurationsp. 1612
Figure 31-64-00-22400-B – PFD – Altitude Presentationp. 1614
Figure 31-64-00-22600-D – PFD – Altitude Indications Displayp. 1615
Figure 31-64-00-22900-D – PFD – Altitude Selected Displayp. 1617
Figure 31-64-00-23400-D – PFD – Altitude Setting Referencep. 1618
Figure 31-64-00-23500-A – PFD – Landing elevation symbolp. 1619
Figure 31-64-00-23800-B – PFD – Other Altitude Indicationsp. 1620
Figure 31-64-00-25400-C – PFD – Airspeed Presentationp. 1621
Figure 31-64-00-25600-A – PFD – Vc Indication Displayp. 1622
Figure 31-64-00-25900-A – PFD – Selected Speed Displayp. 1623
Figure 31-64-00-26400-A – PFD – V1 Displayp. 1624
Figure 31-64-00-26600-C – PFD – Mach Number Displayp. 1625
Figure 31-64-00-27700-C – PFD – Limit Speed Indication Displayp. 1626
Figure 31-64-00-28000-A – PFD – Airspeed Failure Indicationsp. 1628
Figure 31-64-00-29400-A – PFD – Vertical Speed Presentationp. 1629
Figure 31-64-00-29600-A – PFD – Vertical Speed Displayp. 1630
Figure 31-64-00-29800-A – PFD – Examples of Vertical Speed Displayp. 1631
Figure 31-64-00-30400-A – PFD – Particular Vertical Speeds Displaysp. 1632
Figure 31-64-00-30500-A – PFD – Vertical Speed Parametersp. 1633
Figure 31-64-00-30800-B – PFD – TCAS Indications – Preventive Resolution Advisoriesp. 1634
Figure 31-64-00-31000-B – PFD – TCAS Indications – Corrective Resolution Advisoriesp. 1635
Figure 31-64-00-31600-B – PFD – TCAS Indicationsp. 1636
Figure 31-64-00-31800-A – PFD – TCAS Failure Messagep. 1637
Figure 31-64-00-31900-B – PFD – TCAS Flag Indicationp. 1638
Figure 31-64-00-32100-A – PFD – Flight Mode Annunciator Presentationp. 1639
Figure 31-64-00-32300-B – PFD – FMA Zonesp. 1640
Figure 31-64-00-35800-A – PFD – ILS Approach Displayp. 1641
Figure 31-64-00-36600-A – PFD – Marker Indicationsp. 1642
Figure 31-64-00-37800-A – PFD – Non Precision Approach Displayp. 1643
Figure 31-64-00-38600-B – PFD – V/DEV flagp. 1644
Figure 31-64-00-38700-A – PFD – Failure Indicationp. 1645
Figure 31-64-00-38900-A – PFD – ILS Guidance and V/DEV Parametersp. 1646
Figure 31-64-00-39900-A – PFD – Simplified symbologyp. 1647
Figure 31-64-00-41200-A – EIS Acquisitionsp. 1648
Figure 31-64-00-41300-A – EIS Acquisitions : FMGCp. 1649
Figure 31-64-00-41500-A – FMGCs EIS – DMCs Wiring Interfacep. 1650
Figure 31-64-00-42100-A – EIS Acquisitions : ADIRU (IR)p. 1651
Figure 31-64-00-42200-A – EIS Acquisitions : ADIRU (ADR)p. 1652
Figure 31-64-00-42300-A – EIS Acquisitions : FACp. 1653
Figure 31-64-00-42400-A – EIS Acquisitions : ILSp. 1654
Figure 31-64-00-42500-A – EIS Acquisitions : RA (Radio Altimeter)p. 1655
Figure 31-64-00-42600-A – EIS Acquisitions : FCUp. 1656
Figure 31-64-00-42700-A – EIS Acquisitions : VORp. 1657
Figure 31-64-00-42800-A – EIS Acquisitions : DMEp. 1658
Figure 31-64-00-42900-A – Interface with TCASp. 1659
Figure 31-64-00-45900-B – PFD – Component Locationp. 1660
Figure 31-64-00-46000-B – PFD – VR Displayp. 1661
Figure 31-64-00-46100-B – PFD – Back Course title on ILS scalep. 1662
+31-65 – NAVIGATION DISPLAY (ND)p. 1663
+31-65-00 – NAVIGATION DISPLAY (ND)p. 1663
+31-65-00 PB 001 CONF 00 – NAVIGATION DISPLAY (ND) – DESCRIPTION AND OPERATIONp. 1663
Generalp. 1663
Component locationp. 1664
ND Figurationsp. 1668
Interface between the DMCs and the NAV Sensors and AFS Computers for the NDp. 1697
Flags Testp. 1709
Figure 31-65-00-39000-C – Navigation Display – EIS Component Locationp. 1710
Figure 31-65-00-39200-E – Navigation Display-EFIS Acquisitionsp. 1711
Figure 31-65-00-39400-A – Navigation Display Normal Imagep. 1712
Figure 31-65-00-39600-A – Navigation Display ROSE VOR Mode (HDG Mode)p. 1713
Figure 31-65-00-39800-A – Navigation Display-ROSE NAV Modep. 1714
Figure 31-65-00-40000-A – Navigation Display – ROSE Mode ILSp. 1715
Figure 31-65-00-40200-A – Navigation Display – ARC Modep. 1716
Figure 31-65-00-40400-A – Navigation Display – PLAN Modep. 1717
Figure 31-65-00-40600-A – Navigation Display-HDG Flagp. 1718
Figure 31-65-00-40800-A – Navigation Display-CHECK HDG Flagp. 1719
Figure 31-65-00-41000-A – Navigation Display – Speed, Wind, NCDp. 1720
Figure 31-65-00-41100-A – Navigation Display – PFD/ND Controlp. 1721
Figure 31-65-00-41200-A – Navigation Display – MCDU RADIO NAV Pagep. 1722
Figure 31-65-00-41400-A – Navigation Display – Features of Selected Navaidsp. 1723
Figure 31-65-00-41600-A – Navigation Display – VOR (or ADF) Bearing and Frequencyp. 1724
Figure 31-65-00-41800-A – Navigation Display – VOR and ADF Flagsp. 1725
Figure 31-65-00-42000-A – Navigation Display – ROSE VOR Modep. 1726
Figure 31-65-00-42200-A – Navigation Display – LOC and G/S Deviation in NCDp. 1727
Figure 31-65-00-42400-A – Navigation Display – ILS Station Selection in ROSE NAV Modep. 1728
Figure 31-65-00-42600-B – ND – Back Course title in ROSE ILS modep. 1729
Figure 31-65-00-42700-A – Navigation Display – Chrono Indicationp. 1730
Figure 31-65-00-42900-A – Navigation Display – Example of Mask in Arc Modep. 1731
Figure 31-65-00-43100-A – Navigation Display – Flight Plansp. 1732
Figure 31-65-00-43200-A – Navigation Display – Flight Plan Capturep. 1733
Figure 31-65-00-43400-A – Navigation Display – Basic Navaidsp. 1734
Figure 31-65-00-43500-A – Navigation Display – GPS Primary Functionp. 1735
Figure 31-65-00-43700-A – Navigation Display – Symbol Displayp. 1736
Figure 31-65-00-43800-A – Navigation Display – Symbol Display-Sheet 1/2p. 1738
Figure 31-65-00-43900-B – ND – Symbol Displayp. 1739
Figure 31-65-00-44000-A – ND – TCAS Indicationsp. 1740
Figure 31-65-00-44100-B – ND – TCAS Indicationsp. 1741
Figure 31-65-00-44200-B – ND – TCAS Symbologyp. 1742
Figure 31-65-00-44400-A – ND – TCAS Off Scale Intrudersp. 1743
Figure 31-65-00-44500-A – ND – TCAS Displayp. 1744
Figure 31-65-00-44600-AM – ND – TCAS Testp. 1745
Figure 31-65-00-44700-B – ND – TCAS Testp. 1746
Figure 31-65-00-44900-A – ND – TCAS Messagesp. 1747
Figure 31-65-00-45100-A – ND – TCAS Messagesp. 1748
Figure 31-65-00-45200-A – ND – TCAS Fault Messages/Flagsp. 1749
Figure 31-65-00-45400-A – Navigation Display-Messagesp. 1750
Figure 31-65-00-45600-A – Navigation Display – Weather Radar Imagep. 1751
Figure 31-65-00-45800-A – Navigation Display – Interface with ADIRU (IRS/ADC)p. 1752
Figure 31-65-00-45900-A – Navigation Display – Interface with FMGCp. 1753
Figure 31-65-00-46000-A – Navigation Display – Interface with FCUp. 1754
Figure 31-65-00-46100-B – Navigation Display – Interface with ADFp. 1755
Figure 31-65-00-46300-A – Navigation Display – Interface with VORp. 1756
Figure 31-65-00-46400-A – Navigation Display – Interface with DMEp. 1757
Figure 31-65-00-46500-A – Navigation Display – Interface with TCASp. 1758
Figure 31-65-00-46600-A – Navigation Display – Interface with ILSp. 1759
Figure 31-65-00-46800-A – Navigation Display – Flags Test Imagep. 1760
Figure 31-65-00-47300-C – ND – TERRAIN Displayp. 1761
+31-66 – ECAM ENGINE/WARNING DISPLAYp. 1762
+31-66-00 – ECAM ENGINE/WARNING DISPLAYp. 1762
+31-66-00 PB 001 CONF 13 – ECAM ENGINE/WARNING DISPLAY – DESCRIPTION AND OPERATIONp. 1762
Generalp. 1762
Component Locationp. 1763
Display Partitioningp. 1764
Primary Engine Parametersp. 1765
Primary Engine Parameters Descriptionp. 1766
Fuel on Board Informationp. 1770
Engine Typesp. 1771
Engine 1 Parameters Definitionp. 1772
Engine 2 Parameters Definitionp. 1773
Engine 1 & 2 Other Parametersp. 1775
Messages Related to Engine Ratingp. 1777
Slats and Flaps Indicationp. 1778
Warning and Memo Sectionp. 1781
Acquisition and Wiringp. 1782
Figure 31-66-00-12400-A – Upper Display Unit / ECAM Control Locationp. 1783
Figure 31-66-00-13600-A – Upper Display Unit Partitioningp. 1784
Figure 31-66-00-14800-A – Engine Parameters Presentationp. 1785
Figure 31-66-00-21000-A – EPR LIM Mode Selection and Displayp. 1786
Figure 31-66-00-21400-A – Reverse and Failure Indicationp. 1787
Figure 31-66-00-21500-A – Engine Relightp. 1788
Figure 31-66-00-22700-A – Fuel on Board and Half Box Indicationp. 1789
Figure 31-66-00-25000-A – Engine 1 & 2 Parametersp. 1790
Figure 31-66-00-27300-A – Engine 1 & 2 Other Parametersp. 1791
Figure 31-66-00-31700-A – Flaps and Slats Position Indicationp. 1792
Figure 31-66-00-31800-A – Flap and Slat Extensionp. 1793
Figure 31-66-00-31900-A – Flap and Slat Retractionp. 1794
Figure 31-66-00-32000-A – Flap and Slat Abnormal Operationp. 1795
Figure 31-66-00-32100-A – Flap and Slat Position and Selectionp. 1796
Figure 31-66-00-32200-A – Flap and Slat Indication / Memo Sectionp. 1797
Figure 31-66-00-35200-A – Display Unit Lower Section Assignmentp. 1798
Figure 31-66-00-35300-A – STS, ADV and Overflow Indicationp. 1799
Figure 31-66-00-37000-A – FADEC Links (Engine 1)p. 1800
Figure 31-66-00-37400-A – FADEC Links (Engine 2)p. 1801
Figure 31-66-00-37800-A – Fuel Quantity Indicator Linksp. 1802
Figure 31-66-00-37900-A – SDAC Linksp. 1803
Figure 31-66-00-38000-A – FWC Message Linksp. 1804
+31-67 – ECAM SYSTEM/STATUS DISPLAYp. 1805
+31-67-00 – ECAM SYSTEM/STATUS DISPLAYp. 1805
+31-67-00 PB 001 CONF 00 – ECAM SYSTEM/STATUS DISPLAY – DESCRIPTION AND OPERATIONp. 1805
Generalp. 1805
Component Locationp. 1806
System Descriptionp. 1807
Figure 31-67-00-23000-A – SD – Component Locationp. 1816
Figure 31-67-00-23200-A – SD – Display Areasp. 1817
Figure 31-67-00-23300-A – Definition of the Flight Phasesp. 1818
Figure 31-67-00-23500-C – SD – Cruise Pagep. 1819
Figure 31-67-00-23700-A – SD – CAB PRESS Pagep. 1820
Figure 31-67-00-23900-B – SD – COND Pagep. 1821
Figure 31-67-00-24100-A – SD – ELEC Pagep. 1822
Figure 31-67-00-24300-A – SD – F/CTL Pagep. 1823
Figure 31-67-00-24500-B – SD – FUEL Pagep. 1824
Figure 31-67-00-24700-A – SD – HYD Pagep. 1825
Figure 31-67-00-24900-A – SD – WHEEL Pagep. 1826
Figure 31-67-00-25100-A – SD – BLEED Pagep. 1827
Figure 31-67-00-25300-A – SD – APU Pagep. 1828
Figure 31-67-00-25500-F – SD – DOOR/OXY Pagep. 1829
Figure 31-67-00-25700-B – SD – ENGINE (secondary parameters) Pagep. 1830
Figure 31-67-00-25900-A – SD – STATUS Pagep. 1831
Figure 31-67-00-26100-A – SD – Permanent Parametersp. 1832
Figure 31-67-00-26300-A – Permanent Parameters – Display of TAT and SATp. 1833
Figure 31-67-00-26500-A – Permanent Parameters – Display of G LOAD, ALT SEL and the timep. 1834
Figure 31-67-00-26800-A – Permanent Parameters – Display of the Gross Weightp. 1835
Figure 31-67-00-27100-C – SD – CRUISE Page: Display of 9 Parametersp. 1836
+31-67-21 – SYSTEM DISPLAY – COND & CAB PRESS PAGESp. 1837
+31-67-21 PB 001 CONF 00 – SYSTEM DISPLAY – COND & CAB PRESS PAGES – DESCRIPTION AND OPERATIONp. 1837
CAB PRESS Pagep. 1837
COND Pagep. 1844
Figure 31-67-21-28500-A – CAB PRESS Page – Display of the parameters 1 to 13p. 1848
Figure 31-67-21-28700-A – CAB PRESS Page – Display of the parameter: CABIN DIFFERENTIAL PRESSUREp. 1849
Figure 31-67-21-28900-A – CAB PRESS Page – Display of the parameter: CABIN VERTICAL SPEEDp. 1850
Figure 31-67-21-29100-A – CAB PRESS Page – Display of the parameter: CABIN ALTITUDEp. 1851
Figure 31-67-21-29300-A – CAB PRESS Page – Display of the parameters: LANDING ELEVATION and SAFETY VALVEp. 1852
Figure 31-67-21-29500-A – CAB PRESS Page – Display of the parameters: SYSTEM IN CTL and PACK FLOW CTL VALVEp. 1853
Figure 31-67-21-29700-A – CAB PRESS Page – Display of the parameter: OUTFLOW VALVE POSITIONp. 1854
Figure 31-67-21-29900-A – CAB PRESS Page – Display of the parameters: AIR EXTRACT VALVE and EXTRACT INDICATIONp. 1855
Figure 31-67-21-30100-A – CAB PRESS Page – Display of the parameter: AIR INLET VALVE POSITIONp. 1856
Figure 31-67-21-30400-D – COND Page – Display of the Parametersp. 1857
Figure 31-67-21-30600-A – COND Page – Display of the Parameters: PACK CTL MODE, DUCT TEMP., HOT AIR SHUTOFF VALVEp. 1858
Figure 31-67-21-30800-A – COND Page – Display of the Parameters: AFT CARGO UPSTREAM ISOL VALVE, HOT AIR SHUTOFF VALVE, DOWNSTREAM ISOL VALVEp. 1859
+31-67-24 – SYSTEM DISPLAY – ELEC PAGEp. 1860
+31-67-24 PB 001 CONF 00 – SYSTEM DISPLAY – ELEC PAGE – DESCRIPTION AND OPERATIONp. 1860
ELEC Pagep. 1860
ELEC Page linksp. 1866
Figure 31-67-24-29300-A – SD – ELEC Page: Display of the Parameters 1 to 26p. 1870
Figure 31-67-24-29500-A – ELEC Page – Display of the Parameters: BATTERY OPERATION, BATTERY BUSBAR, DC ESS BUSBARp. 1871
Figure 31-67-24-29700-A – ELEC Page – Display of the Parameters: EMERGENCY GENERATOR, ESSENTIAL TR, AC GENERATORSp. 1872
Figure 31-67-24-30400-A – ELEC Page – Display of the Parameters: BATTERY CONTACTORsp. 1873
Figure 31-67-24-30600-A – ELEC Page – Display of the Electrical links 1 to 29p. 1874
+31-67-27 – SYSTEM DISPLAY – F/CTL PAGEp. 1875
+31-67-27 PB 001 CONF 00 – SYSTEM DISPLAY – F/CTL PAGE – DESCRIPTION AND OPERATIONp. 1875
Figure 31-67-27-19900-A – SD – F/CTL Page: Display of the Parameters 1 to 23p. 1881
+31-67-28 – SYSTEM DISPLAY – FUEL PAGEp. 1882
+31-67-28 PB 001 CONF 00 – SYSTEM DISPLAY – FUEL PAGE – DESCRIPTION AND OPERATIONp. 1882
FUEL Pagep. 1882
Fuel linksp. 1891
Figure 31-67-28-34800-C – SD – FUEL Page – Display of the 23 Parametersp. 1893
Figure 31-67-28-35000-D – FUEL Page – Display of the Parameters: FUEL USED and FUEL ON BOARDp. 1894
Figure 31-67-28-35200-D – FUEL Page – Display of the Parameters: ENGINE FIRE VALVE and APU FIRE VALVEp. 1895
Figure 31-67-28-35400-D – FUEL Page – Display of the Parameter: XFEED VALVEp. 1896
Figure 31-67-28-35600-C – FUEL Page – Display of the Parameters: TANKs PUMPsp. 1897
Figure 31-67-28-35800-D – FUEL Page – Display of the Parameters: TRANSFER VALVE POSITION, INNER/OUTER FUEL QUANTITYp. 1898
Figure 31-67-28-36000-D – FUEL Page – Display of the Parameters: INNER/OUTER FUEL TEMPERATUREp. 1899
Figure 31-67-28-36400-B – FUEL Page – Display of the Parameters: CENTER TANK PUMPS, CENTER TANK FUEL QUANTITYp. 1900
+31-67-29 – SYSTEM DISPLAY – HYD PAGEp. 1901
+31-67-29 PB 001 CONF 00 – SYSTEM DISPLAY – HYD PAGE – DESCRIPTION AND OPERATIONp. 1901
HYD Pagep. 1901
Figure 31-67-29-19200-A – SD – HYD Page: Display of the 16 Parametersp. 1908
Figure 31-67-29-19400-A – HYD Page – Display of the Parameters: HYDRAULIC SYSTEM STATUS and HYDRAULIC PRESSUREp. 1909
Figure 31-67-29-19600-A – HYD Page – Display of the Parameters: YELLOW ELEC PUMP and RAT OPERATIONp. 1910
Figure 31-67-29-19800-A – HYD Page – Display of the Parameters: HYDRAULIC PUMPsp. 1911
Figure 31-67-29-20000-A – HYD Page – Display of the Parameters: FLUID LEVELp. 1912
Figure 31-67-29-20200-A – HYD Page – Display of the 10 hydraulic linksp. 1913
Figure 31-67-29-20400-A – HYD Page – PTU linksp. 1914
+31-67-32 – SYSTEM DISPLAY – WHEEL PAGEp. 1915
+31-67-32 PB 001 CONF 00 – SYSTEM DISPLAY – WHEEL PAGE – DESCRIPTION AND OPERATIONp. 1915
WHEEL Pagep. 1915
Figure 31-67-32-22500-A – SD – WHEEL Page: Display of the 12 Parametersp. 1920
Figure 31-67-32-22700-A – WHEEL Page – Display of the Parameters: LEFT LANDING GEAR and DOORp. 1921
Figure 31-67-32-22900-A – WHEEL Page – Display of the Parameters: NOSE LANDING GEAR and DOOR, HOTTEST WHEELp. 1922
Figure 31-67-32-23000-A – WHEEL Page – Display of the Parameters: RIGHT LANDING GEAR, AUTO BRAKE SELECTION and MODEp. 1923
Figure 31-67-32-23100-A – WHEEL Page – Display of the Parameters: RIGHT LANDING GEAR, AUTO BRAKE SELECTION and MODEp. 1924
Figure 31-67-32-23300-A – WHEEL Page – Display of the Parameters: SPOILERs STATUSp. 1925
+31-67-35 – SYSTEM DISPLAY – OXY PAGEp. 1926
+31-67-35 PB 001 CONF 00 – SYSTEM DISPLAY – OXY PAGE – DESCRIPTION AND OPERATIONp. 1926
Generalp. 1926
+31-67-36 – SYSTEM DISPLAY – BLEED PAGEp. 1927
+31-67-36 PB 001 CONF 00 – SYSTEM DISPLAY – BLEED PAGE – DESCRIPTION AND OPERATIONp. 1927
BLEED Pagep. 1927
Figure 31-67-36-25000-A – SD – BLEED Page: Display of the 29 Parametersp. 1936
Figure 31-67-36-25200-A – BLEED Page – Display of the Parameter: RAM AIR VALVEp. 1937
Figure 31-67-36-25400-A – BLEED Page – Display of the Parameters: PACK and PACK OUTLET TEMPERATUREsp. 1938
Figure 31-67-36-25600-A – BLEED Page – Display of the Parameters: PACK FLOW and ANTI ICE VALVEp. 1939
Figure 31-67-36-25800-A – BLEED Page – Display of the Parameters: PACK FLOW CTL VALVE and XFEED VALVEp. 1940
Figure 31-67-36-26000-B – BLEED Page – Display of the Parameters: APU BLEED VALVE, ENGINE BLEED PRESSURE and TEMPERATUREp. 1941
Figure 31-67-36-26200-A – BLEED Page – Display of the Parameters: ENGINE BLEED VALVE and HP BLEED VALVEp. 1942
+31-67-49 – SYSTEM DISPLAY – APU PAGEp. 1943
+31-67-49 PB 001 CONF 00 – SYSTEM DISPLAY – APU PAGE – DESCRIPTION AND OPERATIONp. 1943
APU Pagep. 1943
Figure 31-67-49-16100-A – SD – APU Page: Display of the 10 Parametersp. 1947
Figure 31-67-49-16300-A – APU Page – Display of the Parameter: APU GENERATORp. 1948
Figure 31-67-49-16500-A – APU Page – Display of the Parameters: APU BLEED VALVE and BLEED PRESSUREp. 1949
Figure 31-67-49-16700-A – APU Page – Display of the Parameter: APU AIR INTAKEp. 1950
Figure 31-67-49-16900-A – APU Page – Display of the Parameter: APU SPEEDp. 1951
Figure 31-67-49-17100-A – APU Page – Display of the Parameter: APU EXHAUST GAS TEMPERATUREp. 1952
+31-67-52 – SYSTEM DISPLAY – DOOR/OXY PAGEp. 1953
+31-67-52 PB 001 CONF 00 – SYSTEM DISPLAY – DOOR/OXY PAGE – DESCRIPTION AND OPERATIONp. 1953
DOOp. 1953
Figure 31-67-52-19700-C – SD – DOOR/OXY Page: Display of the 18 Parametersp. 1958
Figure 31-67-52-19900-A – DOOR/OXY Page – Display of the Parameters: DOOR and CARGO DOOR STATUSp. 1959
Figure 31-67-52-20300-A – DOOR/OXY Page – Display of the Parameters: AVIONIC DOORsp. 1960
Figure 31-67-52-20500-A – DOOR/OXY Page – Display of the Parameters: EMER EXITsp. 1961
Figure 31-67-52-20700-A – DOOR/OXY Page – Display of the Parameters: SLIDE OPERATIONp. 1962
Figure 31-67-52-20900-A – DOOR/OXY Page – Display of the Parameter: CABIN VERTICAL SPEEDp. 1963
+31-67-77 – SYSTEM DISPLAY – ENGINE PAGEp. 1964
+31-67-77 PB 001 CONF 00 – SYSTEM DISPLAY – ENGINE PAGE – DESCRIPTION AND OPERATIONp. 1964
ENGINE Pagep. 1964
Figure 31-67-77-18700-B – SD – ENGINE Page: Display of the 10 Parametersp. 1968
Figure 31-67-77-18900-B – ENGINE Page – Display of the Parameter: OIL PRESSUREp. 1969
Figure 31-67-77-19100-B – ENGINE Page – Display of the Parameters: OIL QUANTITY and FUEL USEDp. 1970
Figure 31-67-77-19300-B – ENGINE Page – Display of the Parameter: NACELLE TEMPERATUREp. 1971
Figure 31-67-77-19500-A – ENGINE Page – Display of the Parameter: OIL TEMPERATUREp. 1972
+31-68 – EIS – SWITCHINGp. 1973
+31-68-00 – EIS – SWITCHINGp. 1973
+31-68-00 PB 001 CONF 00 – EIS – SWITCHING – DESCRIPTION AND OPERATIONp. 1973
Generalp. 1973
Links Between DMCs and DUsp. 1974
EIS Switching Operationp. 1975
Switching of the Various Onside & Offside DMC Input Busesp. 1981
Figure 31-68-00-13500-A – EIS – DMCs/DUs Links & Reconfiguration Controlsp. 1989
Figure 31-68-00-13600-A – Master and Feedback DSDLsp. 1990
Figure 31-68-00-16100-A – EIS – Alternate Inputs Selectionp. 1991
Figure 31-68-00-16500-A – EIS – PFD & ND Brightness & ON/OFF Controls PFD/ND XFR P/BSWp. 1992
Figure 31-68-00-16700-A – EIS Relay Boxes – PFD/ND XFR Circuitryp. 1993
Figure 31-68-00-16800-A – EIS Relay Boxes – DME AUDIO VOR/ILS Selection Controlp. 1994
Figure 31-68-00-17400-A – ECAM DUs – Normal/Alternate Inputs Controlp. 1995
Figure 31-68-00-17900-B – DMC Output Busesp. 1996
Figure 31-68-00-20400-A – FMGC – EIS Bus/DMC Interfacep. 1997
Figure 31-68-00-20600-C – FCU Busesp. 1998
Figure 31-68-00-21200-B – EEC – IAE Enginesp. 1999
Figure 31-68-00-21400-A – TCAS Busesp. 2000
Figure 31-68-00-22500-A – W/R Transceiver – DMCs Interfacep. 2001
Figure 31-68-00-22700-A – EFIS/ECAM Reconfigurations Between DMCs and Between DUsp. 2002
Figure 31-68-00-22800-A – EIS (and ADIRS) – Transfer Selector Switchesp. 2003
+31-68-00 PB 401 CONF 00 – EIS – SWITCHING – DEACTIVATION/REACTIVATIONp. 2004
31-68-00-040-005-A – Deactivation of the DMC2 when AC ESS FEED control is operativep. 2004
31-68-00-440-004-A – Reactivation of the DMC2p. 2006
31-68-00-040-004-A – Deactivation of the ATT HDG Selector Switchp. 2007
31-68-00-440-002-A – Reactivation of the ATT HDG Selector Switchp. 2011
31-68-00-040-002-A – Deactivation of the AIR DATA Selector Switchp. 2012
31-68-00-440-003-A – Reactivation of the AIR DATA Selector Switchp. 2016
31-68-00-040-003-A – Deactivation of the EIS DMC Selector Switchp. 2017
31-68-00-440-001-A – Reactivation of the EIS DMC Selector Switchp. 2020
31-68-00-040-006-A – Deactivation of the Lower ECAM DU when AC ESS FEED control is operativep. 2021
31-68-00-440-005-A – Reactivation of the Lower ECAM DUp. 2023
+31-69 – EIS – TEST/BITEp. 2024
+31-69-00 – EIS – TEST/BITEp. 2024
+31-69-00 PB 001 CONF 00 – EIS – TEST/BITE – DESCRIPTION AND OPERATIONp. 2024
Generalp. 2024
Failure Detectiop. 2026
Operation in the Normal Modep. 2029
Operation in the Menu or Maintenance Modep. 2032
A/C Test Plugs for Maintenancep. 2036
List of Error Codesp. 2037
Figure 31-69-00-12000-A – EIS/FWS – CFDS Interfacep. 2044
Figure 31-69-00-27500-A – Flight Phases definitionp. 2045
Figure 31-69-00-31200-A – Access Procedure for the Menu Modep. 2046
Figure 31-69-00-32300-A – Main EIS Menu Displayp. 2048
Figure 31-69-00-32400-A – LEG REPORTS Displayp. 2049
Figure 31-69-00-32500-A – EIS LRU IDENTIFICATION Displayp. 2050
Figure 31-69-00-32700-A – DUMP OF THE BITE MEMORYp. 2051
Figure 31-69-00-32800-A – INTERNAL & EXTERNAL FAULTS IN FLT Menusp. 2052
Figure 31-69-00-32900-A – FAULTS ON GNDp. 2054
Figure 31-69-00-33400-A – MAIN EIS MENU Displayp. 2055
Figure 31-69-00-33500-A – ENGINES OVERSPD/TEMP Testp. 2056
Figure 31-69-00-33700-A – TESTS Menup. 2057
Figure 31-69-00-33800-A – INPUT TEST Operationp. 2058
Figure 31-69-00-33900-A – DISPLAY TESTp. 2059
Figure 31-69-00-34000-A – SYSTEM Testp. 2060
Figure 31-69-00-35500-A – Test Plug Locationp. 2061
Chapter 32 – LANDING GEAR
Chapter 33 – LIGHTS
Chapter 34 – NAVIGATION
Chapter 35 – OXYGEN
Chapter 36 – PNEUMATIC
Chapter 38 – WATER/WASTE
Chapter 46 – INFORMATION SYSTEMS
Chapter 49 – AIRBORNE AUXILIARY POWER
Chapter 51 – STANDARDS PRACTICES AND STRUCTURES
Chapter 52 – DOORS
Chapter 53 – FUSELAGE
Chapter 54 – NACELLES/PYLONS
Chapter 55 – STABILIZERS
Chapter 56 – WINDOWS
Chapter 57 – WINGS
Chapter 70 – (IAE) – STANDARD PRACTICES – ENGINE
Chapter 71 – (IAE) – POWER PLANT
Chapter 72 – (IAE) – ENGINE
Chapter 73 – (IAE) – ENGINE FUEL AND CONTROL
Chapter 74 – (IAE) – IGNITION
Chapter 75 – (IAE) – AIR
Chapter 76 – (IAE) – ENGINE CONTROLS
Chapter 77 – (IAE) – ENGINE INDICATING
Chapter 78 – (IAE) – EXHAUST
Chapter 79 – (IAE) – OIL
Chapter 80 – (IAE) – STARTING
The Aircraft Integrated Data System sections cover DMU and FDIMU configurations, data interfaces, report generation, parameter call-up, programming, stored and manually requested reports, software and database loading, PCMCIA-card procedures, data downloading and unit battery replacement. The manual also includes AIDS input-interface material and report sections for ECS, APU, structural load and engine-related data.
File Details
- Manual type: Aircraft Maintenance Manual – Chapter 31
- Aircraft: A318 / A319 / A320 / A321
- Chapter: 31 – Indicating/Recording Systems
- Revision: 40
- Date: May 01/12
- Language: English
- Page count: 2061 pages
- File format: PDF
Chapters Covered
- 31-00-00 – Indicating/Recording Systems – General
- 31-10-00 – Instruments and Control Panels – Maintenance Practices
- 31-14-25 – Overhead Control and Indicating Panel
- 31-21-00 – Electrical Clock
- 31-21-21 – Clock Removal/Installation
- 31-30-00 – Centralized Fault Display System and Data Recording System
- 31-32-00 – Centralized Fault Display Interface (CFDIU)
- 31-32-34 – Centralized Fault Display Interface Unit Removal/Installation
- 31-33-00 – Digital Flight Data Recording System Interconnection
- 31-33-16 – Three-Axis Accelerometer
- 31-33-34 – Flight Data Interface Unit
- 31-33-55 – Digital Flight Data Recorder
- 31-35-00 – Multifunction Printing
- 31-35-22 – Printer
- 31-36-00 – AIDS Interconnection
- 31-36-34 – Data Management Unit / FDIMU
- 31-37-00 – AIDS Input Interface
- 31-37-21 – AIDS ECS Reports
- 31-37-49 – AIDS APU Reports
- 31-37-51 – AIDS Structure Reports
- 31-37-73 – AIDS Engine Reports
- 31-38-00 – Up and Down Data Loading System Acquisition/Interface and Equipment
- 31-50-00 – Central Warning Systems
- 31-51-00 – Operational Presentation
- 31-52-00 – FWC Acquisition/Interface
- 31-53-21 – Loudspeaker Removal/Installation
- 31-53-34 – Flight Warning Computer Removal/Installation
- 31-54-00 – SDAC Acquisition/Interface
- 31-55-34 – System Data Acquisition Concentrator Removal/Installation
- 31-56-00 – ECAM Control Panel
- 31-60-00 – Electronic Instrument System
- 31-61-00 – EIS Control
- 31-61-12 – ECAM Control Panel Removal/Installation
- 31-62-00 – DMC Acquisition/Interface
- 31-63-00 – Display Management Computer
- 31-63-22 – Display Unit
- 31-63-34 – Display Management Computer Removal/Installation
- 31-64-00 – Primary Flight Display
- 31-65-00 – Navigation Display
- 31-66-00 – ECAM Engine/Warning Display
- 31-67-00 – ECAM System/Status Display
- 31-67-21 – COND and CAB PRESS Pages
- 31-67-24 – ELEC Page
- 31-67-27 – F/CTL Page
- 31-67-28 – FUEL Page
- 31-67-29 – HYD Page
- 31-67-32 – WHEEL Page
- 31-67-35 – OXY Page
- 31-67-36 – BLEED Page
- 31-67-49 – APU Page
- 31-67-52 – DOOR/OXY Page
- 31-67-77 – ENGINE Page
- 31-68-00 – EIS Switching
- 31-69-00 – EIS Test/BITE
IMAGES PREVIEW
Taken together, these sections provide a broad Chapter 31 maintenance reference for understanding system architecture, following aircraft-specific maintenance tasks, replacing relevant LRUs, carrying out operational tests, accessing maintenance reports and interpreting the display, recording and fault-monitoring systems used across the A318/A319/A320/A321 family.
Maintain, Test and Diagnose Chapter 31 Systems
The Airbus A318 A319 A320 A321 Chapter 31 Indicating and Recording Systems Maintenance Manual AES Rev 40 2012 supports practical work on cockpit indication, ECAM and EIS equipment, centralized fault reporting, data recording, printers, DMU/FDIMU functions, display-management computers, PFD and ND systems, Flight Warning Computers, SDACs and associated interfaces. The combination of procedures, system descriptions, component-location information, block diagrams, wiring/interface drawings and test instructions helps technicians work from the documented configuration and task requirements rather than relying on general assumptions.
Correct maintenance data matters when dealing with interconnected avionics and recording systems, where component configuration, aircraft applicability, test sequence and system interfaces can affect the job. This manual is supplied as an instant PDF download after purchase, with no physical shipping required. It can be viewed on compatible computers, tablets and phones and printed for workshop or maintenance-reference use.
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