_________

R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
 The air conditioning system has interfaces with:
 -
the Centralized Fault Display System (CFDS) (Ref. 31-30-00),

 -
the System Data Aquisition Concentrators (SDACs) (Ref. 31-55-00),

 -
the Display Management Computers (DMCs) (Ref. 31-63-00)

 -
the Flight Warning Computers (FWCs) (Ref. 31-53-00)

 -
the electrical power system (Ref. 24-00-00),

 -
the Cabin-Intercommunication Data System (CIDS) (Ref. 23-73-00),

 -
the Engine Interface Units (EIUs) (Ref. 73-25-00),

 -
the Bleed Monitoring Computers (BMCs) (Ref. 36-11-00),

 -
the Smoke-Detection Control Unit (SDCU) (Ref. 26-17-00),

 -
the Landing Gear Control and Interface Unit (LGCIU) (Ref. 32-31-00),

 -
the Electronic Control Box (ECB) (Ref. 49-61-00),

 -
the Air Data Computer (ADC) (Ref. 34-12-00)

 -
the Wing Anti Ice System (WAI) (Ref. 30-11-00)

 Air flows and cabin temperatures for normal operating and 1 pack failure cases

 Figure 002A 
R 1EFF : 1 1 1CES  151-199, 401-499,  1 111 21-00-00 Page 7 Aug 01/05

R AIR flows and cabin temperatures for normal operating and 1 pack failure cases

R  Figure 002B 
R 1EFF :  301-399,  1  21-00-00 Page 8 
1  1  May 01/04
 1  1
 1CES  1

 INTENTIONALLY BLANK

R 1 1
21-00-00Page 9
1 1 May 01/04 1 1 1CES 1

 Power Supply Figure 003 (SHEET 1)
 1EFF : 1 1R 1CES  ALL  1 11 1 21-00-00 Page 10 May 01/04

 Power Supply Figure 003 (SHEET 2)
 1EFF : 1 1R 1CES  ALL  1 11 1 21-00-00 Page 11 May 01/04

 - the Nacelle Anti Ice System (NAI) (Ref. 30-21-00) - the Data Management Unit (DMU) (Ref. 31-36-00). 
R  **ON A/C 401-499, 
R R R R R R R R R R R R R R R R  The air conditioning system has interfaces with: - the Centralized Fault Display System (CFDS) (Ref. 31-30-00), - the System Data Aquisition Concentrators (SDACs) (Ref. 31-55-00), - the Display Management Computers (DMCs) (Ref. 31-63-00) - the Flight Warning Computers (FWCs) (Ref. 31-53-00) - the electrical power system (Ref. 24-00-00), - the Cabin-Intercommunication Data System (CIDS) (Ref. 23-73-00), - the Engine Interface Units (EIUs) (Ref. 73-25-00), - the Bleed Monitoring Computers (BMCs) (Ref. 36-11-00), - the CIDS (Smoke Detection Function) (Ref. 23-73-00), - the Landing Gear Control and Interface Unit (LGCIU) (Ref. 32-31-00), - the Electronic Control Box (ECB) (Ref. 49-61-00), - the Air Data Computer (ADC) (Ref. 34-12-00) - the Wing Anti Ice System (WAI) (Ref. 30-11-00) - the Nacelle Anti Ice System (NAI) (Ref. 30-21-00) - the Data Management Unit (DMU) (Ref. 31-36-00). 
R  **ON A/C ALL
 5. Operation/Control and Indication________________________________
 A. Failure Indications (Ref. Fig. 004) If there is an important failure, indications are shown in the cockpit. The indications can be: - the MASTER WARN lights come on and a continuous repetitive chime is heard, - the MASTER CAUT lights come on and a single chime is heard, - the applicable FAULT light comes on, - a warning message on the Upper Display of the Electronic Centralized Aircraft Monitoring System (ECAM) comes on, - the applicable page comes on the Lower Display of the ECAM and shows the abnormal condition.

 Controls And Indicator Locations Figure 004
 1EFF : 1 1R 1CES  ALL  1 11 1 21-00-00 Page 13 May 01/04

 B. Electronic Centralized Aircraft Monitoring (ECAM) (Ref. Fig. 005, 006, 007, 008, 009) The ECAM system is designed to give operational help for both normal and abnormal operations. It is a display system which gives the crew all necessary information on the functioning of the aircraft systems. This operational aid shows messages and system overviews on two Cathode Ray Tubes (CRT'S). The displayed information is used in normal operations for monitoring systems or to help the crew in their diagnosis and corrective actions during abnormal operations.
 (1)
 ECAM Classifications

 (a)
 Class 1, Level 3 (During Flight) This corresponds to an emergency configuration. The crew must take corrective action immediately.

 (b)
 Class 1, Level 2 (During Flight) This corresponds to an abnormal configuration of the aircraft. The crew must be made aware of this configuration immediately, but immediate corrective action is not required. The crew must decide how soon action has to be taken.
　
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