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时间:2011-03-28 09:16来源:蓝天飞行翻译 作者:航空
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_______________________________________________
 1. Pack Controller
_______________
 A. CFDS Fault Information Additional information about a failed component are available in the MCDU CAB TEMP CONT menu. The related LAST LEG REPORT page shows:
 - the date and time when the fault occurs,

 - the ATA number of the component,

 - the FIN of the component.


R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
 B. Initiated PC Test Data If a fault is detected during the PC initiated test, a fault code for shop maintenance is transmitted to the zone controller (common internal fault processing). The possible fault codes with their attached fault origns are given in the cockpit and cabin temperature control task supporting data (Ref. TSM 216300, P.Block 301).
R **ON A/C 401-499,
 B. Troubleshooting Data: The touble shooting data gives additional information for shop maintenance.


 Pack Temperature Control - Block Diagram Figure 301 (SHEET 1)
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-003, 051-054, ∞∞21-61-00∞∞∞∞∞∞∞∞∞∞Page 302
 May 01/05 CES


 Pack Temperature Control - Block Diagram Figure 301 (SHEET 2)
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-003, 051-054, ∞∞21-61-00∞∞∞∞∞∞∞∞∞∞Page 303
 May 01/05 CES


 Pack Temperature Control - Block Diagram
 Figure 301A (SHEET 1)

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 004-049, 055-099, 101-149, 151-199, ∞∞21-61-00∞∞∞∞∞∞∞∞∞∞Page 304
 201-299, Aug 01/05 CES


 Pack Temperature Control - Block Diagram
 Figure 301A (SHEET 2)

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 004-049, 055-099, 101-149, 151-199, ∞∞21-61-00∞∞∞∞∞∞∞∞∞∞Page 305
 201-299, Aug 01/05 CES


 Pack Temperature Control - Block Diagram
 Figure 301B (SHEET 1)

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 301-399, ∞∞21-61-00∞∞∞∞∞∞∞∞∞∞Page 306
 Aug 01/05 CES


 Pack Temperature Control - Block Diagram
 Figure 301B (SHEET 2)

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 301-399, ∞∞21-61-00∞∞∞∞∞∞∞∞∞∞Page 307
 Aug 01/05 CES


 COCKPIT AND CABIN TEMPERATURE CONTROL - FAULT ISOLATION PROCEDURES
__________________________________________________________________
 TASK 21-63-00-810-801
 Zone Controller Fault
 1. Possible Causes
_______________
 - CONT-ZONE TEMPERATURE (8HK)

 - wiring


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
21-63-00-810-827 Zone Cont Electrical Component with Short Circuit (Primary/Secondary Channels) AMM 21-63-00-710-004 Operational Test of the Cockpit and Cabin Temperature
 Control with CFDS/MCDU
 AMM 21-63-34-000-001 Removal of the Zone Controller (8HK)
 AMM 21-63-34-400-001 Installation of the Zone Controller (8HK)
 ASM 21-63/01
 ASM 21-63/02

 3. Fault Confirmation
__________________
 A. Do the operational test of the cockpit and cabin temperature-control system with CFDS/MCDU (Ref. AMM TASK 21-63-00-710-004).
 NOTE : If a fault is detected, the ZC gives a fault code for shop
____ maintenance in addition to the related CFDS message(s). For detailed information see the applicable Page Block 301.
 4. Fault Isolation
_______________
R
R A. If the test gives the maintenance message ZONE CONT:
 - replace the CONT-ZONE TEMPERATURE (8HK) (Ref. AMM TASK 21-63-34-000-001) and (Ref. AMM TASK 21-63-34-400-001).
 (1) If the fault continues:
 - do a check and repair the wiring if necessary between: ZC (8HK) connector AC/6 and CB (1HK), ZC (8HK) connector AC/4 and GND, ZC (8HK) connector AC/5 and CB (2HK), ZC (8HK) connector AC/1 and GND, ZC (8HK) connector AC/11 and GND,
 
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