- OUTFLOW VALVE ELEC 2 (76),
- OUTFLOW VALVE ELEC 2 (83),
- OUTFLOW VALVE ELEC 2 (87), refer to (Ref. TASK 21-31-00-810-834).
R (9) Fault Code (77)
(a) For the CFDS messages and associated fault code which follows,
- OUTFLOW VALVE ELEC 1 (77), refer to (Ref. TASK 21-31-00-810-835).
- OUTFLOW VALVE ELEC 2 (77), refer to (Ref. TASK 21-31-00-810-836).
R (10) Fault Code (78)
(a) For the CFDS messages and associated fault code which follows,
- OUTFLOW VALVE ELEC 1 (78) or,
- OUTFL.V FEEDB ASSY 1 (78), refer to (Ref. TASK 21-31-00-810-805).
- OUTFLOW VALVE ELEC 2 (78) or,
- OUTFL.V FEEDB ASSY 2 (78),
refer to (Ref. TASK 21-31-00-810-826). R
(11) Fault Code (88)
(a) For the CFDS messages and associated fault code which follows,
- OUTFL.V AUTO MOTOR 1 (88),
- OUTFL.V AUTO MOTOR 2 (88), refer to (Ref. TASK 21-31-00-810-804).
TASK 21-31-00-810-801
Cabin Pressure Controller 1 Fault
1. Possible Causes
_______________
- CONTROLLER-CABIN PRESSURE 1 (11HL)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 21-31-00-710-002 Operational Test of the Pressure Control and
Monitoring AMM 21-31-34-000-001 Removal of the Cabin Pressure Controller (11HL,12HL) AMM 21-31-34-400-001 Installation of the Cabin Pressure Controller
(11HL,12HL)
3. Fault Confirmation
__________________
A. Test
(1) Do the operational test of the pressure control and monitoring system (Ref. AMM TASK 21-31-00-710-002).
4. Fault Isolation
_______________
A. If one or more of these reports, LAST LEG REPORT, PREVIOUS LEG REPORT and CLASS 3 REPORT and/or the test gives one of the maintenance messages which follow:
- PRESS CONTROLLER 1 (00) or,
- PRESS CONTROLLER 1 (01) or,
- PRESS CONTROLLER 1 (08) or,
- PRESS CONTROLLER 1 (12) or,
- PRESS CONTROLLER 1 (13) or,
- PRESS CONTROLLER 1 (18) or,
- PRESS CONTROLLER 1 (22) or,
- PRESS CONTROLLER 1 (36) or,
- PRESS CONTROLLER 1 (37) or,
- PRESS CONTROLLER 1 (38) or,
- PRESS CONTROLLER 1 (39) or,
- PRESS CONTROLLER 1 (40) or,
- PRESS CONTROLLER 1 (41) or,
- PRESS CONTROLLER 1 (45) or,
- PRESS CONTROLLER 1 (46) or,
- PRESS CONTROLLER 1 (47) or,
- PRESS CONTROLLER 1 (49) or,
- PRESS CONTROLLER 1 (53) or,
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞21-31-00∞∞∞∞∞∞∞∞∞∞Page 206
Aug 01/00R CES
R - PRESS CONTROLLER 1 (58) or,
- PRESS CONTROLLER 1 (61),
- replace the CONTROLLER-CABIN PRESSURE 1 (11HL) (Ref. AMM TASK 21-31-34-000-001) and (Ref. AMM TASK 21-31-34-400-001).
B. Do the test as given in the Para. 3.A.
R TASK 21-31-00-810-802
R Manual Mode - CPC Fault
R 1. Possible Causes
_______________
R - CONTROLLER-CABIN PRESSURE 1 (11HL)
R - CONTROLLER-CABIN PRESSURE 2 (12HL)
R - P/BSW-CABIN PRESS/MODE SEL/AUTO (14HL)
R - CONNECTOR (11HL-AB)
R - CONNECTOR (12HL-AB)
R - CONNECTOR (14HL-A)
R 2. Job Set-up Information
______________________
R A. Referenced Information
R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
R AMM 21-31-00-710-002 R R AMM 21-31-34-000-001 R AMM 21-31-34-400-001 R R ASM 21-31/01
R 3. Fault Confirmation
__________________ Operational Test of the Pressure Control and Monitoring Removal of the Cabin Pressure Controller (11HL,12HL) Installation of the Cabin Pressure Controller (11HL,12HL)
R A. Do the operational test of the pressure control and monitoring system R (Ref. AMM TASK 21-31-00-710-002).
R 4. Fault Isolation
_______________
R A. If, when the MAN mode is selected, on the upper ECAM DU the warning CAB
R PR SYS 1+2 FAULT shows and,
R on the MODE SEL p/b switch the FAULT legend comes on do a:
R (1) Wiring Continuity and Ground check (Ref. ASM 21-31/01)
R (a) Do a check for continuity at, 中國航空網 m.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 AIR CONDITIONING 空調1(92)
