- If the fault continues:
. repair the wiring between the pin A/1 of the relay
(8WC) and the first terminal block.
B. Do the operational test given in Para. 3.
TASK 21-26-00-810-836
Avionics Ventilation System Bite Survey
1. Possible Causes
_______________
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 21-26-00-710-001 Operational Check of System via MCDU 21-26-00-991-001 Fig. 201
3. Fault Confirmation
__________________
A. Test
(1) Do the operational check of system via Multipurpose Control and Display Unit (MCDU) (Ref. AMM TASK 21-26-00-710-001).
4. Fault Isolation
_______________
A. If the test does not give the maintenance message AEVC and if the LAST LEG REPORT (LLR) shows no related CFDS message:
(1) Complete the page 11 of the SIL 21-099
(Ref. Fig. 201/TASK 21-26-00-991-001)
and send it back to Airbus for analysis.
Illustration of the Avionics Ventilation System Bite Survey
Figure 201/TASK 21-26-00-991-001
「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 ∞∞21-26-00∞∞∞∞∞∞∞∞∞∞Page 282
May 01/05 CES CARGO COMPARTMENT VENTILATION - FAULT ISOLATION PROCEDURES
__________________________________________________________
TASK 21-28-00-810-802
AFT Cargo-Compartment Isolation Valve(s) Fault
1. Possible Causes
_______________
- VALVE-ISOLATION, AFT CARGO COMPT (33HN)
- CONT-CARGO VENTILATION (10HN)
- VALVE-ISOLATION, AFT CARGO COMPT (34HN)
- BOARD-ANN LT TEST & INTFC (8LP)
- wiring
- PUSHBUTTON SWITCH-CARGO SMOKE/TEST (13WH)
- PUSHBUTTON SWITCH-CARGO VENT/AFT ISOL VALVE (36HN)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 21-26-52-400-001 Installation of the Avionics Ventilation Skin Air Inlet Valve (15HQ) AMM 21-28-00-710-006 Operational Test of the AFT Cargo-Compartment
Ventilation-System AMM 21-28-34-000-001 Removal of the Ventilation Controller (10HN) AMM 21-28-34-400-001 Installation of the Ventilation Controller (10HN) AMM 21-28-52-000-001 Removal of the AFT Cargo-Compartment Ventilation
Isolation-Valves (33HN,34HN)
AMM 21-28-52-400-001 Installation of the AFT Cargo-Compartment Ventilation
Isolation-Valves (33HN,34HN)
AMM 26-17-00-710-001 Operational Test of the Lavatory Smoke-Detection
System R AMM 32-69-00-740-001 BITE Check Landing Gear Control Interface Unit R (LGCIU) using MCDU to Ensure that Continuous BITE is R Operative
ASM 21-28/02
3. Fault Confirmation
__________________
A. Do the operational test of the AFT cargo-compartment ventilation-system (Ref. AMM TASK 21-28-00-710-006).
NOTE : You must visually monitor the inlet and outlet isolation valves in
____
the AFT cargo compartment during the test.
「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 ∞∞21-28-00∞∞∞∞∞∞∞∞∞∞Page 201
Feb 01/05 CES
4. Fault Isolation
_______________
A. If the isolation valve (33HN) does not operate and the FAULT legend on the pushbutton switch AFT ISOL VALVE, which is installed on the panel 22VU, comes on:
- do a check of the valve for damage (Ref. AMM TASK 21-28-52-000-001) and (Ref. AMM TASK 21-26-52-400-001).
(1) If the valve is damaged:
- replace the VALVE-ISOLATION, AFT CARGO COMPT (33HN) (referred to as VALVE (33HN)) (Ref. AMM TASK 21-28-52-000-001) and (Ref. AMM TASK 21-28-52-400-001).
(2) If the fault continues:
- replace the CONT-CARGO VENTILATION (10HN) (Ref. AMM TASK 21-28-34-000-001) and (Ref. AMM TASK 21-28-34-400-001).
(3) If the fault continues:
- do a check and repair the wiring between: VALVE (33HN) connector A/E and VC (10HN) connector B/X, VALVE (33HN) connector A/B and VC (10HN) connector B/Y, VALVE (33HN) connector A/A and VC (10HN) connector B/<B, VALVE (33HN) connector A/D and VC (10HN) connector B/<A, VALVE (33HN) connector A/F and GND, VALVE (33HN) connector A/C and GND (Ref. ASM 21-28/02).
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