(2) Read the LAST LEG REPORT (Ref. AMM TASK 21-26-00-710-009).
4. Fault Isolation
_______________
A. Possible maintenance messages (one or more of the following messages) SKIN AIR INLET V 15HQ SKIN AIR OUTLET V 22HQ
(1) if the test gives SKIN AIR INLET V 15HQ, replace the VALVE-SKIN AIR INLET, AVNCS VENT (15HQ) (Ref. AMM TASK 21-26-52-000-001) and (Ref. AMM TASK 21-26-52-400-001).
(2) if the test gives SKIN AIR OUTLET V 22HQ, replace the VALVE-SKIN AIR OUTLET, AVNCS VENT (22HQ) (Ref. AMM TASK 21-26-53-000-001) and (Ref. AMM TASK 21-26-53-400-001).
B. Do the operational test given in Para. 3.
「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 275
May 01/05R CES
TASK 21-26-00-810-831
Closure of the Avionics Skin Air Inlet and Outlet Valves after Failure of the Cabin Pressure Controller on Ground
1. Possible Causes
_______________
- CONTROLLER-CABIN PRESSURE 1 (11HL)
- CONTROLLER-CABIN PRESSURE 2 (12HL)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 21-26-00-710-001 Operational Check of System via MCDU 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 an operational test of the avionics equipmemt ventilation from the Multipurpose Control and Display Unit (MCDU) (Ref. AMM TASK 21-26-00-710-001).
(a) Make sure that the avionics equipment ventilation system operates correctly.
(b) Make sure that the skin air inlet and outlet valves (15HQ and 22HQ) stay closed.
4. Fault Isolation
_______________
A. If the test confirms the fault:
(1) Remove the two cabin pressure controllers (11HL and 12HL) (Ref. AMM TASK 21-31-34-000-001).
(2) Make sure that the skin air inlet and outlet valves (15HQ and 22HQ) open.
「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 276
May 01/05R
CES
(3) Install the cabin pressure controller 1 (11HL) (Ref. AMM TASK 21-31-34-400-001).
(a) If the skin air inlet and outlet valves close:
(b) If the skin air inlet and outlet valves stay open: 1 Install the cabin pressure controller 2 (12HL) (Ref. AMM TASK
1_ Replace the CONTROLLER-CABIN PRESSURE 1 (11HL) (Ref. AMM TASK
21-31-34-000-001) and (Ref. AMM TASK 21-31-34-400-001).
2_ Install the cabin pressure controller 2 (12HL) (Ref. AMM TASK
21-31-34-400-001).
_
21-31-34-400-001). 2 Make sure that the skin air inlet and outlet valves close.
_ 3 Replace the CONTROLLER-CABIN PRESSURE 2 (12HL) (Ref. AMM TASK
_ 21-31-34-000-001) and (Ref. AMM TASK 21-31-34-400-001).
B. Do the operational test given in Para. 3.
「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 277
May 01/05R
CES
TASK 21-26-00-810-835
Failure of the Mechanic Call Horn During a Smoke Detection in the Avionics Compartment on Ground
1. Possible Causes
_______________
- HORN-MECH CALL (15WC)
- wiring between the relay (4WC) and the mechanic call horn (15WC)
- wiring between the pin A/X2 of the relay (4WC) and the first terminal block
- diode module 1800VD
- wiring between the pin A/D of the relay (12KS2) and the pins A/28 and A/29 of the diode module 1800VD
- RELAY-OIL LOW PRESS AND GROUND, ENG1 (12KS1)
- RELAY-OIL LOW PRESS AND GROUND, ENG2 (12KS2)
- wiring between the pin A/8 of the relay (12KS2) and the pin A/D of the relay (12KS1) 中國航空網(wǎng) www.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(diào)1(85)
