A. If the test gives a maintenance message, you can find the related trouble shooting procedure in the (Ref. TSM 36 PB 101).
(1) If there is no maintenance message:
-replace the BMC-1 (1HA1) (Ref. AMM TASK 36-11-34-000-001) and (Ref. AMM TASK 36-11-34-400-001).
B. After the subsequent flight, make sure that the fault does not continue.
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Amber XX on the Lower ECAM DU Replace the Position Indication of the HP Bleed Valve of the Engine 1
1. Possible Causes
_______________
-BMC-1 (1HA1)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 36-11-00-740-001 BITE Test of the BMC 1(2)
AMM 36-11-34-000-001 Removal of the BMC (1HA1, 1HA2)
AMM 36-11-34-400-001 Installation of the BMC (1HA1, 1HA2)
TSM 36 PB 101
3. Fault Confirmation
__________________
A. Test
(1) Do the BITE test of the BMC1 (Ref. AMM TASK 36-11-00-740-001).
4. Fault Isolation
_______________
A. If the test gives a maintenance message, you can find the related trouble shooting procedure in the (Ref. TSM 36 PB 101).
(1) If there is no maintenance message:
-replace the BMC-1 (1HA1) (Ref. AMM TASK 36-11-34-000-001) and (Ref. AMM TASK 36-11-34-400-001).
B. After the subsequent flight, make sure that the fault does not continue.
1
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-∞∞36-11-00∞∞∞∞∞∞∞∞∞∞Page A283
--Feb 01/05R ---CES -
The Bleed Pressure-Regulator Valve of the Engine 2 is Shown Open Amber on the Lower ECAM DU
1. Possible Causes_______________
-VALVE-BLEED PRESS REG (4001HA)
-SOLENOID-BLEED PRESS REG V CTL, ENG 2 (10HA2)
-XDCR-BLEED TRANSFER PRESS, ENG 2 (7HA2)
-wiring
2. Job Set-up Information______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 36-11-00-740-001 BITE Test of the BMC 1(2)
AMM 36-11-15-000-001 Removal of the Bleed Transferred Pressure Transducer (7HA1,7HA2)
AMM 36-11-15-400-001 Installation of the Bleed Transferred Pressure Transducer (7HA1,7HA2)
AMM 36-11-52-000-040 Removal of the Bleed Pressure-Regulator Valve (4001HA)
AMM 36-11-52-400-040 Installation of the Bleed Pressure-Regulator Valve (4001HA)
AMM 36-11-55-000-001 Removal of the Bleed-Pressure-Regulator Valve Control-Solenoid (10HA1,10HA2)
AMM 36-11-55-400-001 Installation of the Bleed-Pressure-Regulator Valve Control-Solenoid (10HA1,10HA2)
ASM 36-11/02
TSM 36 PB 101
3. Fault Confirmation__________________
A. Test
(1) Do the BITE test of the BMC2 (Ref. AMM TASK 36-11-00-740-001).
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--Feb 01/05R ---CES -
4. Fault Isolation
_______________
A. If the test gives a maintenance message, you can find the related trouble shooting procedure in the (Ref. TSM 36 PB 101).
(1) If there is no maintenance message:
-replace the VALVE-BLEED PRESS REG (4001HA) (Ref. AMM TASK 36-11-52-000-040) and (Ref. AMM TASK 36-11-52-400-040).
(a) If the fault continues:
-replace the SOLENOID-BLEED PRESS REG V CTL, ENG 2 (10HA2) (Ref. AMM TASK 36-11-55-000-001) and (Ref. AMM TASK 36-11-55-400-001).
1_ If the fault continues:
- replace the XDCR-BLEED TRANSFER PRESS, ENG 2 (7HA2) (Ref.
AMM TASK 36-11-15-000-001) and (Ref. AMM TASK 36-11-15-400-
001).
a If the fault continues:
_
-do a check and repair the wiring: . from the FULLY CLOSED signal of the BMC2 (1HA2) to the bleed pressure-regulator valve (4001HA) . from pin A/3 of the bleed pressure-regulator valve (4001HA) to the first terminal block (Ref. ASM 36-11/02).
B. After the subsequent flight, make sure that the fault does not continue.
1
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 PNEUMATIC(81)
