3. Fault Confirmation
__________________
A. Test
(1) Do the BITE test of the BMC 2 (Ref. AMM TASK 36-11-00-740-001).
4. Fault Isolation
_______________
A. If the BITE test gives no maintenance message:
-no maintenance is necessary.
(1)
If the BITE test gives the class 3 maintenance message:
TEMP SENSOR 6HA2
-replace the SENSOR-EXCHANGER OUT TEMP, ENG 2 (6HA2) (Ref. AMM TASK 36-11-17-000-001) and (Ref. AMM TASK 36-11-17-400-001).
(2)
If the BITE test gives the class 3 maintenance message:
HP BLEED-V 4000HA2
-replace the VALVE-HP BLEED (4000HA) of the engine 2 (Ref. AMM TASK 36-11-51-000-042) and (Ref. AMM TASK 36-11-51-400-042).
B. After the subsequent flight, make sure that the fault does not continue.
1
-EFF : ALL
-∞∞36-11-00∞∞∞∞∞∞∞∞∞∞Page A260
--Feb 01/05R ---CES -
Loss of the Bleed Temperature Monitoring of the Engine 2
1. Possible Causes
_______________
-SENSOR-EXCHANGER OUT TEMP, ENG 2 (6HA2)
-BMC-2 (1HA2)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 36-11-00-740-001 BITE Test of the BMC 1(2) AMM 36-11-17-000-001 Removal of the Heat-Exchanger Outlet-Temperature Sensor 6HA1(6HA2) AMM 36-11-17-400-001 Installation of the Heat-Exchanger Outlet-Temperature
Sensor 6HA1(6HA2) 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 BMC2 (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 SENSOR-EXCHANGER OUT TEMP, ENG 2 (6HA2) (Ref. AMM TASK 36-11-17-000-001) and (Ref. AMM TASK 36-11-17-400-001).
(a) If the fault continues:
-replace the BMC-2 (1HA2) (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
-EFF : ALL
-∞∞36-11-00∞∞∞∞∞∞∞∞∞∞Page A261
--Feb 01/05R ---CES -
Small Variation of the Bleed Pressure Indication
1. Possible Causes_______________
2. Job Set-up Information______________________ Not Applicable
3. Fault Confirmation__________________
A. Test
Not applicable, it is not a fault.
4. Fault Isolation_______________
A. No maintenance action is required.
1
-EFF : ALL
-∞∞36-11-00∞∞∞∞∞∞∞∞∞∞Page A262
--Feb 01/05R ---CES -
Variation of the Bleed Pressure Indication for the Engine 1
1. Possible Causes_______________
-SOLENOID-BLEED PRESS REG V CTL, ENG 1 (10HA1)
-sense line
2. Job Set-up Information______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 36-11-00-720-007 Functional Test of the Sense Lines Upstream of the Bleed Pressure Regulator Valve (4001HA) and Connected to the Control Solenoid (10HA1,10HA2)
AMM 36-11-00-740-001 BITE Test of the BMC 1(2)
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)
3. Fault Confirmation__________________
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 PNEUMATIC(74)
