-∞∞36-11-00∞∞∞∞∞∞∞∞∞∞Page 249
--Aug 01/05 ---CES - Shift of Calibration of the Bleed Regulated-Pressure Transducer of the Engine 2
1. Possible Causes
_______________
-XDCR-BLEED REGULATED PRESS, ENG 2 (8HA2)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 36-11-16-000-001 Removal of the Bleed Regulated Pressure Transducer (8HA1,8HA2) AMM 36-11-16-400-001 Installation of the Bleed Regulated Pressure Transducer (8HA1,8HA2)
3. Fault Confirmation
__________________
A. Not applicable.
4. Fault Isolation
_______________
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-228, 301-302,
A. If the fault symptom is identified by the Class 3 maintenance message: 36-11-16 DRIFT REG-PRESS XDCR 8HA2
-replace the XDCR-BLEED REGULATED PRESS, ENG 2 (8HA2) (Ref. AMM TASK 36-11-16-000-001) and (Ref. AMM TASK 36-11-16-400-001).
R **ON A/C 106-149, 229-299, 303-399, 401-499,
A. If the fault symptom is identified by the maintenance message REG PRESS XDCR 8HA2:
-replace the XDCR-BLEED REGULATED PRESS, ENG 2 (8HA2) (Ref. AMM TASK 36-11-16-000-001) and (Ref. AMM TASK 36-11-16-400-001).
**ON A/C ALL
B. After the subsequent flight, make sure that the fault does not continue.
1 -EFF : ALL
-∞∞36-11-00∞∞∞∞∞∞∞∞∞∞Page 250
--Aug 01/05 ---CES - Loss of One Sensing Element of the Exchanger Outlet Temperature-Sensor of the Engine 1
1. Possible Causes
_______________
-SENSOR-EXCHANGER OUT TEMP, ENG 1 (6HA1)
-BMC-1 (1HA1)
-
wiring between pin A/1 of the exchanger outlet temperature-sensor (6HA1) and th ground terminal
-
wiring from the exchanger outlet temperature-sensor (6HA1) to the BMC1 (1HA1)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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) ASM 36-11/01
3. Fault Confirmation
__________________
A. Test.
(1) Not applicable, the fault is evident.
4. Fault Isolation
_______________
A. If the fault symptom is identified by the maintenance message:
TEMP SENSOR 6HA1
-replace the SENSOR-EXCHANGER OUT TEMP, ENG 1 (6HA1) (Ref. AMM TASK 36-11-17-000-001) and (Ref. AMM TASK 36-11-17-400-001).
(1) If the fault continues:
-do a check for ground at pin A/1 of the exchanger outlet temperature-sensor (6HA1).
(a) If there is no ground:
-do a check and repair the wiring between pin A/1 of the exchanger outlet temperature-sensor (6HA1) and th ground terminal (Ref. ASM 36-11/01).
1
-EFF : ALL
-∞∞36-11-00∞∞∞∞∞∞∞∞∞∞Page 251
--Feb 01/05R ---CES -
(b) If there is ground:
-do a check and repair the wiring from the exchanger outlet temperature-sensor (6HA1) to the BMC1 (1HA1), pins A/2 and A/4 to pins AA/9B and AA/10B.
(2) If the fault continues:
-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
-EFF : ALL
-∞∞36-11-00∞∞∞∞∞∞∞∞∞∞Page 252
--Feb 01/05R ---CES -
Loss of One Sensing Element of the Exchanger Outlet Temperature-Sensor of the Engine 2
1. Possible Causes
_______________
-SENSOR-EXCHANGER OUT TEMP, ENG 2 (6HA2)
-BMC-2 (1HA2)
-
wiring between pin A/1 of the exchanger outlet temperature-sensor (6HA2) and the ground terminal
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320 Trouble Shooting Manual 排故手册 PNEUMATIC(36)
