W DOC AIRBUS | TSM A320F

Engine 1 Bleed Pressure Sensor Drift Measurement


TASK 36-11-00-810-A14-A
Engine 1 Bleed Pressure Sensor Drift Measurement


1. Possible Causes
  • XDCR-BLEED REGULATED PRESS, ENG 1 [8HA1]
  • sense line
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 36-11-00-740-805
Drift Test of the Pressure Sensor
AMM 36-11-16-000-802
Removal of the Bleed Regulated Pressure-Transducer
AMM 36-11-16-400-802
Installation of the Bleed Regulated Pressure-Transducer
AMM 36-11-49-000-823
Removal of the Environmental Control System (ECS) Sense Lines
AMM 36-11-49-000-832
Removal of the Sense Lines of the Bleed Regulated Pressure-Transducer and the Bleed Transferred Pressure-Transducer
AMM 36-11-49-400-823
Installation of the Environmental Control System (ECS) Sense Lines
AMM 36-11-49-400-832
Installation of the Sense Lines of the Bleed Regulated Pressure-Transducer and the Bleed Transferred Pressure-Transducer
AMM 36-12-00-860-802
Pressurization of the Bleed System with the APU
AMM 36-12-00-860-803
Pressurization of the Bleed System through the HP Ground Connector
AMM 36-22-00-790-802
Leak Check on all the Bleed Air Ducts and Packs Components
3. Fault Confirmation
Subtask 36-11-00-740-108-A ** ON A/C NOT FOR ALL
A. Test
   (1) Pressurize the Bleed Air System AMM 36-12-00-860-802 or AMM 36-12-00-860-803
   (2) Do the Pressure Sensor Drift Test AMM 36-11-00-740-805.
4. Fault Isolation
Subtask 36-11-00-810-439-A ** ON A/C NOT FOR ALL
A. If the test shows the maintenance message:
DRIFT REG-PRESS XDCR (8HA1)/ SENSE LINE
   (1) Replace the XDCR-BLEED REGULATED PRESS, ENG 1 [8HA1] AMM 36-11-16-000-802 and AMM 36-11-16-400-802.
   (2) Do the test given in Para. 3.
Subtask 36-11-00-810-440-A ** ON A/C NOT FOR ALL
B. If the fault continues:
   (1) Replace the sense line of the bleed regulated pressure-transducer AMM 36-11-49-000-823 AMM 36-11-49-400-823 and AMM 36-11-49-000-832 AMM 36-11-49-400-832.
   (2) Do a leak check of the sense line AMM 36-22-00-790-802.
Subtask 36-11-00-710-644-A ** ON A/C NOT FOR ALL
C. Test
   (1) After the subsequent flight, make sure that the fault does not continue.
[Rev.8 from Aug 2018] 2026.04.04 04:33:55 UTC