Underpressure Fault
TASK 21-58-00-810-816-A
Underpressure Fault
1. Possible Causes
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
C. Referenced Information
3. Fault Confirmation
Subtask 21-58-00-810-076-B ** ON A/C NOT FOR ALL
Subtask 21-58-00-810-088-A ** ON A/C NOT FOR ALL
[Rev.8 from Aug 2018]
2026.04.04 04:24:50 UTC
Underpressure Fault
1. Possible Causes
- SENSOR-PRESS,CSAS [117HW]
- VALVE-ISOLATION,CSAS [111HW]
- wiring
- OZONE CONVERTER-ASSY,CSAS [5101HM]
- EXCHANGER-HEAT,CSAS [5103HM]
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | 1 | WATER - SOAPY SOLUTION |
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.14CCB6) | Testing Medium-Leak Detection - Oxygen System |
| REFERENCE | DESIGNATION |
|---|---|
| ASM 215301 | |
| AMM 21-58-00-710-002 | Operational Test of the Conditioned Service Air System with Bleed Air |
| AMM 21-58-12-000-001 | Removal of the Pressure Sensor |
| AMM 21-58-12-400-001 | Installation of the Pressure Sensor |
| AMM 21-58-41-000-001 | Removal of the CSAS Heat Exchanger |
| AMM 21-58-41-400-001 | Installation of the CSAS Heat Exchanger |
| AMM 21-58-42-000-001 | Removal of the Ozone Converter Assy |
| AMM 21-58-42-400-001 | Installation of the Ozone Converter Assy |
| AMM 21-58-51-000-001 | Removal of the CSAS Isolation Valve |
| AMM 21-58-51-400-001 | Installation of the CSAS Isolation Valve |
Subtask 21-58-00-810-076-B ** ON A/C NOT FOR ALL
A. Access
(1) Get access to the components and ducts of the conditioned service air system (CSAS).
Subtask 21-58-00-710-080-B ** ON A/C NOT FOR ALL (1) Get access to the components and ducts of the conditioned service air system (CSAS).
B. Test.
(1) Apply a solution of Testing Medium-Leak Detection - Oxygen System (Material No.14CCB6) or WATER - SOAPY SOLUTION to all components and ducts of the conditioned service air system to search for a leak.
(2) Do the operational test of the conditioned service air system with bleed air AMM 21-58-00-710-002.
(3) Leak Check
4. Fault Isolation(1) Apply a solution of Testing Medium-Leak Detection - Oxygen System (Material No.14CCB6) or WATER - SOAPY SOLUTION to all components and ducts of the conditioned service air system to search for a leak.
(2) Do the operational test of the conditioned service air system with bleed air AMM 21-58-00-710-002.
(3) Leak Check
- Do a check for leakages at all components and ducts of the conditioned service air system while and immediately after the system test with bleed.
Subtask 21-58-00-810-088-A ** ON A/C NOT FOR ALL
A. If a leakage is found:
Subtask 21-58-00-810-097-B ** ON A/C NOT FOR ALL - remove the leakage by replacement of the faulty component if necessary.
B. If the test gives no failure message and no leakage at CSAS was found, no further trouble shooting is necessary.
(1) If the fault continues:
replace the SENSOR-PRESS,CSAS [117HW] AMM 21-58-12-000-001 AMM 21-58-12-400-001.
Subtask 21-58-00-810-090-B ** ON A/C NOT FOR ALL (1) If the fault continues:
replace the SENSOR-PRESS,CSAS [117HW] AMM 21-58-12-000-001 AMM 21-58-12-400-001.
C. If the test gives a different maintenance message, do the related trouble shooting procedure.
Subtask 21-58-00-810-077-B ** ON A/C NOT FOR ALL D. If the test gives the maintenance message UNDERPRESS and no leakage was found:
Subtask 21-58-00-710-081-A ** ON A/C NOT FOR ALL - replace the VALVE-ISOLATION,CSAS [111HW] AMM 21-58-51-000-001 and AMM 21-58-51-400-001.
- do a check and repair the wiring from:
- the CSAS ISOLATION VALVE (111HW) AA to the CSAS CONTROL UNIT (100HW) AB/5A,
- the CSAS ISOLATION VALVE (111HW) AH to the CSAS CONTROL UNIT (100HW) AB/8A and,
- the CSAS ISOLATION VALVE (111HW) to ground ASM 215301.
- replace the OZONE CONVERTER-ASSY,CSAS [5101HM] AMM 21-58-42-000-001 and AMM 21-58-42-400-001.
- remove the Inlet Duct and Outlet Duct of the TCM (110HW).
- do a visual inspection of the ducts and of the inside of the Heat Exchanger (5103HM).
- replace the EXCHANGER-HEAT,CSAS [5103HM] AMM 21-58-41-000-001 and AMM 21-58-41-400-001.
- do a check for leakages at all components and ducts of the fuel tank inerting system.
E. Do the test as given in the Para. 3.B.