Pressurization of the Bleed System through the HP Ground Connector
TASK 36-12-00-860-803-A
Pressurization of the Bleed System through the HP Ground Connector
1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Work Zones and Access Panels
C. Referenced Information
3. Job Set-up
Subtask 36-12-00-941-054-A ** ON A/C NOT FOR ALL
Subtask 36-12-00-860-075-A ** ON A/C NOT FOR ALL
Subtask 36-12-00-410-058-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 04:52:50 UTC
Pressurization of the Bleed System through the HP Ground Connector
1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | 1 | GROUND AIR-SUPPLY UNIT(HIGH PRESSURE) |
| No specific | 1 | WARNING NOTICE(S) |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 191DB, 811 |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 24-41-00-861-002-A | Energize the Aircraft Electrical Circuits from the External Power |
| TASK 24-41-00-861-002-A-01 | Energize the Aircraft Electrical Circuits from the APU |
| TASK 24-41-00-861-002-A-02 | Energize the Aircraft Electrical Circuits from Engine 1(2) |
| TASK 24-41-00-862-002-A | De-energize the Aircraft Electrical Circuits Supplied from the External Power |
| TASK 24-41-00-862-002-A-01 | De-energize the Aircraft Electrical Circuits Supplied from the APU |
| TASK 24-41-00-862-002-A-02 | De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2) |
| TASK 31-60-00-860-001-A | EIS Start Procedure |
| TASK 31-60-00-860-002-A | EIS Stop Procedure |
| TASK 52-41-00-010-002-A | Open the Avionics Compartment Doors for Access |
| TASK 52-41-00-410-002-A | Close the Avionics Compartment Doors after Access |
Subtask 36-12-00-941-054-A ** ON A/C NOT FOR ALL
A. Safety Precautions
(2) Install a WARNING NOTICE(S) on the access door 811 to tell persons not to close the access door 811.
Subtask 36-12-00-860-074-A ** ON A/C NOT FOR ALL WARNING:
MAKE SURE THAT THE FWD AVIONICS ACCESS DOOR 811 IS OPEN WITH A WARNING PLACARD ATTACHED TO IT.
THE WARNING NOTICE MUST TELL PERSONS NOT TO CLOSE THE DOOR. THIS PREVENTS ACCIDENTAL PRESSURIZATION OF THE AIRCRAFT.
(1) When you operate the air conditioning make sure that the access door 811 is open (Ref. AMM TASK 52-41-00-010-002). (2) Install a WARNING NOTICE(S) on the access door 811 to tell persons not to close the access door 811.
B. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(3) On AIR COND overhead panel 30VU:
Subtask 36-12-00-865-066-A ** ON A/C NOT FOR ALL (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(3) On AIR COND overhead panel 30VU:
- Release the PACK 1 and PACK 2 P/BSWs (the OFF legends come on).
- Make sure that the X-bleed selector switch is in the AUTO position.
C. Make sure that this(these) circuit breaker(s) is(are) closed:
Subtask 36-12-00-010-058-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 121VU | APU/APU/CTL | 2KD | L42 |
| 121VU | APU/ECB/SPLY | 1KD | L41 |
| 122VU | AIR BLEED/X FEED VALVE/NORM | 1HV | Z20 |
D. Get Access
(1) Open the access door 191DB.
(2) Connect the GROUND AIR-SUPPLY UNIT(HIGH PRESSURE) to the aircraft HP Ground Connector (7300HM).
4. Procedure(1) Open the access door 191DB.
(2) Connect the GROUND AIR-SUPPLY UNIT(HIGH PRESSURE) to the aircraft HP Ground Connector (7300HM).
Subtask 36-12-00-860-075-A ** ON A/C NOT FOR ALL
A. Pressurization of the Bleed System through the HP Ground Connector
(1) Start the ground air-supply unit and make sure that:
(3) On the AIR BLEED page of the ECAM lower DU, make sure that all the shown indications are normal (i.e. green indication).
(4) When the pressurization of the bleed system is not necessary, stop the air supply.
5. Close-up(1) Start the ground air-supply unit and make sure that:
- The airflow is between 54 kg.min (119.0496 lb.min) and 78 kg.min (171.9605 lb.min).
- The supplied air pressure is not more than 60 psi (4.14 bar).
- The supplied air temperature is not more than 260 deg.C (500.00 deg.F).
(3) On the AIR BLEED page of the ECAM lower DU, make sure that all the shown indications are normal (i.e. green indication).
(4) When the pressurization of the bleed system is not necessary, stop the air supply.
Subtask 36-12-00-410-058-A ** ON A/C NOT FOR ALL
A. Close Access
(1) Disconnect the GROUND AIR-SUPPLY UNIT(HIGH PRESSURE) from the aircraft HP Ground Connector (7300HM).
(2) Close the access door 191DB.
Subtask 36-12-00-860-076-A ** ON A/C NOT FOR ALL (1) Disconnect the GROUND AIR-SUPPLY UNIT(HIGH PRESSURE) from the aircraft HP Ground Connector (7300HM).
(2) Close the access door 191DB.
B. Aircraft Maintenance Configuration
(1) On the AIR COND overhead panel 30VU:
(3) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
Subtask 36-12-00-942-054-A ** ON A/C NOT FOR ALL (1) On the AIR COND overhead panel 30VU:
- Push the PACK 1 and PACK 2 P/BSWs (the OFF legends go off)
- Make sure that the X-bleed selector switch is in the AUTO position.
(3) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
C. Put the aircraft back to its initial configuration.
(1) Remove the WARNING NOTICE(S).
(2) Close the access door 811 (Ref. AMM TASK 52-41-00-410-002).
(3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(1) Remove the WARNING NOTICE(S).
(2) Close the access door 811 (Ref. AMM TASK 52-41-00-410-002).
(3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.