Pre-conditioning through the LP Ground Connection (Aircraft Electrical Power Available)
TASK 12-33-21-618-001-A
Pre-conditioning through the LP Ground Connection (Aircraft Electrical Power Available)
There are alternative methods for the pre-conditioning. This task gives one of the methods. For the other methods, refer to the related tasks in this page block.
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 12-33-21-861-052-A
Subtask 12-33-21-618-073-A
Subtask 12-33-21-410-050-A
[Rev.10 from 2021]
2026.03.31 22:58:12 UTC
Pre-conditioning through the LP Ground Connection (Aircraft Electrical Power Available)
WARNING:
MAKE SURE THAT DURING THIS PROCEDURE THE AIRCRAFT IS IN ONE OF THESE THREE CONDITIONS:
- THE CABIN PRESSURE OUTFLOW VALVE IS OPEN.
- THE FWD AVIONICS COMPARTMENT ACCESS DOOR 811 IS OPEN.
- ONE OR MORE PASSENGER DOORS ARE OPEN.
CAUTION:
MAKE SURE THAT:
- THE OUTLET TEMPERATURE OF THE GROUND AIR SUPPLY UNIT IS MINIMUM 2.0 DEG. C (35.6 DEG. F)
- THE STATIC PRESSURE AT THE AIRCRAFT CONNECTOR IS LESS THAN 40 MBAR (0.58 PSI).
CAUTION:
DO NOT USE CONDITIONED AIR FROM THE APU OR HIGH-PRESSURE GROUND UNIT AT THE SAME TIME AS AIR FROM THE LOW-PRESSURE GROUND UNIT. IF YOU DO NOT OBEY THIS PRECAUTION, DAMAGE TO THE CHECK VALVES OR THE AIRCRAFT CAN OCCUR.
CAUTION:
MAKE SURE THAT THE GROUND AIR-SUPPLY UNIT IS NOT TOO NEAR THE AIRCRAFT AND THAT THE ENGINE EXHAUST PIPE OF THE GROUND AIR- SUPPLY UNIT POINTS AWAY FROM THE AIRCRAFT. HEAT FROM THIS UNIT AND FROM THE EXHAUST CAN CAUSE DAMAGE TO THE AIRCRAFT STRUCTURE.
1. Reason for the JobThere are alternative methods for the pre-conditioning. This task gives one of the methods. For the other methods, refer to the related tasks in this page block.
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | 1 | ACCESS PLATFORM 2M (6 FT) |
| No specific | 1 | GROUND AIR-SUPPLY UNIT(LOW PRESSURE) |
| No specific | AR | WARNING NOTICE(S) |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 121 | AVIONICS COMPARTMENT |
| 191 | AIR CONDITIONING COMPT AND FAIRINGS |
| 191CB, 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 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 12-33-21-861-052-A
A. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
Subtask 12-33-21-010-050-A (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
B. Get Access
(1) Open access door 191CB.
(2) Connect the GROUND AIR-SUPPLY UNIT(LOW PRESSURE) to the aircraft LP connector.
Subtask 12-33-21-941-052-A (1) Open access door 191CB.
(2) Connect the GROUND AIR-SUPPLY UNIT(LOW PRESSURE) to the aircraft LP connector.
C. Safety Precautions
(1) Do one of the safety precautions that follow:
(a) Make sure that the cabin pressure Outflow Valve (OFV) is open:
1 On the overhead panel, on the CABIN PRESS section of control panel 25VU:
1 Put the ACCESS PLATFORM 2M (6 FT) in position below forward-avionics-compartment access door 811.
2 Open forward-avionics-compartment access door 811 (Ref. AMM TASK 52-41-00-010-002).
(c) Make sure that a minimum of one passenger/crew door is in good condition and in the open position:
1 Put the WARNING NOTICE(S) in position to tell persons not to close the passenger/crew door.
(2) Make sure that the APU BLEED AIR does not operate:
(a) Put the WARNING NOTICE(S) in position of the APU BLEED AIR to tell persons not to operate the APU BLEED AIR.
(3) If the LP ground-air-supply flow is more than 60 kg.min (132.28 lb.min):
(a) On the VENTILATION section of panel 22VU:
4. Procedure(1) Do one of the safety precautions that follow:
(a) Make sure that the cabin pressure Outflow Valve (OFV) is open:
1 On the overhead panel, on the CABIN PRESS section of control panel 25VU:
- Put the WARNING NOTICE(S) in position to tell persons not to close the OFV.
1 Put the ACCESS PLATFORM 2M (6 FT) in position below forward-avionics-compartment access door 811.
2 Open forward-avionics-compartment access door 811 (Ref. AMM TASK 52-41-00-010-002).
(c) Make sure that a minimum of one passenger/crew door is in good condition and in the open position:
1 Put the WARNING NOTICE(S) in position to tell persons not to close the passenger/crew door.
(2) Make sure that the APU BLEED AIR does not operate:
(a) Put the WARNING NOTICE(S) in position of the APU BLEED AIR to tell persons not to operate the APU BLEED AIR.
(3) If the LP ground-air-supply flow is more than 60 kg.min (132.28 lb.min):
(a) On the VENTILATION section of panel 22VU:
- Release the CAB FANS pushbutton switch (the OFF legend comes on).
Subtask 12-33-21-618-073-A
A. Pre-conditioning through the LP Ground Connection (Aircraft Electrical Power Available)
(1) Obey the instructions given in the ground-air supply unit.
(2) Start the ground air-supply unit, and make sure that:
(a) The airflow is not more than 78 kg.min (171.96 lb.min).
(b) The supplied air pressure is not more than 40 mbar (0.58 psi) at the aircraft interface connector.
(3) Set the necessary output air temperature on the ground air-supply unit, and make sure that:
(a) The supplied air temperature does not increase to more than 70 DEG.C (158 DEG.F).
(b) The supplied air temperature does not decrease to less than 2 DEG.C (35.6 DEG.F).
(4) When the pre-conditioning is not necessary, stop the GROUND AIR-SUPPLY UNIT(LOW PRESSURE):
(a) Obey the instructions given in the ground-air supply unit.
5. Close-up(1) Obey the instructions given in the ground-air supply unit.
(2) Start the ground air-supply unit, and make sure that:
(a) The airflow is not more than 78 kg.min (171.96 lb.min).
(b) The supplied air pressure is not more than 40 mbar (0.58 psi) at the aircraft interface connector.
(3) Set the necessary output air temperature on the ground air-supply unit, and make sure that:
(a) The supplied air temperature does not increase to more than 70 DEG.C (158 DEG.F).
(b) The supplied air temperature does not decrease to less than 2 DEG.C (35.6 DEG.F).
(4) When the pre-conditioning is not necessary, stop the GROUND AIR-SUPPLY UNIT(LOW PRESSURE):
(a) Obey the instructions given in the ground-air supply unit.
Subtask 12-33-21-410-050-A
A. Close Access
(1) Disconnect and remove the GROUND AIR-SUPPLY UNIT(LOW PRESSURE) from the aircraft LP connector.
(2) Close access door 191CB.
(3) On the VENTILATION section of panel 22VU:
(5) Remove the WARNING NOTICE(S).
(6) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(7) If opened, close the passenger/crew door.
Subtask 12-33-21-862-052-A (1) Disconnect and remove the GROUND AIR-SUPPLY UNIT(LOW PRESSURE) from the aircraft LP connector.
(2) Close access door 191CB.
(3) On the VENTILATION section of panel 22VU:
- Push the CAB FANS pushbutton switch.
(5) Remove the WARNING NOTICE(S).
(6) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(7) If opened, close the passenger/crew door.
B. Put the aircraft back to its initial configuration.
(1) De-energize the aircraft electrical circuit (Ref. AMM TASK 24-41-00-862-002).
(1) De-energize the aircraft electrical circuit (Ref. AMM TASK 24-41-00-862-002).
LP and HP Ground Connectors