Installation of the Pressure Regulating Valve
TASK 21-63-52-400-001-A
Installation of the Pressure Regulating Valve
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
C. Work Zones and Access Panels
D. Expendable Parts
E. Referenced Information
3. Job Set-up
Subtask 21-63-52-941-052-A
Subtask 21-63-52-420-053-B ** ON A/C NOT FOR ALL
Subtask 21-63-52-410-050-A
[Rev.10 from 2021]
2026.04.01 04:09:50 UTC
Installation of the Pressure Regulating Valve
WARNING:
MAKE SURE THAT AIR IS NOT SUPPLIED TO THE AIR CONDITIONING SYSTEM FROM THE MAIN ENGINE, THE APU OR A GROUND SOURCE.
HOT COMPRESSED AIR CAN CAUSE INJURY TO PERSONNEL.
WARNING:
MAKE SURE THAT THE COMPONENTS OF THE BLEED AIR SYSTEM ARE COOL. HOT COMPONENTS WILL BURN YOU.
WARNING:
MAKE SURE THAT THE PNEUMATIC SYSTEM IS DEPRESSURIZED BEFORE YOU START WORK. PRESSURIZED AIR CAN CAUSE INJURY TO PERSONNEL.
WARNING:
BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
CAUTION:
BE VERY CAREFUL WHEN YOU DO WORK ON OR NEAR THE AIR-CONDITIONING DUCTS. THE DUCTS ARE MADE OF THIN MATERIAL AND YOU CAN EASILY BREAK THEM.
CAUTION:
DO NOT PUT YOUR WEIGHT ON THE DUCTS. IT IS VERY EASY TO BREAK THEM.
FIN: 14HK
1. Reason for the JobSelf explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.08ABC1) | Aqueous Cleaner-Aircraft Exterior Pressure Spraying - |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 825 |
| FIG.ITEM | DESIGNATION | IPC-CSN |
|---|---|---|
| 25 | O-RINGS | AIPC 21-63-03-05-090 |
| 25 | SEAL | AIPC 21-63-83-01-170 |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 12-33-21-618-001-A-01 | Pre-conditioning through the HP Ground Connection |
| TASK 12-33-21-618-001-A-02 | Pre-conditioning with the APU |
| TASK 20-28-00-912-802-A | Electrical Bonding - General Maintenance Procedure |
| TASK 21-63-00-720-001-A | Functional Test of the Cockpit and Cabin Temperature Control without CFDS/MCDU. |
| 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 25-54-12-000-001-A | Removal of the Forward Cargo-Compartment Partition |
| TASK 25-54-12-400-001-A | Installation of the Forward Cargo-Compartment Partition |
| TASK 52-30-00-860-001-A | Open the FWD or Aft Cargo-Compartment Door with the Yellow Electric Pump |
| TASK 52-30-00-860-002-A | Close the FWD or Aft Cargo-Compartment Door with the Yellow Electric Pump |
| TASK 06-41-53-00 | FUSELAGE-DESCRIPTION AND OPERATION |
Subtask 21-63-52-941-052-A
A. Safety Precautions
(1) On the panel 30VU:
(a) Make sure that:
(2) On the HP and the LP ground connector put a warning notice in position to tell persons not to supply the ground air.
Subtask 21-63-52-860-050-A (1) On the panel 30VU:
(a) Make sure that:
- the APU BLEED pushbutton switch is in the off position (the ON legend is off) and,
- the ENG 1 BLEED and the ENG 2 BLEED pushbutton switches are in the off position (the OFF legends are on).
(2) On the HP and the LP ground connector put a warning notice in position to tell persons not to supply the ground air.
B. Aircraft Maintenance Configuration
(1) Make sure that:
(a) The aircraft electrical circuits are energized (Ref. AMM TASK 25-54-12-000-001).
(b) The ACCESS PLATFORM 2M (6 FT) is in position at the forward cargo-compartment door 825.
(c) The forward cargo-compartment door 825 is open (Ref. AMM TASK 52-30-00-860-001).
(d) The access panels at partition FR34 (Ref. AMM D/O 06-41-53-00) are removed (Ref. AMM TASK 25-54-12-000-001).
Subtask 21-63-52-865-051-A (1) Make sure that:
(a) The aircraft electrical circuits are energized (Ref. AMM TASK 25-54-12-000-001).
(b) The ACCESS PLATFORM 2M (6 FT) is in position at the forward cargo-compartment door 825.
(c) The forward cargo-compartment door 825 is open (Ref. AMM TASK 52-30-00-860-001).
(d) The access panels at partition FR34 (Ref. AMM D/O 06-41-53-00) are removed (Ref. AMM TASK 25-54-12-000-001).
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | AIR COND/TEMP CTL/SYS 1 CHAN B/28VDC | 52HH | D08 |
| ** ON A/C NOT FOR ALL | |||
| 122VU | AIR COND/ZONE TEMP CTL/28VDC/SYS2 | 4HK | V20 |
| 122VU | AIR COND/ZONE TEMP CTL/28VDC/SYS1 | 3HK | V19 |
| 122VU | AIR COND/ZONE TEMP CTL/115VAC/SYS2 | 2HK | V18 |
| 122VU | AIR COND/ZONE TEMP CTL/115VAC/SYS1 | 1HK | V17 |
| ** ON A/C NOT FOR ALL | |||
| 122VU | AIR COND/TEMP CTL SYS 2/CHAN A/115VAC | 53HH | W22 |
| 122VU | AIR COND/TEMP CTL SYS 2/CHAN A/28VDC | 55HH | W21 |
| 122VU | AIR COND/TEMP CTL SYS 1/CHAN A/115VAC | 49HH | X22 |
| 122VU | AIR COND/TEMP CTL SYS 1/CHAN A/28VDC | 51HH | X21 |
| 122VU | AIR COND/TEMP CTL SYS 2/CHAN B/28VDC | 56HH | Y21 |
| 122VU | AIR COND/TEMP CTL SYS 2/CHAN B/115VAC | 54HH | Y20 |
| 122VU | AIR COND/TEMP CTL SYS 1/CHAN B/115VAC | 50HH | Y18 |
Subtask 21-63-52-420-053-B ** ON A/C NOT FOR ALL
A. Installation of the Pressure Regulating Valve
(1) Remove the blanking plugs from the duct flanges (24) and (29), the duct assembly (27), and the pressure regulating valve (30).
(2) Clean the component interfaces and the adjacent area.
(3) Make sure that the parts retained from the removed component are clean and in the correct condition.
(4) Put a new AIPC 21-63-03-05-090 O-RINGS (25) and the pressure regulating valve (30) in position on the duct flange (24).
(5) Install the clamp (31).
(6) Do not fully tighten the bolt of the clamp (31) at this time.
Make sure that:
(8) Put the duct assembly (27) in position on the duct flange (29) and the pressure regulating valve (30).
(9) Install the clamps (26) and (28).
(10) Do not fully tighten the bolts of the clamps (26) and (28) at this time.
(11) Clean the control tubes (4) and (5):
(a) Remove the blanking plugs from the disconnected line ends.
(b) Clean the control tubes with Aqueous Cleaner-Aircraft Exterior Pressure Spraying - (Material No.08ABC1) .
(c) From the pressure regulating valve (30) position, blow clean, dry compressed air into the control tubes to remove any dust-like contamination or humidity.
(12) Make sure that the pressure regulating valve (30) is in the correct position and install the control tubes (4) and (5).
(13) Install the control tubes (4) to the check valves [7270HM] and [7272HM]
(14) TORQUE the bolts of the clamps (31) and (26) to between 0.546 and 0.491 m.daN (48.32 and 43.45 lbf.in )
.
(15) TORQUE the bolt of the clamp (28) to between 0.5 and 0.4 m.daN (44.25 and 35.40 lbf.in )
.
(16) Put the bonding strap (8) in position and install the washer (7), the screw (6), the washer (9) and the nut (10) (Ref. AMM TASK 20-28-00-912-802).
(17) Remove the blanking caps from the disconnected electrical connections.
(18) Make sure that all the electrical connections are clean and in the correct condition.
(20) Make sure that the work area is clean and clear of tools and other items.
Subtask 21-63-52-420-053-C ** ON A/C NOT FOR ALL (1) Remove the blanking plugs from the duct flanges (24) and (29), the duct assembly (27), and the pressure regulating valve (30).
(2) Clean the component interfaces and the adjacent area.
(3) Make sure that the parts retained from the removed component are clean and in the correct condition.
(4) Put a new AIPC 21-63-03-05-090 O-RINGS (25) and the pressure regulating valve (30) in position on the duct flange (24).
(5) Install the clamp (31).
(6) Do not fully tighten the bolt of the clamp (31) at this time.
Make sure that:
- the pressure regulating valve (30) faces in the correct direction.
- when you look in a rearwards direction the manual closure lever is in the 3 o'clock position.
(8) Put the duct assembly (27) in position on the duct flange (29) and the pressure regulating valve (30).
(9) Install the clamps (26) and (28).
(10) Do not fully tighten the bolts of the clamps (26) and (28) at this time.
(11) Clean the control tubes (4) and (5):
(a) Remove the blanking plugs from the disconnected line ends.
(b) Clean the control tubes with Aqueous Cleaner-Aircraft Exterior Pressure Spraying - (Material No.08ABC1) .
(c) From the pressure regulating valve (30) position, blow clean, dry compressed air into the control tubes to remove any dust-like contamination or humidity.
(12) Make sure that the pressure regulating valve (30) is in the correct position and install the control tubes (4) and (5).
(13) Install the control tubes (4) to the check valves [7270HM] and [7272HM]
(14) TORQUE the bolts of the clamps (31) and (26) to between 0.546 and 0.491 m.daN (48.32 and 43.45 lbf.in )
. (15) TORQUE the bolt of the clamp (28) to between 0.5 and 0.4 m.daN (44.25 and 35.40 lbf.in )
. (16) Put the bonding strap (8) in position and install the washer (7), the screw (6), the washer (9) and the nut (10) (Ref. AMM TASK 20-28-00-912-802).
(17) Remove the blanking caps from the disconnected electrical connections.
(18) Make sure that all the electrical connections are clean and in the correct condition.
CAUTION:
TO PREVENT POSSIBLE CROSS-CONNECTION OF THE ELECTRICAL CONNECTORS, MAKE SURE THAT PLUGS AND RECEPTACLES ARE CLEARLY IDENTIFIED.
(19) Connect the electrical connectors (1), (2) and (3). receptacles. (20) Make sure that the work area is clean and clear of tools and other items.
A. Installation of the Pressure Regulating Valve
(1) Remove the blanking plugs from the duct flanges (24) and (29), the duct assembly (27), and the pressure regulating valve (30).
(2) Clean the component interfaces and the adjacent area.
(3) Make sure that the parts retained from the removed component are clean and in the correct condition.
(4) Put a new AIPC 21-63-03-05-090 O-RINGS (25) or AIPC 21-63-83-01-170 SEAL (25) and the pressure regulating valve (30) in position on the duct flange (24).
(5) Install the clamp (31).
(6) Do not fully tighten the bolt of the clamp (31) at this time.
Make sure that:
(8) Put the duct assembly (27) in position on the duct flange (29) and the pressure regulating valve (30).
(9) Install the clamps (26) and (28).
(10) Do not fully tighten the bolts of the clamps (26) and (28) at this time.
(a) Remove the blanking plugs from the disconnected line ends.
(b) Clean the control tubes with Aqueous Cleaner-Aircraft Exterior Pressure Spraying - (Material No.08ABC1) .
(c) From the pressure regulating valve (30) position, blow clean, dry compressed air into the control tubes to remove any dust-like contamination or humidity.
(12) Make sure that the pressure regulating valve (30) is in the correct position and install the control tubes (4) and (3).
(13) Install the control tube (4) to the check valves [7270HM] and [7272HM]
(14) TORQUE the bolts of the clamps (31) and (26) to between 0.546 and 0.491 m.daN (48.32 and 43.45 lbf.in )
.
(15) TORQUE the bolt of the clamp (28) to between 0.5 and 0.4 m.daN (44.25 and 35.40 lbf.in )
.
(16) Put the bonding strap (7) in position and install the washer (6), the screw (5), the washer (8) and the nut (9) (Ref. AMM TASK 20-28-00-912-802).
(17) Remove the blanking caps from the disconnected electrical connections.
(18) Make sure that all the electrical connections are clean and in the correct condition.
Subtask 21-63-52-865-053-A (1) Remove the blanking plugs from the duct flanges (24) and (29), the duct assembly (27), and the pressure regulating valve (30).
(2) Clean the component interfaces and the adjacent area.
(3) Make sure that the parts retained from the removed component are clean and in the correct condition.
(4) Put a new AIPC 21-63-03-05-090 O-RINGS (25) or AIPC 21-63-83-01-170 SEAL (25) and the pressure regulating valve (30) in position on the duct flange (24).
(5) Install the clamp (31).
(6) Do not fully tighten the bolt of the clamp (31) at this time.
Make sure that:
- the pressure regulating valve (30) faces in the correct direction.
- when you look in a rearwards direction the manual closure lever is in the 3 o'clock position.
NOTE: For pressure regulating valve (30) P/N 70853A01xxxx only, make sure that:
(7) Put a new packing (25) in position on the pressure regulating valve (30). - the clamp (31) bolt is horizontal in the 6 o' clock position.
(8) Put the duct assembly (27) in position on the duct flange (29) and the pressure regulating valve (30).
(9) Install the clamps (26) and (28).
(10) Do not fully tighten the bolts of the clamps (26) and (28) at this time.
NOTE: For pressure regulating valve (30) P/N 70853A01xxxx only, make sure that:
(11) Clean the control tubes (4) and (3): - the clamp (26) bolt is horizontal in the 6 o' clock position.
(a) Remove the blanking plugs from the disconnected line ends.
(b) Clean the control tubes with Aqueous Cleaner-Aircraft Exterior Pressure Spraying - (Material No.08ABC1) .
(c) From the pressure regulating valve (30) position, blow clean, dry compressed air into the control tubes to remove any dust-like contamination or humidity.
(12) Make sure that the pressure regulating valve (30) is in the correct position and install the control tubes (4) and (3).
(13) Install the control tube (4) to the check valves [7270HM] and [7272HM]
(14) TORQUE the bolts of the clamps (31) and (26) to between 0.546 and 0.491 m.daN (48.32 and 43.45 lbf.in )
. (15) TORQUE the bolt of the clamp (28) to between 0.5 and 0.4 m.daN (44.25 and 35.40 lbf.in )
. (16) Put the bonding strap (7) in position and install the washer (6), the screw (5), the washer (8) and the nut (9) (Ref. AMM TASK 20-28-00-912-802).
(17) Remove the blanking caps from the disconnected electrical connections.
(18) Make sure that all the electrical connections are clean and in the correct condition.
CAUTION:
TO PREVENT POSSIBLE CROSS-CONNECTION OF THE ELECTRICAL CONNECTORS, MAKE SURE THAT PLUGS AND RECEPTACLES ARE CLEARLY IDENTIFIED.
(19) Connect the electrical connectors (1) and (2). receptacles. NOTE: For pressure regulating valve (30) P/N 746A0000-XX make sure that: the third receptacle must be left blank with its blanking cap on it.
(20) Make sure that the work area is clean and clear of tools and other items.B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 21-63-52-710-050-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | AIR COND/TEMP CTL/SYS 1 CHAN B/28VDC | 52HH | D08 |
| ** ON A/C NOT FOR ALL | |||
| 122VU | AIR COND/ZONE TEMP CTL/28VDC/SYS2 | 4HK | V20 |
| 122VU | AIR COND/ZONE TEMP CTL/28VDC/SYS1 | 3HK | V19 |
| 122VU | AIR COND/ZONE TEMP CTL/115VAC/SYS2 | 2HK | V18 |
| 122VU | AIR COND/ZONE TEMP CTL/115VAC/SYS1 | 1HK | V17 |
| ** ON A/C NOT FOR ALL | |||
| 122VU | AIR COND/TEMP CTL SYS 2/CHAN A/115VAC | 53HH | W22 |
| 122VU | AIR COND/TEMP CTL SYS 2/CHAN A/28VDC | 55HH | W21 |
| 122VU | AIR COND/TEMP CTL SYS 1/CHAN A/115VAC | 49HH | X22 |
| 122VU | AIR COND/TEMP CTL SYS 1/CHAN A/28VDC | 51HH | X21 |
| 122VU | AIR COND/TEMP CTL SYS 2/CHAN B/28VDC | 56HH | Y21 |
| 122VU | AIR COND/TEMP CTL SYS 2/CHAN B/115VAC | 54HH | Y20 |
| 122VU | AIR COND/TEMP CTL SYS 1/CHAN B/115VAC | 50HH | Y18 |
C. Test
(1) Do the pre-conditioning through the HP ground connector or with the APU (Ref. AMM TASK 12-33-21-618-001) (Ref. AMM TASK 12-33-21-618-001).
(2) Do a leak check of the pressure regulating valve (30) connections.
(3) Make sure that there are no leaks.
(4) After approximately 15 minutes stop the pre-conditioning (Ref. AMM TASK 12-33-21-618-001) (Ref. AMM TASK 12-33-21-618-001).
(5) Do the functional test of the cockpit and cabin temperature control system (Ref. AMM TASK 21-63-00-720-001).
5. Close-up(1) Do the pre-conditioning through the HP ground connector or with the APU (Ref. AMM TASK 12-33-21-618-001) (Ref. AMM TASK 12-33-21-618-001).
(2) Do a leak check of the pressure regulating valve (30) connections.
(3) Make sure that there are no leaks.
(4) After approximately 15 minutes stop the pre-conditioning (Ref. AMM TASK 12-33-21-618-001) (Ref. AMM TASK 12-33-21-618-001).
(5) Do the functional test of the cockpit and cabin temperature control system (Ref. AMM TASK 21-63-00-720-001).
Subtask 21-63-52-410-050-A
A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the access panels at partition FR34 (Ref. AMM D/O 06-41-53-00) (Ref. AMM TASK 25-54-12-400-001).
(3) Close the forward cargo-compartment door 825 (Ref. AMM TASK 52-30-00-860-002).
(4) Remove the access platform(s).
Subtask 21-63-52-862-050-A (1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the access panels at partition FR34 (Ref. AMM D/O 06-41-53-00) (Ref. AMM TASK 25-54-12-400-001).
(3) Close the forward cargo-compartment door 825 (Ref. AMM TASK 52-30-00-860-002).
(4) Remove the access platform(s).
Pressure Regulating Valve