W DOC AIRBUS | AMM A320F

Installation of the Trim Air Valve


TASK 21-63-51-400-001-A
Installation of the Trim Air 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.
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.
FIN: 11HK
FIN: 12HK
FIN: 13HK
1. Reason for the Job

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
WARNING NOTICE(S)
FOR [11HK] (TRIM VALVE CKPT)
No specific
Torque wrench: range to between 0.546 and 0.491 m.daN (48.32 and 43.45 lbf.in ) T
FOR [12HK] (TRIM VALVE FWD CAB)
No specific
Torque wrench: range to between 0.546 and 0.491 m.daN (48.32 and 43.45 lbf.in ) T
FOR [13HK] (TRIM VALVE AFT CAB)
No specific
Torque wrench: range to between 0.546 and 0.491 m.daN (48.32 and 43.45 lbf.in ) T
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
191CB, 191DB, 825
 C. Expendable Parts
FIG.ITEM
DESIGNATION
IPC-CSN
FOR [11HK] (TRIM VALVE CKPT)
15
SEAL
AIPC 21-63-03-07-100
10
INSULATION
AIPC 21-63-03-07-180
1
TIE-CABLE
AIPC 21-63-03-07-190
15
SEAL
AIPC 21-63-83-01-340
1
TIE-CABLE
AIPC 21-63-83-03-010
10
BLANKET-INSULATION
AIPC 21-63-83-03-020
FOR [12HK] (TRIM VALVE FWD CAB)
15
SEAL
AIPC 21-63-03-07-100
3
INSULATION
AIPC 21-63-03-07-170
1
TIE-CABLE
AIPC 21-63-03-07-190
15
SEAL
AIPC 21-63-83-01-340
1
TIE-CABLE
AIPC 21-63-83-03-010
3
BLANKET-INSULATION
AIPC 21-63-83-03-070
FOR [13HK] (TRIM VALVE AFT CAB)
15
SEAL
AIPC 21-63-03-07-100
2
BLANKET-INSULATION
AIPC 21-63-03-07-160
1
TIE-CABLE
AIPC 21-63-03-07-190
15
SEAL
AIPC 21-63-83-01-340
1
TIE-CABLE
AIPC 21-63-83-03-010
2
BLANKET-INSULATION
AIPC 21-63-83-03-180
 D. Referenced Information
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 21-63-00-710-004-A
Operational Test of the Cockpit and Cabin Temperature Control with CFDS/MCDU
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 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
F Trim Air Valve ** ON A/C NOT FOR ALL
F Trim Air Valve ** ON A/C NOT FOR ALL
FOR [11HK] (TRIM VALVE CKPT)
TASK 20-28-00-912-802-A
Electrical Bonding - General Maintenance Procedure
FOR [12HK] (TRIM VALVE FWD CAB)
TASK 20-28-00-912-802-A
Electrical Bonding - General Maintenance Procedure
FOR [13HK] (TRIM VALVE AFT CAB)
TASK 20-28-00-912-802-A
Electrical Bonding - General Maintenance Procedure
3. Job Set-up
Subtask 21-63-51-860-050-A
A. Aircraft Maintenance Configuration
   (1) Make sure that the aircraft electrical circuits are energized
(Ref. AMM TASK 24-41-00-861-002).
   (2) In the cockpit, on AIR COND panel 30VU:
     (a) Make sure that the APU BLEED pushbutton switch is released (the OFF legend is on).
     (b) Make sure that the ENG 1 BLEED and the ENG 2 BLEED pushbutton switches are released (the OFF legends are on).
     (c) Make sure that the PACK 1 and the PACK 2 pushbutton switches are released (the OFF legends are on).
     (d) Make sure that the HOT AIR pushbutton switch is released (the OFF legend is on).
     (e) Make sure that the WARNING NOTICE(S) is (are) in position to tell persons not to operate these pushbutton switches.
   (3) At access doors 191CB and 191DB:
     (a) On the LP and the HP ground connectors, make sure that the WARNING NOTICE(S) is (are) in position to tell persons not to supply the ground air.
   (4) Make sure that forward cargo-compartment door 825 is open (Ref. AMM TASK 52-30-00-860-001).
   (5) Make sure that the ACCESS PLATFORM 2M (6 FT) is in position at forward cargo-compartment door 825.
   (6) Make sure that the access panels at partition FR 34 are removed (Ref. AMM TASK 25-54-12-000-001).
Subtask 21-63-51-865-051-A
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUAIR COND/TEMP CTL/SYS 1 CHAN B/28VDC52HHD08
** ON A/C NOT FOR ALL
122VUAIR COND/ZONE TEMP CTL/28VDC/SYS24HKV20
122VUAIR COND/ZONE TEMP CTL/28VDC/SYS13HKV19
122VUAIR COND/ZONE TEMP CTL/115VAC/SYS22HKV18
122VUAIR COND/ZONE TEMP CTL/115VAC/SYS11HKV17
** ON A/C NOT FOR ALL
122VUAIR COND/TEMP CTL SYS 2/CHAN A/115VAC53HHW22
122VUAIR COND/TEMP CTL SYS 2/CHAN A/28VDC55HHW21
122VUAIR COND/TEMP CTL SYS 1/CHAN A/115VAC49HHX22
122VUAIR COND/TEMP CTL SYS 1/CHAN A/28VDC51HHX21
122VUAIR COND/TEMP CTL SYS 2/CHAN B/28VDC56HHY21
122VUAIR COND/TEMP CTL SYS 2/CHAN B/115VAC54HHY20
122VUAIR COND/TEMP CTL SYS 1/CHAN B/115VAC50HHY18
4. Procedure
Subtask 21-63-51-420-050-B
A. Installation of the Trim Air Valve
CAUTION: DURING INSTALLATION, MAKE SURE THAT THE CLAMP FASTENERS ARE NOT DIRECTLY ABOVE OR BELOW THE VALVE POSITION INDICATOR. THE VALVE POSITION INDICATOR MUST MOVE FREELY. IF IT TOUCHES A CLAMP FASTENER, THE TRIM-AIR VALVE WILL NOT OPERATE CORRECTLY.
   (1) FOR [11HK] (TRIM VALVE CKPT)
     (a) Remove the blanking plugs from the duct flange (17), the trim air valve (8) and the duct assembly (11),
     (b) Clean the component interfaces and the adjacent area.
     (c) Make sure that the parts retained from the removed component are clean and in the correct condition.
     (d) Make sure that the seals (15) are in a good condition. If necessary replace the AIPC 21-63-03-07-100 SEAL (15) or AIPC 21-63-83-01-340 SEAL (15).
     (e) Put the O-ring (15) in position on the trim air valve (8).
     (f) Put the trim air valve (8) in position on the duct flange (17) and install the clamp (14).
     (g) Make sure that the trim air valve is in the correct position.
     (h) TORQUE the clamp (14) to between 0.546 and 0.491 m.daN (48.32 and 43.45 lbf.in )
T.
NOTE: The electrical actuator of the trim air valve (8) must face in a forward direction.
     (i) Put the O-ring (15) in position on the duct assembly (11).
     (j) Move the duct assembly (11) downwards and into position on the trim air valve (8).
     (k) Install the clamp (22).
     (l) TORQUE the clamp (22) to between 0.546 and 0.491 m.daN (48.32 and 43.45 lbf.in )
T.
     (m) Put the bonding strap (21) in position and install the washer (20), the screw (19), the washer (13) and the nut (12) (
Ref. AMM TASK 20-28-00-912-802).
     (n) Remove the blanking caps from the disconnected electrical connectors.
     (o) Make sure that all the electrical connections are clean and in the correct condition.
     (p) Connect the electrical connector (9).
     (q) Make sure that the work area is clean and clear of tools and other items.
   (2) FOR [12HK] (TRIM VALVE FWD CAB)
     (a) Remove the blanking plugs from the duct flange (16), the trim air valve (6) and the duct assembly (11),
     (b) Clean the component interfaces and the adjacent area.
     (c) Make sure that the parts retained from the removed component are clean and in the correct condition.
     (d) Make sure that the seals (15) are in a good condition. If necessary replace the AIPC 21-63-03-07-100 SEAL (15) or AIPC 21-63-83-01-340 SEAL (15).
     (e) Put the seal (15) in position on the trim air valve (6).
     (f) Put the trim air valve (6) in position on the duct flange (16) and install the clamp (14).
     (g) Make sure that the trim air valve is in the correct position.
     (h) TORQUE the clamp (14) to between 0.546 and 0.491 m.daN (48.32 and 43.45 lbf.in )
T.
NOTE: The electrical actuator of the trim air valve (6) must face in a rearwards direction.
     (i) Put the seal (15) in position on the duct assembly (11).
     (j) Move the duct assembly (11) downwards and into position on the trim air valve (6).
     (k) Install the clamp (22).
     (l) TORQUE the clamp (22) to between 0.546 and 0.491 m.daN (48.32 and 43.45 lbf.in )
T.
     (m) Put the bonding strap (21) in position and install the washer (20), the screw (19), the washer (13) and the nut (12) (
Ref. AMM TASK 20-28-00-912-802).
     (n) Remove the blanking caps from the disconnected electrical connectors.
     (o) Make sure that all the electrical connections are clean and in the correct condition.
     (p) Connect the electrical connector (7).
     (q) Make sure that the work area is clean and clear of tools and other items.
   (3) FOR [13HK] (TRIM VALVE AFT CAB)
     (a) Remove the blanking plugs from the duct flange (18), the trim air valve (4) and the duct assembly (11),
     (b) Clean the component interfaces and the adjacent area.
     (c) Make sure that the parts retained from the removed component are clean and in the correct condition.
     (d) Make sure that the seals (15) are in a good condition. If necessary replace the AIPC 21-63-03-07-100 SEAL (15) or AIPC 21-63-83-01-340 SEAL (15).
     (e) Put seal (15) in position on the trim air valve (4).
     (f) Put the trim air valve (4) in position on the duct flange (18) and install the clamp (14).
     (g) Make sure that the trim air valve is in the correct position.
     (h) TORQUE the clamp (14) to between 0.546 and 0.491 m.daN (48.32 and 43.45 lbf.in )
T.
NOTE: The electrical actuator of the trim air valve (4) must face in a rearwards direction.
     (i) Put the seal (15) in position on the duct assembly (11).
     (j) Move the duct assembly (11) downwards and into position on the trim air valve (4).
     (k) Install the clamp (22).
     (l) TORQUE the clamp (22) to between 0.546 and 0.491 m.daN (48.32 and 43.45 lbf.in )
T.
     (m) Put the bonding strap (21) in position and install the washer (20), the screw (19), the washer (13) and the nut (12) (
Ref. AMM TASK 20-28-00-912-802).
     (n) Remove the blanking caps from the disconnected electrical connectors.
     (o) Make sure that all the electrical connections are clean and in the correct condition.
     (p) Connect the electrical connector (5).
     (q) Make sure that the work area is clean and clear of tools and other items.
Subtask 21-63-51-865-053-A
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUAIR COND/TEMP CTL/SYS 1 CHAN B/28VDC52HHD08
** ON A/C NOT FOR ALL
122VUAIR COND/ZONE TEMP CTL/28VDC/SYS24HKV20
122VUAIR COND/ZONE TEMP CTL/28VDC/SYS13HKV19
122VUAIR COND/ZONE TEMP CTL/115VAC/SYS22HKV18
122VUAIR COND/ZONE TEMP CTL/115VAC/SYS11HKV17
** ON A/C NOT FOR ALL
122VUAIR COND/TEMP CTL SYS 2/CHAN A/115VAC53HHW22
122VUAIR COND/TEMP CTL SYS 2/CHAN A/28VDC55HHW21
122VUAIR COND/TEMP CTL SYS 1/CHAN A/115VAC49HHX22
122VUAIR COND/TEMP CTL SYS 1/CHAN A/28VDC51HHX21
122VUAIR COND/TEMP CTL SYS 2/CHAN B/28VDC56HHY21
122VUAIR COND/TEMP CTL SYS 2/CHAN B/115VAC54HHY20
122VUAIR COND/TEMP CTL SYS 1/CHAN B/115VAC50HHY18
Subtask 21-63-51-710-050-A
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 trim air valve connections.
NOTE: Leaks are not permitted.
   (3) After approx. 15 minutes stop the pre-conditioning (Ref. AMM TASK 12-33-21-618-001) (Ref. AMM TASK 12-33-21-618-001).
   (4) Do the operational test of the cockpit and cabin temperature control system (Ref. AMM TASK 21-63-00-710-004)>.
Subtask 21-63-51-420-052-B 5. Close-up
Subtask 21-63-51-410-050-A
A. Close Access
   (1) Install the access panels at partition FR 34 (
Ref. AMM TASK 25-54-12-400-001).
   (2) Remove the access platform(s).
   (3) Close forward cargo-compartment door 825 (Ref. AMM TASK 52-30-00-860-002).
   (4) Remove the WARNING NOTICE(S).
Subtask 21-63-51-862-050-A
B. De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
[Rev.10 from 2021] 2026.04.02 06:11:44 UTC