W DOC AIRBUS | AMM A320F

Removal of the Mixer Flap Actuator


TASK 21-51-52-000-001-A
Removal of the Mixer Flap Actuator


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.
FIN: 20HB
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
ACCESS PLATFORM 2M (6 FT)
No specific
AR
CAP - BLANKING
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
AR
WARNING NOTICE(S)
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
131NW, 131PW, 825
 C. Referenced Information
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 25-54-12-000-001-A
Removal 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
3. Job Set-up
Subtask 21-51-52-861-051-A
A. Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
Subtask 21-51-52-865-050-A
B. Open, safety and tag 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/FLOW/MIXER/FLAP3HBV22
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 ALL
122VUAIR COND/RECIRC FAN/R/CTL11HGW20
122VUAIR COND/RECIRC FAN/R/SPLY3HGW18
122VUAIR COND/RECIRC FAN/L/CTL2HGX20
122VUAIR COND/RECIRC FAN/L/SPLY1HGX18
** 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 21-51-52-941-051-A
C. Safety Precautions
   (1) On the overhead panel, on AIR COND panel 30VU:
     (a) Make sure that:
  • The APU BLEED pushbutton switch is released (the ON legend is off).
  • The ENG 1 BLEED and the ENG 2 BLEED pushbutton switches are released (the OFF legends are on).
     (b) Put a WARNING NOTICE(S) in position to tell persons not to operate these pushbutton switches.
   (2) On the HP and the LP ground connectors, put a WARNING NOTICE(S) in position to tell persons not to supply the ground air.
Subtask 21-51-52-010-050-A
D. Get Access
   (1) Put an ACCESS PLATFORM 2M (6 FT) in position at the forward cargo-compartment door 825.
WARNING: DO NOT OPEN OR GO NEAR PRESSURE-SEALED DOORS WHEN THE AIRCRAFT IS PRESSURIZED. A PRESSURE-SEALED DOOR THAT OPENS WHEN THE AIRCRAFT IS PRESSURIZED:
  • WILL CAUSE EXPLOSIVE DECOMPRESSION.
  • CAN KILL OR CAUSE INJURY TO PERSONS AND/OR CAUSE DAMAGE TO THE AIRCRAFT OR EQUIPMENT.
   (2) Open the FWD cargo-compartment door 825 (Ref. AMM TASK 52-30-00-860-001).
   (3) Remove access panels 131PW and 131NW (Ref. AMM TASK 25-54-12-000-001).
4. Procedure
Subtask 21-51-52-020-050-A
A. Removal of the Mixer Flap Actuator
   (1) Disconnect the electrical connector (3).
   (2) Put the CAP-BLANKING on each disconnected electrical connector and receptacle.
   (3) Loosen the clamp (8) and disconnect the sleeve (7).
   (4) Remove the nuts (13), the washers (12) and the bolts (10).
   (5) Carefully remove the mixer-flap actuator housing (9) and the seal (11).
   (6) Remove the bolts (4), the washers (5) and the mixer flap actuator (6).
   (7) Put protective covers on the open ends of the sleeve (7), the mixer unit (14) and the mixer-flap actuator housing (9).
[Rev.10 from 2021] 2026.04.05 10:34:31 UTC