W DOC AIRBUS | AMM A320F

Installation of the Air-Inlet Flap Mechanism


TASK 21-61-51-400-003-A
Installation of the Air-Inlet Flap Mechanism


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.
NOTE: The procedure is the same for the left and the right air-inlet flap mechanism .
FIN: 28HH
FIN: 8HH
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
191BB, 192FB
 B. Referenced Information
REFERENCE
DESIGNATION
TASK 21-61-00-710-001-A
Operational Test of the Pack Temperature-Control System
TASK 21-61-51-000-001-A
Removal of the Air-Inlet Flap Actuator
TASK 21-61-51-400-001-A
Installation of the Air-Inlet Flap Actuator
TASK 21-61-51-820-001-A
Adjustment of the Air Inlet Flap
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 53-35-13-000-002-A
Removal of the Quick-Release Access Panels from the Belly Fairing Structure
TASK 53-35-13-400-002-A
Installation of the Quick-Release Access Panels on the Belly Fairing Structure
3. Job Set-up
Subtask 21-61-51-860-050-A
A. Aircraft Maintenance Configuration
   (1) Make sure that:
     (a) The aircraft electrical circuits are energized (Ref. AMM TASK 24-41-00-861-002).
     (b) On the panel 30VU:
       1 The APU BLEED and the ENG BLEED/1(2) pushbutton switches are released.
       2 The warning notice to tell persons not to operate these pushbutton switches is in position.
     (c) On the HP ground connector the warning notice to tell persons not to supply the ground air is in position.
     (d) The access panel is removed (Ref. AMM TASK 53-35-13-000-002).
       1 For the Left air-inlet flap mechanism,
       2 For the Right air-inlet flap mechanism,
     (e) The air-inlet flap actuator is removed (Ref. AMM TASK 21-61-51-000-001).
       1 For the left air-inlet flap mechanism,
  • 8HH.
       2 For the Right air-inlet flap mechanism,
  • 28HH.
Subtask 21-61-51-865-060-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/PACK TEMP/CTL SYS1/2/115VAC21HHW22
122VUAIR COND/PACK TEMP/CTL SYS1/2/28VDC23HHW21
122VUAIR COND/PACK TEMP/CTL SYS1/1/115VAC1HHX22
122VUAIR COND/PACK TEMP/CTL SYS1/1/28VDC3HHX21
122VUAIR COND/PACK TEMP CTL SYS2/2/28VDC24HHY21
122VUAIR COND/PACK TEMP CTL SYS2/2/115VAC22HHY20
122VUAIR COND/PACK TEMP CTL SYS2/1/28VDC4HHY19
122VUAIR COND/PACK TEMP CTL SYS2/1/115VAC2HHY18
** 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 21-61-51-420-052-B
A. Installation of the Air-Inlet Flap Mechanism
   (1) Make sure that the parts retained from the removed component are clean and in the correct condition.
   (2) Put the lever (12) in position in the bracket (15).
   (3) Install the bolt (1), the bushing (18), the washer (19) the nut (20) and the cotter (21).
   (4) Put the tie-rod (10) in position in the lever (12) and install the bushing (8), the bolt (7), the washer (11) and the nut (16).
   (5) Move the air inlet to the open position.
   (6) Put the tie rod (10) in position in the bracket (17) and install the sleeve (8), the bolt (7), the washer (11) and the nut (16).
   (7) Install the air-inlet flap actuator (Ref. AMM TASK 21-61-51-400-001).
   (8) Do the adjustment of the air inlet flap (Ref. AMM TASK 21-61-51-820-001).
   (9) Make sure that the work area is clean and clear of tools and other items.
Subtask 21-61-51-865-077-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
FOR FIN: 8HH (P1 RAM AIR IN ACTUATOR)
49VUAIR COND/TEMP CTL/SYS 1 CHAN B/28VDC52HHD08
** ON A/C NOT FOR ALL
122VUAIR COND/PACK TEMP/CTL SYS1/1/115VAC1HHX22
122VUAIR COND/PACK TEMP/CTL SYS1/1/28VDC3HHX21
122VUAIR COND/PACK TEMP CTL SYS2/1/28VDC4HHY19
122VUAIR COND/PACK TEMP CTL SYS2/1/115VAC2HHY18
** ON A/C NOT FOR ALL
122VUAIR COND/TEMP CTL SYS 1/CHAN A/115VAC49HHX22
122VUAIR COND/TEMP CTL SYS 1/CHAN A/28VDC51HHX21
122VUAIR COND/TEMP CTL SYS 1/CHAN B/115VAC50HHY18
** ON A/C NOT FOR ALL
FOR FIN: 28HH (P2 RAM AIR IN ACTUATOR)
122VUAIR COND/PACK TEMP/CTL SYS1/2/115VAC21HHW22
122VUAIR COND/PACK TEMP/CTL SYS1/2/28VDC23HHW21
122VUAIR COND/PACK TEMP CTL SYS2/2/28VDC24HHY21
122VUAIR COND/PACK TEMP CTL SYS2/2/115VAC22HHY20
** 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 2/CHAN B/28VDC56HHY21
122VUAIR COND/TEMP CTL SYS 2/CHAN B/115VAC54HHY20
Subtask 21-61-51-710-053-A
C. Do the operational test of the pack temperature-control system (Ref. AMM TASK 21-61-00-710-001).
5. Close-up
Subtask 21-61-51-410-054-A
A. Close Access
   (1) Remove the WARNING NOTICE(S).
   (2) Make sure that the work area is clean and clear of tools and other items.
   (3) Install the access panel (Ref. AMM TASK 53-35-13-400-002).
     (a) For the Left air-inlet flap mechanism,
     (b) For the Right air-inlet flap mechanism,
Subtask 21-61-51-862-050-A
B. De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
[Rev.10 from 2021] 2026.04.02 06:49:00 UTC