W DOC AIRBUS | AMM A320F

Inspection of the Air Inlet Flap Backlash


TASK 21-61-51-200-002-A
Inspection of the Air Inlet Flap Backlash


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.
1. Reason for the Job
This procedure is optional. It is to assist in early detection of possible excessive wear in the ram-air inlet flap offset mechanism system.
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
 B. Referenced Information
REFERENCE
DESIGNATION
TASK 21-61-00-300-001-A
Attachment and Linkage Components - Repair/Replacement
TASK 21-61-51-000-003-A
Removal of the Air-Inlet Flap Mechanism
TASK 21-61-51-200-003-A
Air-Inlet Flap Mechanism - In-Service Wear Limits
TASK 21-61-51-400-003-A
Installation of the Air-Inlet Flap Mechanism
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)
3. Job Set-up
Subtask 21-61-51-861-056-A
A. Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002)
Subtask 21-61-51-865-067-A
B. Open, safety and tag 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 21-61-51-941-056-A
C. Safety Precautions
   (1) On the panel 30VU:
     (a) Make sure that the APU BLEED and the ENG BLEED/1(2) pushbutton switches are released.
     (b) Put a warning notice in position to tell persons not to operate these pushbutton switches.
   (2) On the HP ground connector put a warning notice in position to tell persons not to supply the ground air.
4. Procedure
Subtask 21-61-51-220-051-A
A. Measurement of the Air Inlet Flap Backlash
   (1) At the centre line of the air inlet flap (1) and the diffuser nose (2):
     (a) Measure and note the dimension "A".
     (b) Measure and note the dimension "B".
NOTE: The measurement for the dimension "B" must be made with the load applied (hand pressure). Do not apply excessive hand pressure as this could result in a false measurement.
   (2) Subtract dimension "A" from dimension "B". This will give you the backlash which exists in the air-inlet flap system.
   (3) If the backlash is more than 3mm (0.118 in) you must do a check of the in-service wear limits of the air-inlet flap mechanism (Ref. AMM TASK 21-61-51-000-003) and (Ref. AMM TASK 21-61-51-200-003).
   (4) If necessary replace the affected parts (Ref. AMM TASK 21-61-51-400-003) and (Ref. AMM TASK 21-61-00-300-001).
   (5) Make sure that the work area is clean and clear of tools and other items.
5. Close-up
Subtask 21-61-51-865-068-A
A. 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 21-61-51-410-058-A
B. Remove the WARNING NOTICE(S).
Subtask 21-61-51-862-056-A
C. De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
[Rev.10 from 2021] 2026.04.02 06:11:40 UTC