W DOC AIRBUS | AMM A320F

Removal of the Air-Inlet Flap Actuator


TASK 21-61-51-000-001-A
Removal of the Air-Inlet 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.
NOTE: The procedure is the same for the air-inlet flap actuator 8HH and 28HH.
FIN: 28HH
FIN: 8HH
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
CAP - BLANKING
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
FOR [28HH] (P2 RAM AIR IN ACTUATOR)
192FB, 192KB
FOR [8HH] (P1 RAM AIR IN ACTUATOR)
191BB, 191KB
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 21-61-51-200-003-A
Air-Inlet Flap Mechanism - In-Service Wear Limits
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 53-35-13-000-002-A
Removal of the Quick-Release Access Panels from the Belly Fairing Structure
3. Job Set-up
Subtask 21-61-51-861-051-A
A. Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
Subtask 21-61-51-865-072-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 21-61-51-941-052-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.
Subtask 21-61-51-010-050-A
D. Get Access
   (1) Remove the access panel (Ref. AMM TASK 53-35-13-000-002).
     (a) FOR [8HH] (P1 RAM AIR IN ACTUATOR)
     (b) FOR [28HH] (P2 RAM AIR IN ACTUATOR)
4. Procedure
Subtask 21-61-51-020-050-B
A. Removal of the Air-Inlet Flap Actuator
CAUTION: MAKE SURE THAT THE ELECTRICAL CONNECTORS ARE CLEAN BEFORE YOU DISCONNECT OR CONNECT THEM. CONTAMINATION ON THE ELECTRICAL CONNECTORS CAN CAUSE DAMAGE TO EQUIPMENT.
   (1) Disconnect the electrical connector (1).
   (2) Put the CAP-BLANKING on each disconnected electrical connector and receptacle.
   (3) Remove the nut (8), the washer (7) and the screw (2).
CAUTION: MAKE SURE THAT THE ELECTRICAL CONNECTOR(S) IS(ARE) DISCONNECTED BEFORE YOU DISCONNECT THE BONDING STRAP(S).
   (4) Disconnect the bonding strap (3).
WARNING: USE PROTECTIVE GOGGLES WHEN YOU REMOVE OR INSTALL A COTTER PIN. EACH TIME YOU REMOVE A COTTER PIN DURING THE TASK, DISCARD IT IMMEDIATELY. A LOOSE COTTER PIN CAN CUT YOU OR MAKE YOU BLIND.
   (5) Remove and discard the cotter pin (5).
   (6) Hold the air-inlet flap actuator (9) and remove:
  • The nut (6), the washer (4) and the bolt (16)
  • The nut (10), washer (11), bolt (14) and sleeve (13).
   (7) Remove the air-inlet flap actuator (9).
   (8) Do the inspection of the air-inlet-flap mechanism - in-service wear-limits (Ref. AMM TASK 21-61-51-200-003).
   (9) Measure dimension "C" and record it (Ref. AMM TASK 21-61-51-820-001).
[Rev.10 from 2021] 2026.03.31 23:08:54 UTC