W DOC AIRBUS | AMM A320F

Removal of the Flight Control Pressure Switch


TASK 27-92-17-000-003-A
Removal of the Flight Control Pressure Switch


WARNING: MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING GEAR. THIS WILL PREVENT UNWANTED MOVEMENT OF THE LANDING GEAR, AND THUS POSSIBLE INJURY TO PERSONS AND DAMAGE TO THE AIRCRAFT AND/OR EQUIPMENT.
FIN: 10CE1
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
1
CONTAINER - HYDRAULIC FLUID RESISTANT
No specific
AR
PLUG - BLANKING
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
1
WARNING NOTICE(S)
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
195BB
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 29-00-00-864-001-A
Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action
TASK 29-00-00-910-002-A
Safety Procedures of the Hydraulic System
TASK 29-14-00-614-001-A
Depressurization of the Hydraulic Reservoirs
3. Job Set-up
Subtask 27-92-17-860-054-A
A. Aircraft Maintenance Configuration
WARNING: MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS SURFACES ARE CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT.
WARNING: OBEY THE HYDRAULIC SAFETY PROCEDURES.
   (1) Obey the hydraulic safety procedures (Ref. AMM TASK 29-00-00-910-002).
   (2) Make sure that the Blue hydraulic system is depressurized and put it in the maintenance configuration.
(Ref. AMM TASK 29-00-00-864-001).
   (3) Depressurize the reservoir of the Blue hydraulic system (Ref. AMM TASK 29-14-00-614-001).
Subtask 27-92-17-010-053-A
B. Open the access panel 195BB.
Subtask 27-92-17-941-052-A
C. Safety Precautions
   (1) Put the WARNING NOTICE(S) in position to tell persons not to pressurize the Blue hydraulic system:
  • In the cockpit on the hydraulic section 40VU of the overhead panel,
  • On the ground service panel of the Blue hydraulic system.
   (2) Put the CONTAINER - HYDRAULIC FLUID RESISTANT in position below the flight control pressure switch to collect hydraulic fluid.
Subtask 27-92-17-865-052-A
D. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/ELAC1/NORM/SPLY15CE1B11
49VUFLIGHT CONTROLS/SEC1/NORM/SPLY21CE1B08
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/ELAC1/NORM/SPLY15CE1B06
49VUFLIGHT CONTROLS/SEC1/NORM/SPLY21CE1B03
** ON A/C ALL
105VUFLIGHT CONTROLS/ELAC2/STBY SPLY16CE2A02
105VUFLT CTL/ELAC1/STBY SPLY16CE1A01
121VUFLIGHT CONTROLS/ELAC2/NORM/SPLY15CE2R20
4. Procedure
Subtask 27-92-17-020-054-B
A. Removal of the Flight Control Pressure Switch 10CE1
   (1) Disconnect the electrical connector (1).
   (2) Put a CAP - BLANKING on the disconnected electrical connector (1).
   (3) Remove the nut (5), the washer (6), the screw (8), the bonding strap (7) and the clamp (9) from the flight control pressure switch (2).
   (4) Cut and remove the lockwire.
   (5) Loosen the flight control pressure switch (2) and remove it together with the packing (3) from the manifold (4).
   (6) Discard the packing.
   (7) Install the PLUG - BLANKING in the open ports.
[Rev.10 from 2021] 2026.03.31 23:58:45 UTC