W DOC AIRBUS | AMM A320F

Removal of the Solenoid Valve


TASK 27-26-51-000-003-A
Removal of the Solenoid Valve


WARNING: PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU START A TASK ON OR NEAR:
  • THE FLIGHT CONTROLS
  • THE FLIGHT CONTROL SURFACES
  • THE LANDING GEAR AND THE RELATED DOORS
  • COMPONENTS THAT MOVE.
MOVEMENT OF COMPONENTS CAN KILL OR CAUSE INJURY TO PERSONS AND/OR CAN CAUSE DAMAGE TO THE EQUIPMENT.
ZONE: 325
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
ACCESS PLATFORM 6M (20 FT) - ADJUSTABLE
No specific
AR
CONTAINER 3 L(3/4 USGAL)
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
AR
WARNING NOTICE(S)
98D27207549000
1
PIN-RIGGING
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
325
VERTICAL STABILIZER TRAILING EDGE
325BL, 325BR
 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
TASK 55-33-13-010-002-A
Opening/Removal of the Trailing Edge Access-Panels of the Vertical Stabilizer
3. Job Set-up
Subtask 27-26-51-010-053-B
A. Get Access
   (1) Put the ACCESS PLATFORM 6M (20 FT) - ADJUSTABLE in position.
   (2) Open the access panels 325BL (for the solenoid valve on 3CC1) and/or 325BR (for the solenoid valve on 3CC2) at the trailing edge of the vertical stabilizer (Ref. AMM TASK 55-33-13-010-002).
Subtask 27-26-51-860-052-B
B. 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) Put the rudder pedals in the neutral position.
   (3) Make sure that the rudder trim control is set at the zero position.
NOTE: Make sure that the trailing edge of the rudder is in line with the red triangle on the tail cone.
   (4) Put the WARNING NOTICE(S) in the flight compartment to tell persons not to operate the flight controls.
   (5) Depressurize the Green and the Yellow hydraulic systems and put them in the maintenance configuration (Ref. AMM TASK 29-00-00-864-001).
   (6) Make sure that the Blue hydraulic system is depressurized and put it in the maintenance configuration.
(Ref. AMM TASK 29-00-00-864-001).
   (7) Depressurize the reservoir of the Green and the Yellow hydraulic system (Ref. AMM TASK 29-14-00-614-001).
   (8) Put the warning notices in position to tell persons not to operate the Green, the Yellow and the Blue hydraulic systems:
  • in the cockpit on the hydraulic section 40VU of the overhead panel,
  • on the ground service panels of the Green, Yellow and Blue hydraulic systems.
   (9) Put a CONTAINER 3 L(3/4 USGAL) below the yaw damper to collect the unwanted fluid.
   (10) Put the rigging pin 98D27207549000 PIN-RIGGING in the yaw damper bellcrank.
Subtask 27-26-51-865-056-A
C. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUAUTO FLT/FAC1/28VDC5CC1B04
49VUAUTO FLT/FAC1/26VAC14CC1B03
** ON A/C NOT FOR ALL
49VUAUTO FLT/FAC1/28VDC5CC1H10
49VUAUTO FLT/FAC1/26VAC14CC1H09
** ON A/C ALL
121VUAUTO FLT/FAC2/28VDC5CC2M19
121VUAUTO FLT/FAC2/26VAC14CC2M18
4. Procedure
Subtask 27-26-51-020-052-A
A. Removal of the Solenoid Valve
   (1) Cut and remove the lockwire which safeties the screws (1).
   (2) Remove the screws (1) with the washers (2).
   (3) Remove the solenoid valve (3) from the yaw damper (7).
   (4) Remove and discard the packings (4),(5),(6).
   (5) Remove and discard the lock washer (8) and the packing (9).
[Rev.10 from 2021] 2026.03.31 23:49:53 UTC