W DOC AIRBUS | AMM A320F

Installation of the Position Transducer to the THS Actuator

TASK 27-44-56-400-001-A
Installation of the Position Transducer to the THS Actuator

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.
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: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
ZONE: 310
FIN: 9CE
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 3M (10 FT)- ADJUSTABLE
No specific
AR
WARNING NOTICE(S)
No specific
Torque wrench: range to between 0.94 and 0.76 m.daN (83.19 and 67.26 lbf.in ) T
0U190360
1
PIN-RIGGING,THS ACTUATOR,MECHANICAL INPUT LEVER
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.08BBB1)
Non Aqueous Cleaner-- Petroleum Based -
(Material No.14QEB1)
Wire-Locking Dia: 0.6 mm CRES Nickel Alloy -
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
310
FUSLG TAIL SECTION AFT OF AFT PRESS BHD
312AR
 D. Expendable Parts
FIG.ITEM
DESIGNATION
IPC-CSN
9
PACKING
AIPC 27-44-56-01-020
 E. Referenced Information
REFERENCE
DESIGNATION
TASK 27-41-00-720-001-A
Functional Test of the THS-Actuator Overtravel Related to the Mechanical Indicator
TASK 27-44-51-210-004-A
Check Oil Level of THS Actuator Gearbox
TASK 29-00-00-864-001-A
Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action
F Position Transducer
3. Job Set-up
Subtask 27-44-56-860-053-A
A. Aircraft Maintenance Configuration
   (1) Make sure that Green and the Yellow hydraulic systems are depressurized and put them in the maintenance configuration. (Ref. AMM TASK 29-00-00-864-001).
   (2) Make sure that the THS actuator (1) near to the zero position.
   (3) Make sure that the 0U190360 PIN-RIGGING,THS ACTUATOR,MECHANICAL INPUT LEVER is installed in the mechanical input of the THS actuator (1).
   (4) Make sure that the WARNING NOTICE(S) are in the position.
   (5) Make sure that the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE is in position.
   (6) Make sure that the access door is opened 312AR.
Subtask 27-44-56-865-051-A
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/ELAC1/NORM/SPLY15CE1B11
49VUFLIGHT CONTROLS/THS/ACTR/MOT219CE2B09
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/ELAC1/NORM/SPLY15CE1B06
49VUFLIGHT CONTROLS/THS/ACTR/MOT219CE2B04
** ON A/C ALL
105VUFLT CTL/ELAC1/STBY SPLY16CE1A01
121VUFLIGHT CONTROLS/THS ACTR/MOT319CE3Q17
121VUFLIGHT CONTROLS/THS ACTR/MOT119CE1Q16
4. Procedure
Subtask 27-44-56-910-052-A
A. Preparation for the Installation
   (1) Make sure that the interface of the THS actuator (1) is clean and has no corrosion and shows no damage.
   (2) Make sure that the parts retained from the removed component are clean and in the correct condition.
   (3) Make sure that all the electrical connections are clean and in the correct condition.
   (4) Clean the interface of the THS actuator (1) and the position transducer (2) with the Non Aqueous Cleaner-- Petroleum Based - (Material No.08BBB1) and let it dry.
   (5) Make sure that the AIPC 27-44-56-01-020 PACKING (9) is in the correct condition. If necessary, replace the packing.
Subtask 27-44-56-420-050-A
B. Installation of the Position Transducer
NOTE: The installation of the Command (COM) position transducer and the installation of the Monitor (MON) position transducer are the same. The installation procedure for one of the position transducers only is given.
   (1) Put the position transducer (2) in position at the THS actuator (1).
   (2) Hold the position transducer (2) in position at the THS actuator (1) and attach it with the screws (7) and the washers (8).
   (3) TORQUE the screws (7) to between 0.94 and 0.76 m.daN (83.19 and 67.26 lbf.in ) T.
   (4) Safety the screws (7) with lockwire 0.6 mm (0.0236 in.) 14QEB1Wire-Locking Dia: 0.6 mm CRES Nickel Alloy -.
   (5) Remove the blanking caps and connect the electrical connectors (3), (4) to the receptacles (5), (6).
Subtask 27-44-56-860-052-A
C. Preparation for the Test
   (1) Make sure that the THS actuator 9CE has the correct quantity of oil (Ref. AMM TASK 27-44-51-210-004).
   (2) Remove the rigging pin OU 190360 from the mechanical input of the THS actuator 9CE.
   (3) Make sure that the travel range of the THS actuator 9CE and the travel range of the control surfaces are free.
Subtask 27-44-56-865-052-A
D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/ELAC1/NORM/SPLY15CE1B11
49VUFLIGHT CONTROLS/THS/ACTR/MOT219CE2B09
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/ELAC1/NORM/SPLY15CE1B06
49VUFLIGHT CONTROLS/THS/ACTR/MOT219CE2B04
** ON A/C ALL
105VUFLT CTL/ELAC1/STBY SPLY16CE1A01
121VUFLIGHT CONTROLS/THS ACTR/MOT319CE3Q17
121VUFLIGHT CONTROLS/THS ACTR/MOT119CE1Q16
Subtask 27-44-56-720-050-A
E. Do a functional test of the THS actuator overtravel related to the mechanical indicator (Ref. AMM TASK 27-41-00-720-001).
5. Close-up
Subtask 27-44-56-410-050-A
A. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Close the access door 312AR.
   (3) Remove the WARNING NOTICE(S).
   (4) Remove the access platform(s).
[Rev.10 from 2021] 2026.04.01 06:54:33 UTC
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