W DOC AIRBUS | AMM A320F

Detailed Inspection of Horizontal Stabilizer Hinge Fittings and Support Ribs and Actuator Fittings for the Elevator, LH/RH


TASK 55-16-00-200-004-A
Detailed Inspection of Horizontal Stabilizer Hinge Fittings and Support Ribs and Actuator Fittings for the Elevator, LH/RH


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: 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: YOU MUST PUT ON AND ATTACH A SAFETY HARNESS BEFORE YOU START WORK:
  • ON THE THS OR IN THE REAR FUSELAGE
  • ON TOP OF THE WINGS OR PYLONS.
WITHOUT A SAFETY HARNESS, YOU CAN FALL. THIS CAN KILL YOU OR CAUSE YOU INJURY.
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.
WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
CAUTION: DO NOT CAUSE DAMAGE TO THE SURFACES. THE COMPONENTS ARE MADE OF CARBONFIBER REINFORCED PLASTIC.
ZONE: 334
ZONE: 344
1. Reason for the Job
Refer to the MPD TASK: 551020-01
DETAILED INSPECTION OF HORIZONTAL STABILIZER, HINGE FITTINGS AND SUPPORT RIBS AND ACTUATOR FITTINGS FOR THE ELEVATOR, LH/RH
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
AR
WARNING NOTICE(S)
98D27903500000
2
PIN-SIDE STICK LOCKING
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.05RCB1)
Adhesive Film Tape-Masking or Labelling Film Polyester -
(Material No.05RDA1)
Adhesive Film Tape-Masking - -
(Material No.08BAA9)
Non Aqueous Cleaner-General - -
(Material No.12ABB1)
Corrosion Preventive Compound-Water Displacing Hard Film -
(Material No.12ABC1)
Corrosion Preventive Compound_Water Displacing Soft Film -
(Material No.14SBA1)
Textile-Lint free Cotton -
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
334
THS TRAILING EDGE
344
THS TRAILING EDGE
334AT, 334BB, 334BT, 334CT, 334DB, 334DT, 334FB, 334HB, 344AT, 344BB, 344BT, 344CT, 344DB, 344DT, 344FB, 344HB
 D. Referenced Information
REFERENCE
DESIGNATION
TASK 29-10-00-864-001-A
Depressurize the Green Hydraulic System
TASK 29-10-00-864-002-A
Depressurize the Yellow Hydraulic System
TASK 29-10-00-864-003-A
Depressurize the Blue Hydraulic System
TASK 51-78-00-916-001-A
Application of Temporary Protection System (TPS)
TASK 55-13-11-000-001-A
Remove/Open of the Trimmable Horizontal Stabilizer (THS) Trailing-Edge Access-Panels
TASK 55-13-11-400-001-A
Install/Close of the Trimmable Horizontal Stabilizer (THS) Trailing-Edge Access-Panels
SRM 551600
3. Job Set-up
Subtask 55-16-00-860-053-A
A. Depressurize Hydraulic Systems
   (1) Depressurize the Green, Yellow and Blue hydraulic systems. (Ref. AMM TASK 29-10-00-864-001) (Ref. AMM TASK 29-10-00-864-002) (Ref. AMM TASK 29-10-00-864-003)
Subtask 55-16-00-865-057-A
B. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/ELAC1/NORM/SPLY15CE1B11
49VUFLIGHT CONTROLS/THS/ACTR/MOT219CE2B09
49VUFLIGHT CONTROLS/SEC1/NORM/SPLY21CE1B08
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/ELAC1/NORM/SPLY15CE1B06
49VUFLIGHT CONTROLS/THS/ACTR/MOT219CE2B04
49VUFLIGHT CONTROLS/SEC1/NORM/SPLY21CE1B03
** ON A/C ALL
105VUFLIGHT CONTROLS/ELAC2/STBY SPLY16CE2A02
105VUFLT CTL/ELAC1/STBY SPLY16CE1A01
105VUFLT CTL/SEC1/STBY SPLY22CEB01
121VUFLIGHT CONTROLS/SEC3/SPLY21CE3Q19
121VUFLIGHT CONTROLS/SEC2/SPLY21CE2Q18
121VUFLIGHT CONTROLS/THS ACTR/MOT319CE3Q17
121VUFLIGHT CONTROLS/THS ACTR/MOT119CE1Q16
121VUFLIGHT CONTROLS/ELAC2/NORM/SPLY15CE2R20
Subtask 55-16-00-481-053-A
C. Install Locking Devices
   (1) Put the 98D27903500000 PIN-SIDE STICK LOCKING in the CAPT and F/O side stick controllers.
Subtask 55-16-00-941-057-A
D. Safety Precautions
   (1) Put the WARNING NOTICE(S) in the flight compartment to tell persons not to operate the flight controls.
   (2) Put the WARNING NOTICE(S) in position to tell persons not to operate the hydraulic systems.
   (3) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at zone 334 for the left hand THS and/or zone 344 for the right hand THS.
Subtask 55-16-00-010-054-A Subtask 55-16-00-560-050-A
F. Preparation of the Inspection Area
   (1) Make sure that the inspection area is sufficiently clean to do a satisfactory inspection of the area.
   (2) If not, clean the inspection area with Non Aqueous Cleaner-General - - (Material No.08BAA9) and Textile-Lint free Cotton - (Material No.14SBA1) .
   (3) If there is a TPS layer and if it does not let you do a satisfactory inspection, remove the TPS layer (Ref. AMM TASK 51-78-00-916-001).
4. Procedure
Subtask 55-16-00-210-056-A
A. Detailed Inspection
   (1) Make a detailed inspection of the horizontal stabilizer hinge fittings, support ribs and actuator fittings for the elevator and the adjacent structure for:
  • delamination,
  • deterioration of the structure,
  • scratches, marks and dents,
  • cracks,
  • corrosion,
  • condition of the bearings,
  • damaged paintwork. gives details.
   (2) If damage is found, look for allowable damage limits SRM 551600.
Subtask 55-16-00-916-051-A
B. Application of Corrosion Preventive Compound
   (1) Cover the area adjacent to the elevator hinge supports and the attachment fittings with Adhesive Film Tape-Masking or Labelling Film Polyester - (Material No.05RCB1) and Adhesive Film Tape-Masking - - (Material No.05RDA1) .
   (2) If there is a TPS layer, do a check of the condition and integrity of the TPS layer (Ref. AMM TASK 51-78-00-916-001).
NOTE: Airbus recommends that you always apply a new layer of TPS. This is to make sure that the TPS layer continues to give satisfactory corrosion protection. If, after the check, you think that the TPS layer is in the correct condition, you can apply a new layer as a spray on the existing layer.
   (3) If the TPS layer has local damage, remove the damaged TPS layer and apply a new layer of Corrosion Preventive Compound_Water Displacing Soft Film - (Material No.12ABC1) or Corrosion Preventive Compound-Water Displacing Hard Film - (Material No.12ABB1) on the inspection area (Ref. AMM TASK 51-78-00-916-001).
   (4) If, before the inspection, there was:
  • Removal of the TPS layer
  • Or cleaning of the inspection area with high pressure water, steam, solvents and/or cleaning agents
    Apply a full new layer of Corrosion Preventive Compound_Water Displacing Soft Film - (Material No.12ABC1) or Corrosion Preventive Compound-Water Displacing Hard Film - (Material No.12ABB1) on the inspection area.
NOTE: Do not apply the corrosion preventive compound to the bush or bearing of each fitting assembly.
   (5) Remove the masking tape from the adjacent structure area.
5. Close-up
Subtask 55-16-00-410-056-A
A. Visual Inspection
   (1) Make sure that the work area is clean and clear of tools and other items.
Subtask 55-16-00-410-057-A
B. Close Access
   (1) Close the access panels 334AT 334BB 334BT 334CT 334DB 334DT 334FB 334HB and/or 344AT 344BB 344BT 344CT 344DB 344DT 344FB 344HB. (Ref. AMM TASK 55-13-11-400-001)
Subtask 55-16-00-942-053-A
C. Remove Ground Equipment
   (1) Remove the WARNING NOTICE(S).
   (2) Remove the access platform(s).
Subtask 55-16-00-810-050-A
D. Remove Locking Devices
   (1) Remove the 98D27903500000 PIN-SIDE STICK LOCKING from the CAPT and F/O side stick controllers.
Subtask 55-16-00-865-058-A
E. 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
49VUFLIGHT CONTROLS/SEC1/NORM/SPLY21CE1B08
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/ELAC1/NORM/SPLY15CE1B06
49VUFLIGHT CONTROLS/THS/ACTR/MOT219CE2B04
49VUFLIGHT CONTROLS/SEC1/NORM/SPLY21CE1B03
** ON A/C ALL
105VUFLIGHT CONTROLS/ELAC2/STBY SPLY16CE2A02
105VUFLT CTL/ELAC1/STBY SPLY16CE1A01
105VUFLT CTL/SEC1/STBY SPLY22CEB01
121VUFLIGHT CONTROLS/SEC3/SPLY21CE3Q19
121VUFLIGHT CONTROLS/SEC2/SPLY21CE2Q18
121VUFLIGHT CONTROLS/THS ACTR/MOT319CE3Q17
121VUFLIGHT CONTROLS/THS ACTR/MOT119CE1Q16
121VUFLIGHT CONTROLS/ELAC2/NORM/SPLY15CE2R20
[Rev.10 from 2021] 2026.04.01 04:12:53 UTC